VZ SERIES
T-Motor VZ16x6.5 VTOL 16 Zoll Carbon Propeller 1x CW 1x CCW
Artikelnr.: PM-7258 | HAN: VZ16x6.5
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VZ SERIES -VTOL PROPELLERS
Break through the performance limitations of traditional multi-rotor propellers. VZ series propellers deliver superior power, durability, and lightweight design for VTOL applications
What Does a VTOL Propeller Need?
High Strength High Stiffness & Lightweight Design
High Strength
Withstands immense centrifugal loads and maneuver-induced alternating loads at high RPM, preventing structural failure
High Stiffness
Ensures safe blade-tip clearance in compact layouts, suppresses aeroelastic deformation, and prevents flutter
Lightweight Design
Reduce the moment of inertia to achieve rapid thrust response and higher attitude control bandwidth for the flight control system
Superior Aerodynamic Design
The unique dual operational modes of VTOL—vertical takeoff/landing and cruise—demand new propeller capabilities
Vertical Takeoff & Landing Phase
Requiring high thrust and power, demanding maximum lift output from the propeller disk within a limited blade area
Cruise Phase
When the propeller stops rotating, it is necessary to minimize profile drag to reduce power consumption, achieving "stealthy" low-drag efficiency
Transition Stability: Resisting Complex Flow Field Interference
The extreme challenges posed by high angle of attack, low speed and unsteady flow field, coupled with the insufficient strength and poor transition stability of traditional blades, make this an accident-prone region
Unsteady Flow Fields at High Angle of Attack
The aircraft operates at high angles of attack and low speeds within an extremely complex flow environment
Asymmetric Airflow
Significant angle between incoming flow and the rotation axis causes asymmetric airflow entering the propeller disc
Severe Periodic Variations
Local forces on the blade fluctuate drastically per rotation, inducing flutter and causing significant thrust fluctuation
To address the challenges of traditional propellers in VTOL (Vertical Takeoff and Landing mode) applications
we introduce the VZ Series Propellers
Technical Features of the VZ Series Propellers
Advanced composite materials and exceptional aerodynamic design work in synergy to ensure consistently efficient, reliable, and controllable power output
Bending & Torsion Resistant Layup Design
Optimized fiber orientation and ratio maximize strength and stiffness
Prepreg Compression Molding for Integrated Forming
Product porosity below 1%, ensuring stable and reliable quality
PMI Foam Core
Lightweight, high-strength core material effectively increases stiffness while controlling total weight
30%
Flexural Strength
Significantly enhanced impact resistance and deformation resistance for greater durability in complex operating conditions
20%
Torsional Stiffness
Optimized power transmission efficiency reduces energy loss during operation
Blade Root Optimization: Safety Redundancy Design
The blade root thickness is optimized to provide structural redundancy while reducing loads on the connecting bolts
V30 Propeller
VZ30 Propeller
Aerodynamic Priority: Engineered for High VTOL Thrust
Dedicated High Lift-to- Drag Ratio Airfoil
Optimized for VTOL conditions to enhance maximum lift coefficient
Low-Drag Cruise Blade Shape
Improved aerodynamic blade boundaries reduce cruise drag
Specialized Blade Tip
Optimized tip design weakens vortex strength and enhances flight quality
Custom VTOL Propeller Service: 10 to 100 Inches
Supports precise matching with various pitch specifications and motors Full in-house R&D ensures stable and controllable quality
Aerodynamic/Structural Design
Mold Manufacturing
Composite Molding
Testing & Validation
? The appearance diagrams and product renderings in this document are for reference only; the actual product shall prevail.
? Data regarding improvements in flexural strength and torsional stiffness are derived from comparative testing between the VZ Series propeller and the G Series propellers.
? Data regarding the reduction in bolt shear load is sourced from simulation comparisons between the installation bolts for the VZ Series propellers and those for the V Series propellers.
? The test data presented above were obtained under specific conditions, using equipment within our company's laboratory. Actual data and parameters may vary slightly depending on the test environment, platform, software, and other factors.
Technical Drawing
Specification Export to Excel
Diameter (Inch)
16(381.0mm)
Material
Resin-basedCarbonFiberComposite+PMIFoamCore
Pitch (Inch)
6.5(165.1mm)
Surface Treatment
Matte
AverageSingleblade Weight (g)
30
Type
One-Piece Straight Propeller
RecommendedMax RPM (RPM)
10200
Application
VTOL Fixed-Wing UAVs, Multicopter Mode
RecommendedMax Thrust (kg)
8
Connections & Dimensions
Flange Mount, Ø4 mm Center Hole, Ø12 mm Bolt Circle, with 2x Ø3 mm Mounting Holes
Limit RPM (RPM)
11500
Recommendations
Recommended Solution：V505 KV260+FLAME 60A
Limit Thrust (kg)
10
Test Data Export to Excel
Ambient Temperature 22 °C Altitude 25 m
RPM (RPM)
Torque （N·m)
RecommendedThrust （gf）
Output Power （W）
力Effciency （gf/W）
vz16x6.5-draw.png
4500.00
0.31
1456
146.62
9.93
5000.00
0.38
1799
200.58
8.97
5500.00
0.46
2190
267.46
8.19
6000.00
0.56
2629
348.73
7.54
6500.00
0.66
3117
445.87
6.99
7000.00
0.76
3652
560.34
6.52
7500.00
0.88
4235
693.61
6.11
8000.00
1.01
4866
847.16
5.74
8500.00
1.15
5545
1022.44
5.42
9000.00
1.30
6273
1220.94
5.14
9500.00
1.45
7048
1444.13
4.88
10000.00
1.62
7871
1693.46
4.65
10500.00
1.79
8743
1970.42
4.44
11000.00
1.98
9662
2276.47
4.24
11500.00
2.17
10629
2613.08
4.07
Important Notes
Data may vary under different testing standards due to factors such as equipment, methodology, and environment. Ensure compatibility between the propeller mounting holes and motors. Refer to the drawing above for details.
Packing List
T-Motor VZ18x7 VTOL 18 Zoll Carbon Propeller 1x CW 1x CCW
Artikelnr.: PM-7259 | HAN: VZ18x7
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VZ SERIES -VTOL PROPELLERS
Break through the performance limitations of traditional multi-rotor propellers. VZ series propellers deliver superior power, durability, and lightweight design for VTOL applications
What Does a VTOL Propeller Need?
High Strength High Stiffness & Lightweight Design
High Strength
Withstands immense centrifugal loads and maneuver-induced alternating loads at high RPM, preventing structural failure
High Stiffness
Ensures safe blade-tip clearance in compact layouts, suppresses aeroelastic deformation, and prevents flutter
Lightweight Design
Reduce the moment of inertia to achieve rapid thrust response and higher attitude control bandwidth for the flight control system
Superior Aerodynamic Design
The unique dual operational modes of VTOL—vertical takeoff/landing and cruise—demand new propeller capabilities
Vertical Takeoff & Landing Phase
Requiring high thrust and power, demanding maximum lift output from the propeller disk within a limited blade area
Cruise Phase
When the propeller stops rotating, it is necessary to minimize profile drag to reduce power consumption, achieving "stealthy" low-drag efficiency
Transition Stability: Resisting Complex Flow Field Interference
The extreme challenges posed by high angle of attack, low speed and unsteady flow field, coupled with the insufficient strength and poor transition stability of traditional blades, make this an accident-prone region
Unsteady Flow Fields at High Angle of Attack
The aircraft operates at high angles of attack and low speeds within an extremely complex flow environment
Asymmetric Airflow
Significant angle between incoming flow and the rotation axis causes asymmetric airflow entering the propeller disc
Severe Periodic Variations
Local forces on the blade fluctuate drastically per rotation, inducing flutter and causing significant thrust fluctuation
To address the challenges of traditional propellers in VTOL (Vertical Takeoff and Landing mode) applications
we introduce the VZ Series Propellers
Technical Features of the VZ Series Propellers
Advanced composite materials and exceptional aerodynamic design work in synergy to ensure consistently efficient, reliable, and controllable power output
Bending & Torsion Resistant Layup Design
Optimized fiber orientation and ratio maximize strength and stiffness
Prepreg Compression Molding for Integrated Forming
Product porosity below 1%, ensuring stable and reliable quality
PMI Foam Core
Lightweight, high-strength core material effectively increases stiffness while controlling total weight
30%
Flexural Strength
Significantly enhanced impact resistance and deformation resistance for greater durability in complex operating conditions
20%
Torsional Stiffness
Optimized power transmission efficiency reduces energy loss during operation
Blade Root Optimization: Safety Redundancy Design
The blade root thickness is optimized to provide structural redundancy while reducing loads on the connecting bolts
V30 Propeller
VZ30 Propeller
Aerodynamic Priority: Engineered for High VTOL Thrust
Dedicated High Lift-to- Drag Ratio Airfoil
Optimized for VTOL conditions to enhance maximum lift coefficient
Low-Drag Cruise Blade Shape
Improved aerodynamic blade boundaries reduce cruise drag
Specialized Blade Tip
Optimized tip design weakens vortex strength and enhances flight quality
Custom VTOL Propeller Service: 10 to 100 Inches
Supports precise matching with various pitch specifications and motors Full in-house R&D ensures stable and controllable quality
Aerodynamic/Structural Design
Mold Manufacturing
Composite Molding
Testing & Validation
? The appearance diagrams and product renderings in this document are for reference only; the actual product shall prevail.
? Data regarding improvements in flexural strength and torsional stiffness are derived from comparative testing between the VZ Series propeller and the G Series propellers.
? Data regarding the reduction in bolt shear load is sourced from simulation comparisons between the installation bolts for the VZ Series propellers and those for the V Series propellers.
? The test data presented above were obtained under specific conditions, using equipment within our company's laboratory. Actual data and parameters may vary slightly depending on the test environment, platform, software, and other factors.
Technical Drawing
Specification Export to Excel
Diameter (Inch)
18(457.2mm)
Material
Resin-basedCarbonFiberComposite+PMIFoamCore
Pitch (Inch)
7(177.8mm)
Surface Treatment
Matte
AverageSingleblade Weight (g)
31
Type
One-Piece Straight Propeller
RecommendedMax RPM (RPM)
8800
Application
VTOL Fixed-Wing UAVs, Multicopter Mode
RecommendedMax Thrust (kg)
9.6
Connections & Dimensions
Flange Mount, Ø6 mm Center Hole, Ø12 mm Bolt Circle, with 2x Ø3 mm Mounting Holes
Limit RPM (RPM)
10000
Recommendations
Limit Thrust (kg)
12
Test Data Export to Excel
Ambient Temperature 22 °C Altitude 25 m
RPM (RPM)
Torque （N·m)
RecommendedThrust （gf）
Output Power （W）
力Effciency （gf/W）
vz18x7-draw.png
3000
0.23
1034
72.54
14.26
3500
0.31
1399
112.84
12.40
4000
0.40
1835
167.72
10.94
4500
0.51
2341
239.60
9.77
5000
0.63
2917
330.94
8.81
5500
0.77
3563
444.17
8.02
6000
0.93
4280
581.72
7.36
6500
1.10
5067
746.06
6.79
7000
1.28
5925
939.60
6.31
7500
1.48
6852
1164.80
5.88
8000
1.70
7850
1424.09
5.51
8500
1.93
8919
1719.91
5.19
9000
2.18
10057
2054.71
4.89
9500
2.44
11266
2430.93
4.63
10000
2.72
12546
2851.00
4.40
Important Notes
Data may vary under different testing standards due to factors such as equipment, methodology, and environment. Ensure compatibility between the propeller mounting holes and motors. Refer to the drawing above for details.
Packing List
T-Motor VZ20x8.2 VTOL 20 Zoll Carbon Propeller 1x CW 1x CCW
Artikelnr.: PM-7260 | HAN: VZ20x8.2
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transform: none !important; transition: none !important; } .scaleInit { opacity: 1 !important; transform: none !important; transition: none !important; } #parameter { display: block !important; padding: 20px 5%; background: #fff; color: #333; } #parameter .mainBox { margin-bottom: 30px; } #parameter .tableTitle { font-size: 20px; font-weight: bold; padding: 15px 0; border-bottom: 2px solid #333; } #parameter table { width: 100%; border-collapse: collapse; margin: 10px 0; } #parameter td, #parameter th { border: 1px solid #ddd; padding: 8px; font-size: 14px; } #parameter img { max-width: 100%; height: auto; }
VZ SERIES -VTOL PROPELLERS
Break through the performance limitations of traditional multi-rotor propellers. VZ series propellers deliver superior power, durability, and lightweight design for VTOL applications
What Does a VTOL Propeller Need?
High Strength High Stiffness & Lightweight Design
High Strength
Withstands immense centrifugal loads and maneuver-induced alternating loads at high RPM, preventing structural failure
High Stiffness
Ensures safe blade-tip clearance in compact layouts, suppresses aeroelastic deformation, and prevents flutter
Lightweight Design
Reduce the moment of inertia to achieve rapid thrust response and higher attitude control bandwidth for the flight control system
Superior Aerodynamic Design
The unique dual operational modes of VTOL—vertical takeoff/landing and cruise—demand new propeller capabilities
Vertical Takeoff & Landing Phase
Requiring high thrust and power, demanding maximum lift output from the propeller disk within a limited blade area
Cruise Phase
When the propeller stops rotating, it is necessary to minimize profile drag to reduce power consumption, achieving "stealthy" low-drag efficiency
Transition Stability: Resisting Complex Flow Field Interference
The extreme challenges posed by high angle of attack, low speed and unsteady flow field, coupled with the insufficient strength and poor transition stability of traditional blades, make this an accident-prone region
Unsteady Flow Fields at High Angle of Attack
The aircraft operates at high angles of attack and low speeds within an extremely complex flow environment
Asymmetric Airflow
Significant angle between incoming flow and the rotation axis causes asymmetric airflow entering the propeller disc
Severe Periodic Variations
Local forces on the blade fluctuate drastically per rotation, inducing flutter and causing significant thrust fluctuation
To address the challenges of traditional propellers in VTOL (Vertical Takeoff and Landing mode) applications
we introduce the VZ Series Propellers
Technical Features of the VZ Series Propellers
Advanced composite materials and exceptional aerodynamic design work in synergy to ensure consistently efficient, reliable, and controllable power output
Bending & Torsion Resistant Layup Design
Optimized fiber orientation and ratio maximize strength and stiffness
Prepreg Compression Molding for Integrated Forming
Product porosity below 1%, ensuring stable and reliable quality
PMI Foam Core
Lightweight, high-strength core material effectively increases stiffness while controlling total weight
30%
Flexural Strength
Significantly enhanced impact resistance and deformation resistance for greater durability in complex operating conditions
20%
Torsional Stiffness
Optimized power transmission efficiency reduces energy loss during operation
Blade Root Optimization: Safety Redundancy Design
The blade root thickness is optimized to provide structural redundancy while reducing loads on the connecting bolts
V30 Propeller
VZ30 Propeller
Aerodynamic Priority: Engineered for High VTOL Thrust
Dedicated High Lift-to- Drag Ratio Airfoil
Optimized for VTOL conditions to enhance maximum lift coefficient
Low-Drag Cruise Blade Shape
Improved aerodynamic blade boundaries reduce cruise drag
Specialized Blade Tip
Optimized tip design weakens vortex strength and enhances flight quality
Custom VTOL Propeller Service: 10 to 100 Inches
Supports precise matching with various pitch specifications and motors Full in-house R&D ensures stable and controllable quality
Aerodynamic/Structural Design
Mold Manufacturing
Composite Molding
Testing & Validation
? The appearance diagrams and product renderings in this document are for reference only; the actual product shall prevail.
? Data regarding improvements in flexural strength and torsional stiffness are derived from comparative testing between the VZ Series propeller and the G Series propellers.
? Data regarding the reduction in bolt shear load is sourced from simulation comparisons between the installation bolts for the VZ Series propellers and those for the V Series propellers.
? The test data presented above were obtained under specific conditions, using equipment within our company's laboratory. Actual data and parameters may vary slightly depending on the test environment, platform, software, and other factors.
Technical Drawing
Specification Export to Excel
Diameter (Inch)
20(508mm)
Material
Resin-basedCarbonFiberComposite+PMIFoamCore
Pitch (Inch)
8.2(208.3mm)
Surface Treatment
Matte
AverageSingleblade Weight (g)
38
Type
One-Piece Straight Propeller
RecommendedMax RPM (RPM)
7300
Application
VTOL Fixed-Wing UAVs, Multicopter Mode
RecommendedMax Thrust (kg)
11.2
Connections & Dimensions
Flange Mount, Ø6 mm Center Hole, Ø12 mm Bolt Circle, with 2x Ø3 mm Mounting Holes
Limit RPM (RPM)
8000
Recommendations
Limit Thrust (kg)
14
Test Data Export to Excel
Ambient Temperature 22 °C Altitude 25 m
RPM (RPM)
Torque （N·m)
RecommendedThrust （gf）
Output Power （W）
力Effciency （gf/W）
vz20x8.2-draw.png
3800
0.71
2942
281.95
10.43
4100
0.83
3447
356.32
9.67
4400
0.96
3998
443.54
9.01
4700
1.11
4594
544.68
8.43
5000
1.26
5236
660.79
7.92
5300
1.43
5922
792.95
7.47
5600
1.61
6654
942.22
7.06
5900
1.80
7432
1109.67
6.70
6200
2.00
8254
1296.37
6.37
6500
2.21
9122
1503.39
6.07
6800
2.43
10035
1731.78
5.79
7100
2.67
10994
1982.63
5.54
7400
2.91
11997
2257.00
5.32
7700
3.17
13046
2555.95
5.10
8000
3.44
14141
2880.55
4.91
Important Notes
Data may vary under different testing standards due to factors such as equipment, methodology, and environment. Ensure compatibility between the propeller mounting holes and motors. Refer to the drawing above for details.
Packing List
T-Motor VZ22x7.4 VTOL 22 Zoll Carbon Propeller 1x CW 1x CCW
Artikelnr.: PM-7261 | HAN: VZ22x7.4
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VZ SERIES -VTOL PROPELLERS
Break through the performance limitations of traditional multi-rotor propellers. VZ series propellers deliver superior power, durability, and lightweight design for VTOL applications
What Does a VTOL Propeller Need?
High Strength High Stiffness & Lightweight Design
High Strength
Withstands immense centrifugal loads and maneuver-induced alternating loads at high RPM, preventing structural failure
High Stiffness
Ensures safe blade-tip clearance in compact layouts, suppresses aeroelastic deformation, and prevents flutter
Lightweight Design
Reduce the moment of inertia to achieve rapid thrust response and higher attitude control bandwidth for the flight control system
Superior Aerodynamic Design
The unique dual operational modes of VTOL—vertical takeoff/landing and cruise—demand new propeller capabilities
Vertical Takeoff & Landing Phase
Requiring high thrust and power, demanding maximum lift output from the propeller disk within a limited blade area
Cruise Phase
When the propeller stops rotating, it is necessary to minimize profile drag to reduce power consumption, achieving "stealthy" low-drag efficiency
Transition Stability: Resisting Complex Flow Field Interference
The extreme challenges posed by high angle of attack, low speed and unsteady flow field, coupled with the insufficient strength and poor transition stability of traditional blades, make this an accident-prone region
Unsteady Flow Fields at High Angle of Attack
The aircraft operates at high angles of attack and low speeds within an extremely complex flow environment
Asymmetric Airflow
Significant angle between incoming flow and the rotation axis causes asymmetric airflow entering the propeller disc
Severe Periodic Variations
Local forces on the blade fluctuate drastically per rotation, inducing flutter and causing significant thrust fluctuation
To address the challenges of traditional propellers in VTOL (Vertical Takeoff and Landing mode) applications
we introduce the VZ Series Propellers
Technical Features of the VZ Series Propellers
Advanced composite materials and exceptional aerodynamic design work in synergy to ensure consistently efficient, reliable, and controllable power output
Bending & Torsion Resistant Layup Design
Optimized fiber orientation and ratio maximize strength and stiffness
Prepreg Compression Molding for Integrated Forming
Product porosity below 1%, ensuring stable and reliable quality
PMI Foam Core
Lightweight, high-strength core material effectively increases stiffness while controlling total weight
30%
Flexural Strength
Significantly enhanced impact resistance and deformation resistance for greater durability in complex operating conditions
20%
Torsional Stiffness
Optimized power transmission efficiency reduces energy loss during operation
Blade Root Optimization: Safety Redundancy Design
The blade root thickness is optimized to provide structural redundancy while reducing loads on the connecting bolts
V30 Propeller
VZ30 Propeller
Aerodynamic Priority: Engineered for High VTOL Thrust
Dedicated High Lift-to- Drag Ratio Airfoil
Optimized for VTOL conditions to enhance maximum lift coefficient
Low-Drag Cruise Blade Shape
Improved aerodynamic blade boundaries reduce cruise drag
Specialized Blade Tip
Optimized tip design weakens vortex strength and enhances flight quality
Custom VTOL Propeller Service: 10 to 100 Inches
Supports precise matching with various pitch specifications and motors Full in-house R&D ensures stable and controllable quality
Aerodynamic/Structural Design
Mold Manufacturing
Composite Molding
Testing & Validation
? The appearance diagrams and product renderings in this document are for reference only; the actual product shall prevail.
? Data regarding improvements in flexural strength and torsional stiffness are derived from comparative testing between the VZ Series propeller and the G Series propellers.
? Data regarding the reduction in bolt shear load is sourced from simulation comparisons between the installation bolts for the VZ Series propellers and those for the V Series propellers.
? The test data presented above were obtained under specific conditions, using equipment within our company's laboratory. Actual data and parameters may vary slightly depending on the test environment, platform, software, and other factors.
Technical Drawing
Specification Export to Excel
Diameter (Inch)
22(558.8mm)
Material
Resin-basedCarbonFiberComposite+PMIFoamCore
Pitch (Inch)
7.4(188.0mm)
Surface Treatment
Matte
AverageSingleblade Weight (g)
43
Type
One-Piece Straight Propeller
RecommendedMax RPM (RPM)
7350
Application
VTOL Fixed-Wing UAVs, Multicopter Mode
RecommendedMax Thrust (kg)
14.4
Connections & Dimensions
Flange Mount, Ø6 mm Center Hole, Ø12 mm Bolt Circle, with 2x Ø3 mm Mounting Holes
Limit RPM (RPM)
8200
Recommendations
Recommended Solution：V605 KV210+FLAME 80A 12S V2.0/VL6011 KV180+V60A/VL6013 KV210+V80A
Limit Thrust (kg)
18
Test Data Export to Excel
Ambient Temperature 22 °C Altitude 25 m
RPM (RPM)
Torque （N·m)
RecommendedThrust （gf）
Output Power （W）
力Effciency （gf/W）
vz22x7.4-draw.png
4000
0.946
3901
396.21
9.85
4300
1.103
4553
496.87
9.16
4600
1.276
5261
614.73
8.56
4900
1.464
6027
751.23
8.02
5200
1.667
6850
907.78
7.55
5500
1.885
7731
1085.83
7.12
5800
2.119
8668
1286.79
6.74
6100
2.367
9662
1512.10
6.39
6400
2.631
10714
1763.18
6.08
6700
2.910
11822
2041.47
5.79
7000
3.204
12988
2348.40
5.53
7300
3.513
14211
2685.39
5.29
7600
3.837
15491
3053.87
5.07
7900
4.177
16828
3455.27
4.87
8200
4.531
18222
3891.02
4.68
Important Notes
Data may vary under different testing standards due to factors such as equipment, methodology, and environment. Ensure compatibility between the propeller mounting holes and motors. Refer to the drawing above for details.
Packing List
T-Motor VZ24x.8.2 VTOL 24 Zoll Carbon Propeller 1x CW 1x CCW
Artikelnr.: PM-7262 | HAN: VZ24x.8.2
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VZ SERIES -VTOL PROPELLERS
Break through the performance limitations of traditional multi-rotor propellers. VZ series propellers deliver superior power, durability, and lightweight design for VTOL applications
What Does a VTOL Propeller Need?
High Strength High Stiffness & Lightweight Design
High Strength
Withstands immense centrifugal loads and maneuver-induced alternating loads at high RPM, preventing structural failure
High Stiffness
Ensures safe blade-tip clearance in compact layouts, suppresses aeroelastic deformation, and prevents flutter
Lightweight Design
Reduce the moment of inertia to achieve rapid thrust response and higher attitude control bandwidth for the flight control system
Superior Aerodynamic Design
The unique dual operational modes of VTOL—vertical takeoff/landing and cruise—demand new propeller capabilities
Vertical Takeoff & Landing Phase
Requiring high thrust and power, demanding maximum lift output from the propeller disk within a limited blade area
Cruise Phase
When the propeller stops rotating, it is necessary to minimize profile drag to reduce power consumption, achieving "stealthy" low-drag efficiency
Transition Stability: Resisting Complex Flow Field Interference
The extreme challenges posed by high angle of attack, low speed and unsteady flow field, coupled with the insufficient strength and poor transition stability of traditional blades, make this an accident-prone region
Unsteady Flow Fields at High Angle of Attack
The aircraft operates at high angles of attack and low speeds within an extremely complex flow environment
Asymmetric Airflow
Significant angle between incoming flow and the rotation axis causes asymmetric airflow entering the propeller disc
Severe Periodic Variations
Local forces on the blade fluctuate drastically per rotation, inducing flutter and causing significant thrust fluctuation
To address the challenges of traditional propellers in VTOL (Vertical Takeoff and Landing mode) applications
we introduce the VZ Series Propellers
Technical Features of the VZ Series Propellers
Advanced composite materials and exceptional aerodynamic design work in synergy to ensure consistently efficient, reliable, and controllable power output
Bending & Torsion Resistant Layup Design
Optimized fiber orientation and ratio maximize strength and stiffness
Prepreg Compression Molding for Integrated Forming
Product porosity below 1%, ensuring stable and reliable quality
PMI Foam Core
Lightweight, high-strength core material effectively increases stiffness while controlling total weight
30%
Flexural Strength
Significantly enhanced impact resistance and deformation resistance for greater durability in complex operating conditions
20%
Torsional Stiffness
Optimized power transmission efficiency reduces energy loss during operation
Blade Root Optimization: Safety Redundancy Design
The blade root thickness is optimized to provide structural redundancy while reducing loads on the connecting bolts
V30 Propeller
VZ30 Propeller
Aerodynamic Priority: Engineered for High VTOL Thrust
Dedicated High Lift-to- Drag Ratio Airfoil
Optimized for VTOL conditions to enhance maximum lift coefficient
Low-Drag Cruise Blade Shape
Improved aerodynamic blade boundaries reduce cruise drag
Specialized Blade Tip
Optimized tip design weakens vortex strength and enhances flight quality
Custom VTOL Propeller Service: 10 to 100 Inches
Supports precise matching with various pitch specifications and motors Full in-house R&D ensures stable and controllable quality
Aerodynamic/Structural Design
Mold Manufacturing
Composite Molding
Testing & Validation
? The appearance diagrams and product renderings in this document are for reference only; the actual product shall prevail.
? Data regarding improvements in flexural strength and torsional stiffness are derived from comparative testing between the VZ Series propeller and the G Series propellers.
? Data regarding the reduction in bolt shear load is sourced from simulation comparisons between the installation bolts for the VZ Series propellers and those for the V Series propellers.
? The test data presented above were obtained under specific conditions, using equipment within our company's laboratory. Actual data and parameters may vary slightly depending on the test environment, platform, software, and other factors.
Technical Drawing
Specification Export to Excel
Diameter (Inch)
24(609.6mm)
Material
Resin-basedCarbonFiberComposite+PMIFoamCore
Pitch (Inch)
8.2(208.3mm)
Surface Treatment
Matte
AverageSingleblade Weight (g)
54
Type
One-Piece Straight Propeller
RecommendedMax RPM (RPM)
6800
Application
VTOL Fixed-Wing UAVs, Multicopter Mode
RecommendedMax Thrust (kg)
16.8
Connections & Dimensions
Flange Mount, Ø10 mm Center Hole,Ø18mm and Ø20mm Bolt Cirde, with 6x Ø3 mm Mounting Holes
Limit RPM (RPM)
7600
Recommendations
Recommended Solution：VL7015+KV190+V80A
Limit Thrust (kg)
21
Test Data Export to Excel
Ambient Temperature 22 °C Altitude 25 m
RPM (RPM)
Torque （N·m)
RecommendedThrust （gf）
Output Power （W）
力Effciency （gf/W）
vz24x8.2-draw.png
2000
0.43
1434
89.31
16.05
2400
0.54
1940
135.85
14.28
2800
0.70
2588
204.08
12.68
3200
0.89
3379
299.21
11.29
3600
1.13
4311
426.42
10.11
4000
1.41
5386
590.91
9.11
4400
1.73
6602
797.90
8.27
4800
2.09
7961
1052.57
7.56
5200
2.50
9462
1360.12
6.96
5600
2.94
11105
1725.76
6.43
6000
3.43
12890
2154.67
5.98
6400
3.96
14817
2652.07
5.59
6800
4.53
16887
3223.15
5.24
7200
5.14
19098
3873.11
4.93
7600
5.79
21452
4607.15
4.66
Important Notes
Data may vary under different testing standards due to factors such as equipment, methodology, and environment. Ensure compatibility between the propeller mounting holes and motors. Refer to the drawing above for details.
Packing List
T-Motor VZ26x9.5 VTOL 26 Zoll Carbon Propeller 1x CW 1x CCW
Artikelnr.: PM-7263 | HAN: VZ26x9.5
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VZ SERIES -VTOL PROPELLERS
Break through the performance limitations of traditional multi-rotor propellers. VZ series propellers deliver superior power, durability, and lightweight design for VTOL applications
What Does a VTOL Propeller Need?
High Strength High Stiffness & Lightweight Design
High Strength
Withstands immense centrifugal loads and maneuver-induced alternating loads at high RPM, preventing structural failure
High Stiffness
Ensures safe blade-tip clearance in compact layouts, suppresses aeroelastic deformation, and prevents flutter
Lightweight Design
Reduce the moment of inertia to achieve rapid thrust response and higher attitude control bandwidth for the flight control system
Superior Aerodynamic Design
The unique dual operational modes of VTOL—vertical takeoff/landing and cruise—demand new propeller capabilities
Vertical Takeoff & Landing Phase
Requiring high thrust and power, demanding maximum lift output from the propeller disk within a limited blade area
Cruise Phase
When the propeller stops rotating, it is necessary to minimize profile drag to reduce power consumption, achieving "stealthy" low-drag efficiency
Transition Stability: Resisting Complex Flow Field Interference
The extreme challenges posed by high angle of attack, low speed and unsteady flow field, coupled with the insufficient strength and poor transition stability of traditional blades, make this an accident-prone region
Unsteady Flow Fields at High Angle of Attack
The aircraft operates at high angles of attack and low speeds within an extremely complex flow environment
Asymmetric Airflow
Significant angle between incoming flow and the rotation axis causes asymmetric airflow entering the propeller disc
Severe Periodic Variations
Local forces on the blade fluctuate drastically per rotation, inducing flutter and causing significant thrust fluctuation
To address the challenges of traditional propellers in VTOL (Vertical Takeoff and Landing mode) applications
we introduce the VZ Series Propellers
Technical Features of the VZ Series Propellers
Advanced composite materials and exceptional aerodynamic design work in synergy to ensure consistently efficient, reliable, and controllable power output
Bending & Torsion Resistant Layup Design
Optimized fiber orientation and ratio maximize strength and stiffness
Prepreg Compression Molding for Integrated Forming
Product porosity below 1%, ensuring stable and reliable quality
PMI Foam Core
Lightweight, high-strength core material effectively increases stiffness while controlling total weight
30%
Flexural Strength
Significantly enhanced impact resistance and deformation resistance for greater durability in complex operating conditions
20%
Torsional Stiffness
Optimized power transmission efficiency reduces energy loss during operation
Blade Root Optimization: Safety Redundancy Design
The blade root thickness is optimized to provide structural redundancy while reducing loads on the connecting bolts
V30 Propeller
VZ30 Propeller
Aerodynamic Priority: Engineered for High VTOL Thrust
Dedicated High Lift-to- Drag Ratio Airfoil
Optimized for VTOL conditions to enhance maximum lift coefficient
Low-Drag Cruise Blade Shape
Improved aerodynamic blade boundaries reduce cruise drag
Specialized Blade Tip
Optimized tip design weakens vortex strength and enhances flight quality
Custom VTOL Propeller Service: 10 to 100 Inches
Supports precise matching with various pitch specifications and motors Full in-house R&D ensures stable and controllable quality
Aerodynamic/Structural Design
Mold Manufacturing
Composite Molding
Testing & Validation
? The appearance diagrams and product renderings in this document are for reference only; the actual product shall prevail.
? Data regarding improvements in flexural strength and torsional stiffness are derived from comparative testing between the VZ Series propeller and the G Series propellers.
? Data regarding the reduction in bolt shear load is sourced from simulation comparisons between the installation bolts for the VZ Series propellers and those for the V Series propellers.
? The test data presented above were obtained under specific conditions, using equipment within our company's laboratory. Actual data and parameters may vary slightly depending on the test environment, platform, software, and other factors.
Technical Drawing
Specification Export to Excel
Diameter (Inch)
26(660.4mm)
Material
Resin-basedCarbonFiberComposite+PMIFoamCore
Pitch (Inch)
9.5(241.3mm)
Surface Treatment
Matte
AverageSingleblade Weight (g)
68
Type
One-Piece Straight Propeller
RecommendedMax RPM (RPM)
5900
Application
VTOL Fixed-Wing UAVs, Multicopter Mode
RecommendedMax Thrust (kg)
20
Connections & Dimensions
Flange Mount, Ø10 mm Center Hole, Ø20 mm Bolt Circle, with 4x Ø3 mm Mounting Holes
Limit RPM (RPM)
6500
Recommendations
Recommended Solution：VL8015+KV170+V80A/VL8018+KV180+V120A
Limit Thrust (kg)
25
Test Data Export to Excel
Ambient Temperature 22 °C Altitude 25 m
RPM (RPM)
Torque （N·m)
RecommendedThrust （gf）
Output Power （W）
力Effciency （gf/W）
vz26x9.5-draw.png
1100
0.39
884
45.34
19.49
1500
0.50
1305
78.00
16.72
1900
0.67
1946
133.79
14.54
2300
0.92
2808
221.85
12.66
2700
1.24
3891
351.35
11.07
3100
1.64
5194
531.43
9.77
3500
2.10
6718
771.27
8.71
3900
2.64
8462
1080.00
7.84
4300
3.26
10427
1466.79
7.11
4700
3.94
12613
1940.79
6.50
5100
4.70
15019
2511.16
5.98
5500
5.53
17646
3187.05
5.54
5900
6.44
20494
3977.63
5.15
6300
7.42
23562
4892.04
4.82
6500
7.93
25179
5398.54
4.66
Important Notes
Data may vary under different testing standards due to factors such as equipment, methodology, and environment. Ensure compatibility between the propeller mounting holes and motors. Refer to the drawing above for details.
Packing List
T-Motor VZ27x11 VTOL 27 Zoll Carbon Propeller 1x CW 1x CCW
Artikelnr.: PM-7264 | HAN: VZ27x11
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VZ SERIES -VTOL PROPELLERS
Break through the performance limitations of traditional multi-rotor propellers. VZ series propellers deliver superior power, durability, and lightweight design for VTOL applications
What Does a VTOL Propeller Need?
High Strength High Stiffness & Lightweight Design
High Strength
Withstands immense centrifugal loads and maneuver-induced alternating loads at high RPM, preventing structural failure
High Stiffness
Ensures safe blade-tip clearance in compact layouts, suppresses aeroelastic deformation, and prevents flutter
Lightweight Design
Reduce the moment of inertia to achieve rapid thrust response and higher attitude control bandwidth for the flight control system
Superior Aerodynamic Design
The unique dual operational modes of VTOL—vertical takeoff/landing and cruise—demand new propeller capabilities
Vertical Takeoff & Landing Phase
Requiring high thrust and power, demanding maximum lift output from the propeller disk within a limited blade area
Cruise Phase
When the propeller stops rotating, it is necessary to minimize profile drag to reduce power consumption, achieving "stealthy" low-drag efficiency
Transition Stability: Resisting Complex Flow Field Interference
The extreme challenges posed by high angle of attack, low speed and unsteady flow field, coupled with the insufficient strength and poor transition stability of traditional blades, make this an accident-prone region
Unsteady Flow Fields at High Angle of Attack
The aircraft operates at high angles of attack and low speeds within an extremely complex flow environment
Asymmetric Airflow
Significant angle between incoming flow and the rotation axis causes asymmetric airflow entering the propeller disc
Severe Periodic Variations
Local forces on the blade fluctuate drastically per rotation, inducing flutter and causing significant thrust fluctuation
To address the challenges of traditional propellers in VTOL (Vertical Takeoff and Landing mode) applications
we introduce the VZ Series Propellers
Technical Features of the VZ Series Propellers
Advanced composite materials and exceptional aerodynamic design work in synergy to ensure consistently efficient, reliable, and controllable power output
Bending & Torsion Resistant Layup Design
Optimized fiber orientation and ratio maximize strength and stiffness
Prepreg Compression Molding for Integrated Forming
Product porosity below 1%, ensuring stable and reliable quality
PMI Foam Core
Lightweight, high-strength core material effectively increases stiffness while controlling total weight
30%
Flexural Strength
Significantly enhanced impact resistance and deformation resistance for greater durability in complex operating conditions
20%
Torsional Stiffness
Optimized power transmission efficiency reduces energy loss during operation
Blade Root Optimization: Safety Redundancy Design
The blade root thickness is optimized to provide structural redundancy while reducing loads on the connecting bolts
V30 Propeller
VZ30 Propeller
Aerodynamic Priority: Engineered for High VTOL Thrust
Dedicated High Lift-to- Drag Ratio Airfoil
Optimized for VTOL conditions to enhance maximum lift coefficient
Low-Drag Cruise Blade Shape
Improved aerodynamic blade boundaries reduce cruise drag
Specialized Blade Tip
Optimized tip design weakens vortex strength and enhances flight quality
Custom VTOL Propeller Service: 10 to 100 Inches
Supports precise matching with various pitch specifications and motors Full in-house R&D ensures stable and controllable quality
Aerodynamic/Structural Design
Mold Manufacturing
Composite Molding
Testing & Validation
? The appearance diagrams and product renderings in this document are for reference only; the actual product shall prevail.
? Data regarding improvements in flexural strength and torsional stiffness are derived from comparative testing between the VZ Series propeller and the G Series propellers.
? Data regarding the reduction in bolt shear load is sourced from simulation comparisons between the installation bolts for the VZ Series propellers and those for the V Series propellers.
? The test data presented above were obtained under specific conditions, using equipment within our company's laboratory. Actual data and parameters may vary slightly depending on the test environment, platform, software, and other factors.
Technical Drawing
Specification Export to Excel
Diameter (Inch)
27(685.8mm)
Material
Resin-basedCarbonFiberComposite+PMIFoamCore
Pitch (Inch)
11(279.4mm)
Surface Treatment
Matte
AverageSingleblade Weight (g)
75
Type
One-Piece Straight Propeller
RecommendedMax RPM (RPM)
6200
Application
VTOL Fixed-Wing UAVs, Multicopter Mode
RecommendedMax Thrust (kg)
22.4
Connections & Dimensions
Flange Mount, Ø10 mm Center Hole, Ø20 mm Bolt Circle, with 4x Ø3 mm Mounting Holes
Limit RPM (RPM)
6900
Recommendations
Limit Thrust (kg)
28
Test Data Export to Excel
Ambient Temperature 22 °C Altitude 25 m
RPM (RPM)
Torque （N·m)
RecommendedThrust （gf）
Output Power （W）
力Effciency （gf/W）
vz27x11-draw.png
1500
0.40
1254
62.93
19.92
1900
0.62
1988
123.00
16.16
2300
0.90
2926
216.59
13.51
2700
1.24
4068
351.66
11.57
3100
1.65
5415
536.20
10.10
3500
2.12
6966
778.17
8.95
3900
2.66
8720
1085.55
8.03
4300
3.26
10680
1466.31
7.28
4700
3.92
12843
1928.44
6.66
5100
4.64
15211
2479.89
6.13
5500
5.43
17783
3128.65
5.68
5900
6.28
20559
3882.70
5.29
6300
7.20
23539
4749.99
4.96
6700
8.18
26723
5738.52
4.66
6900
8.69
28392
6280.74
4.52
Important Notes
Data may vary under different testing standards due to factors such as equipment, methodology, and environment. Ensure compatibility between the propeller mounting holes and motors. Refer to the drawing above for details.
Packing List
T-Motor VZ28x10.8 VTOL 28 Zoll Carbon Propeller 1x CW 1x CCW
Artikelnr.: PM-7265 | HAN: VZ28x10.8
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transform: none !important; transition: none !important; } .scaleInit { opacity: 1 !important; transform: none !important; transition: none !important; } #parameter { display: block !important; padding: 20px 5%; background: #fff; color: #333; } #parameter .mainBox { margin-bottom: 30px; } #parameter .tableTitle { font-size: 20px; font-weight: bold; padding: 15px 0; border-bottom: 2px solid #333; } #parameter table { width: 100%; border-collapse: collapse; margin: 10px 0; } #parameter td, #parameter th { border: 1px solid #ddd; padding: 8px; font-size: 14px; } #parameter img { max-width: 100%; height: auto; }
VZ SERIES -VTOL PROPELLERS
Break through the performance limitations of traditional multi-rotor propellers. VZ series propellers deliver superior power, durability, and lightweight design for VTOL applications
What Does a VTOL Propeller Need?
High Strength High Stiffness & Lightweight Design
High Strength
Withstands immense centrifugal loads and maneuver-induced alternating loads at high RPM, preventing structural failure
High Stiffness
Ensures safe blade-tip clearance in compact layouts, suppresses aeroelastic deformation, and prevents flutter
Lightweight Design
Reduce the moment of inertia to achieve rapid thrust response and higher attitude control bandwidth for the flight control system
Superior Aerodynamic Design
The unique dual operational modes of VTOL—vertical takeoff/landing and cruise—demand new propeller capabilities
Vertical Takeoff & Landing Phase
Requiring high thrust and power, demanding maximum lift output from the propeller disk within a limited blade area
Cruise Phase
When the propeller stops rotating, it is necessary to minimize profile drag to reduce power consumption, achieving "stealthy" low-drag efficiency
Transition Stability: Resisting Complex Flow Field Interference
The extreme challenges posed by high angle of attack, low speed and unsteady flow field, coupled with the insufficient strength and poor transition stability of traditional blades, make this an accident-prone region
Unsteady Flow Fields at High Angle of Attack
The aircraft operates at high angles of attack and low speeds within an extremely complex flow environment
Asymmetric Airflow
Significant angle between incoming flow and the rotation axis causes asymmetric airflow entering the propeller disc
Severe Periodic Variations
Local forces on the blade fluctuate drastically per rotation, inducing flutter and causing significant thrust fluctuation
To address the challenges of traditional propellers in VTOL (Vertical Takeoff and Landing mode) applications
we introduce the VZ Series Propellers
Technical Features of the VZ Series Propellers
Advanced composite materials and exceptional aerodynamic design work in synergy to ensure consistently efficient, reliable, and controllable power output
Bending & Torsion Resistant Layup Design
Optimized fiber orientation and ratio maximize strength and stiffness
Prepreg Compression Molding for Integrated Forming
Product porosity below 1%, ensuring stable and reliable quality
PMI Foam Core
Lightweight, high-strength core material effectively increases stiffness while controlling total weight
30%
Flexural Strength
Significantly enhanced impact resistance and deformation resistance for greater durability in complex operating conditions
20%
Torsional Stiffness
Optimized power transmission efficiency reduces energy loss during operation
Blade Root Optimization: Safety Redundancy Design
The blade root thickness is optimized to provide structural redundancy while reducing loads on the connecting bolts
V30 Propeller
VZ30 Propeller
Aerodynamic Priority: Engineered for High VTOL Thrust
Dedicated High Lift-to- Drag Ratio Airfoil
Optimized for VTOL conditions to enhance maximum lift coefficient
Low-Drag Cruise Blade Shape
Improved aerodynamic blade boundaries reduce cruise drag
Specialized Blade Tip
Optimized tip design weakens vortex strength and enhances flight quality
Custom VTOL Propeller Service: 10 to 100 Inches
Supports precise matching with various pitch specifications and motors Full in-house R&D ensures stable and controllable quality
Aerodynamic/Structural Design
Mold Manufacturing
Composite Molding
Testing & Validation
? The appearance diagrams and product renderings in this document are for reference only; the actual product shall prevail.
? Data regarding improvements in flexural strength and torsional stiffness are derived from comparative testing between the VZ Series propeller and the G Series propellers.
? Data regarding the reduction in bolt shear load is sourced from simulation comparisons between the installation bolts for the VZ Series propellers and those for the V Series propellers.
? The test data presented above were obtained under specific conditions, using equipment within our company's laboratory. Actual data and parameters may vary slightly depending on the test environment, platform, software, and other factors.
Technical Drawing
Specification Export to Excel
Diameter (Inch)
28(711.2mm)
Material
Resin-basedCarbonFiberComposite+PMIFoamCore
Pitch (Inch)
10.8(274.4mm)
Surface Treatment
Matte
AverageSingleblade Weight (g)
80
Type
One-Piece Straight Propeller
RecommendedMax RPM (RPM)
5900
Application
VTOL Fixed-Wing UAVs, Multicopter Mode
RecommendedMax Thrust (kg)
26.4
Connections & Dimensions
Flange Mount, Ø10 mm Center Hole, Ø20 mm Bolt Circle, with 4x Ø3 mm Mounting Holes
Limit RPM (RPM)
6600
Recommendations
Recommended Solution：VL8020 KV170+V150A
Limit Thrust (kg)
33
Test Data Export to Excel
Ambient Temperature 22 °C Altitude 25 m
RPM (RPM)
Torque （N·m)
RecommendedThrust （gf）
Output Power （W）
力Effciency （gf/W）
vz28x11-draw.png
1200
0.37
1057
46.77
22.59
1600
0.61
1808
102.59
17.63
2000
0.94
2823
196.83
14.34
2400
1.35
4101
340.48
12.04
2800
1.86
5642
544.53
10.36
3200
2.45
7447
819.97
9.08
3600
3.12
9514
1177.80
8.08
4000
3.89
11845
1628.98
7.27
4400
4.74
14440
2184.52
6.61
4800
5.68
17297
2855.40
6.06
5200
6.71
20418
3652.62
5.59
5600
7.82
23802
4587.15
5.19
6000
9.02
27449
5669.98
4.84
6400
10.31
31360
6912.12
4.54
6600
10.99
33414
7596.35
4.40
Important Notes
Data may vary under different testing standards due to factors such as equipment, methodology, and environment. Ensure compatibility between the propeller mounting holes and motors. Refer to the drawing above for details.
Packing List
T-Motor VZ29x11 VTOL 29 Zoll Carbon Propeller 1x CW 1x CCW
Artikelnr.: PM-7267 | HAN: VZ29x11
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VZ SERIES -VTOL PROPELLERS
Break through the performance limitations of traditional multi-rotor propellers. VZ series propellers deliver superior power, durability, and lightweight design for VTOL applications
What Does a VTOL Propeller Need?
High Strength High Stiffness & Lightweight Design
High Strength
Withstands immense centrifugal loads and maneuver-induced alternating loads at high RPM, preventing structural failure
High Stiffness
Ensures safe blade-tip clearance in compact layouts, suppresses aeroelastic deformation, and prevents flutter
Lightweight Design
Reduce the moment of inertia to achieve rapid thrust response and higher attitude control bandwidth for the flight control system
Superior Aerodynamic Design
The unique dual operational modes of VTOL—vertical takeoff/landing and cruise—demand new propeller capabilities
Vertical Takeoff & Landing Phase
Requiring high thrust and power, demanding maximum lift output from the propeller disk within a limited blade area
Cruise Phase
When the propeller stops rotating, it is necessary to minimize profile drag to reduce power consumption, achieving "stealthy" low-drag efficiency
Transition Stability: Resisting Complex Flow Field Interference
The extreme challenges posed by high angle of attack, low speed and unsteady flow field, coupled with the insufficient strength and poor transition stability of traditional blades, make this an accident-prone region
Unsteady Flow Fields at High Angle of Attack
The aircraft operates at high angles of attack and low speeds within an extremely complex flow environment
Asymmetric Airflow
Significant angle between incoming flow and the rotation axis causes asymmetric airflow entering the propeller disc
Severe Periodic Variations
Local forces on the blade fluctuate drastically per rotation, inducing flutter and causing significant thrust fluctuation
To address the challenges of traditional propellers in VTOL (Vertical Takeoff and Landing mode) applications
we introduce the VZ Series Propellers
Technical Features of the VZ Series Propellers
Advanced composite materials and exceptional aerodynamic design work in synergy to ensure consistently efficient, reliable, and controllable power output
Bending & Torsion Resistant Layup Design
Optimized fiber orientation and ratio maximize strength and stiffness
Prepreg Compression Molding for Integrated Forming
Product porosity below 1%, ensuring stable and reliable quality
PMI Foam Core
Lightweight, high-strength core material effectively increases stiffness while controlling total weight
30%
Flexural Strength
Significantly enhanced impact resistance and deformation resistance for greater durability in complex operating conditions
20%
Torsional Stiffness
Optimized power transmission efficiency reduces energy loss during operation
Blade Root Optimization: Safety Redundancy Design
The blade root thickness is optimized to provide structural redundancy while reducing loads on the connecting bolts
V30 Propeller
VZ30 Propeller
Aerodynamic Priority: Engineered for High VTOL Thrust
Dedicated High Lift-to- Drag Ratio Airfoil
Optimized for VTOL conditions to enhance maximum lift coefficient
Low-Drag Cruise Blade Shape
Improved aerodynamic blade boundaries reduce cruise drag
Specialized Blade Tip
Optimized tip design weakens vortex strength and enhances flight quality
Custom VTOL Propeller Service: 10 to 100 Inches
Supports precise matching with various pitch specifications and motors Full in-house R&D ensures stable and controllable quality
Aerodynamic/Structural Design
Mold Manufacturing
Composite Molding
Testing & Validation
? The appearance diagrams and product renderings in this document are for reference only; the actual product shall prevail.
? Data regarding improvements in flexural strength and torsional stiffness are derived from comparative testing between the VZ Series propeller and the G Series propellers.
? Data regarding the reduction in bolt shear load is sourced from simulation comparisons between the installation bolts for the VZ Series propellers and those for the V Series propellers.
? The test data presented above were obtained under specific conditions, using equipment within our company's laboratory. Actual data and parameters may vary slightly depending on the test environment, platform, software, and other factors.
Technical Drawing
Specification Export to Excel
Diameter (Inch)
29(736.6mm)
Material
Resin-basedCarbonFiberComposite+PMIFoamCore
Pitch (Inch)
11(279.4mm)
Surface Treatment
Matte
AverageSingleblade Weight (g)
89
Type
One-Piece Straight Propeller
RecommendedMax RPM (RPM)
5800
Application
VTOL Fixed-Wing UAVs, Multicopter Mode
RecommendedMax Thrust (kg)
28.8
Connections & Dimensions
Flange Mount, Ø10 mm Center Hole, Ø20 mm Bolt Circle, with 4x Ø3 mm Mounting Holes
Limit RPM (RPM)
6400
Recommendations
Recommended Solution：VL8022 KV170+V150A/VL1028 KV190+V200A
Limit Thrust (kg)
36
Test Data Export to Excel
Ambient Temperature 22 °C Altitude 25 m
RPM (RPM)
Torque （N·m)
RecommendedThrust （gf）
Output Power （W）
力Effciency （gf/W）
vz29x11-draw.png
2200
1.35
3957
311.14
12.72
2500
1.71
5074
446.51
11.36
2800
2.13
6377
623.82
10.22
3100
2.62
7864
849.38
9.26
3400
3.17
9536
1129.49
8.44
3700
3.80
11393
1470.48
7.75
4000
4.48
13434
1878.65
7.15
4300
5.24
15661
2360.31
6.64
4600
6.07
18072
2921.78
6.19
4900
6.96
20668
3569.35
5.79
5200
7.91
23449
4309.35
5.44
5500
8.94
26415
5148.09
5.13
5800
10.03
29566
6091.87
4.85
6100
11.19
32901
7147.00
4.60
6400
12.41
36421
8319.80
4.38
Important Notes
Data may vary under different testing standards due to factors such as equipment, methodology, and environment. Ensure compatibility between the propeller mounting holes and motors. Refer to the drawing above for details.
Packing List
T-Motor VZ29x9.5 VTOL 29 Zoll Carbon Propeller 1x CW 1x CCW
Artikelnr.: PM-7266 | HAN: VZ29x9.5
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VZ SERIES -VTOL PROPELLERS
Break through the performance limitations of traditional multi-rotor propellers. VZ series propellers deliver superior power, durability, and lightweight design for VTOL applications
What Does a VTOL Propeller Need?
High Strength High Stiffness & Lightweight Design
High Strength
Withstands immense centrifugal loads and maneuver-induced alternating loads at high RPM, preventing structural failure
High Stiffness
Ensures safe blade-tip clearance in compact layouts, suppresses aeroelastic deformation, and prevents flutter
Lightweight Design
Reduce the moment of inertia to achieve rapid thrust response and higher attitude control bandwidth for the flight control system
Superior Aerodynamic Design
The unique dual operational modes of VTOL—vertical takeoff/landing and cruise—demand new propeller capabilities
Vertical Takeoff & Landing Phase
Requiring high thrust and power, demanding maximum lift output from the propeller disk within a limited blade area
Cruise Phase
When the propeller stops rotating, it is necessary to minimize profile drag to reduce power consumption, achieving "stealthy" low-drag efficiency
Transition Stability: Resisting Complex Flow Field Interference
The extreme challenges posed by high angle of attack, low speed and unsteady flow field, coupled with the insufficient strength and poor transition stability of traditional blades, make this an accident-prone region
Unsteady Flow Fields at High Angle of Attack
The aircraft operates at high angles of attack and low speeds within an extremely complex flow environment
Asymmetric Airflow
Significant angle between incoming flow and the rotation axis causes asymmetric airflow entering the propeller disc
Severe Periodic Variations
Local forces on the blade fluctuate drastically per rotation, inducing flutter and causing significant thrust fluctuation
To address the challenges of traditional propellers in VTOL (Vertical Takeoff and Landing mode) applications
we introduce the VZ Series Propellers
Technical Features of the VZ Series Propellers
Advanced composite materials and exceptional aerodynamic design work in synergy to ensure consistently efficient, reliable, and controllable power output
Bending & Torsion Resistant Layup Design
Optimized fiber orientation and ratio maximize strength and stiffness
Prepreg Compression Molding for Integrated Forming
Product porosity below 1%, ensuring stable and reliable quality
PMI Foam Core
Lightweight, high-strength core material effectively increases stiffness while controlling total weight
30%
Flexural Strength
Significantly enhanced impact resistance and deformation resistance for greater durability in complex operating conditions
20%
Torsional Stiffness
Optimized power transmission efficiency reduces energy loss during operation
Blade Root Optimization: Safety Redundancy Design
The blade root thickness is optimized to provide structural redundancy while reducing loads on the connecting bolts
V30 Propeller
VZ30 Propeller
Aerodynamic Priority: Engineered for High VTOL Thrust
Dedicated High Lift-to- Drag Ratio Airfoil
Optimized for VTOL conditions to enhance maximum lift coefficient
Low-Drag Cruise Blade Shape
Improved aerodynamic blade boundaries reduce cruise drag
Specialized Blade Tip
Optimized tip design weakens vortex strength and enhances flight quality
Custom VTOL Propeller Service: 10 to 100 Inches
Supports precise matching with various pitch specifications and motors Full in-house R&D ensures stable and controllable quality
Aerodynamic/Structural Design
Mold Manufacturing
Composite Molding
Testing & Validation
? The appearance diagrams and product renderings in this document are for reference only; the actual product shall prevail.
? Data regarding improvements in flexural strength and torsional stiffness are derived from comparative testing between the VZ Series propeller and the G Series propellers.
? Data regarding the reduction in bolt shear load is sourced from simulation comparisons between the installation bolts for the VZ Series propellers and those for the V Series propellers.
? The test data presented above were obtained under specific conditions, using equipment within our company's laboratory. Actual data and parameters may vary slightly depending on the test environment, platform, software, and other factors.
Technical Drawing
Specification Export to Excel
Diameter (Inch)
29(736.6mm)
Material
Resin-basedCarbonFiberComposite+PMIFoamCore
Pitch (Inch)
9.5(241.3mm)
Surface Treatment
Matte
AverageSingleblade Weight (g)
85
Type
One-Piece Straight Propeller
RecommendedMax RPM (RPM)
6100
Application
VTOL Fixed-Wing UAVs, Multicopter Mode
RecommendedMax Thrust (kg)
28.8
Connections & Dimensions
Flange Mount, Ø10 mm Center Hole, Ø20 mm Bolt Circle, with 4x Ø3 mm Mounting Holes
Limit RPM (RPM)
6800
Recommendations
Recommended Solution：VL8022 KV170+V150A/VL1028 KV190+V200A
Limit Thrust (kg)
36
Test Data Export to Excel
Ambient Temperature 22 °C Altitude 25 m
RPM (RPM)
Torque （N·m)
RecommendedThrust （gf）
Output Power （W）
力Effciency （gf/W）
vz29x9.5-draw.png
1400
0.84
2111
122.98
17.16
1800
0.98
2707
184.01
14.71
2200
1.22
3614
281.24
12.85
2600
1.57
4832
428.12
11.29
3000
2.03
6362
638.12
9.97
3400
2.60
8202
924.70
8.87
3800
3.27
10355
1301.34
7.96
4200
4.05
12818
1781.49
7.20
4600
4.94
15592
2378.61
6.56
5000
5.93
18678
3106.18
6.01
5400
7.03
22075
3977.65
5.55
5800
8.24
25784
5006.50
5.15
6200
9.56
29803
6206.17
4.80
6600
10.98
34134
7590.15
4.50
6800
11.73
36416
8355.45
4.36
Important Notes
Data may vary under different testing standards due to factors such as equipment, methodology, and environment. Ensure compatibility between the propeller mounting holes and motors. Refer to the drawing above for details.
Packing List
T-Motor VZ30x10.5 VTOL 30 Zoll Carbon Propeller 1x CW 1x CCW
Artikelnr.: PM-7268 | HAN: VZ30x10.5
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VZ SERIES -VTOL PROPELLERS
Break through the performance limitations of traditional multi-rotor propellers. VZ series propellers deliver superior power, durability, and lightweight design for VTOL applications
What Does a VTOL Propeller Need?
High Strength High Stiffness & Lightweight Design
High Strength
Withstands immense centrifugal loads and maneuver-induced alternating loads at high RPM, preventing structural failure
High Stiffness
Ensures safe blade-tip clearance in compact layouts, suppresses aeroelastic deformation, and prevents flutter
Lightweight Design
Reduce the moment of inertia to achieve rapid thrust response and higher attitude control bandwidth for the flight control system
Superior Aerodynamic Design
The unique dual operational modes of VTOL—vertical takeoff/landing and cruise—demand new propeller capabilities
Vertical Takeoff & Landing Phase
Requiring high thrust and power, demanding maximum lift output from the propeller disk within a limited blade area
Cruise Phase
When the propeller stops rotating, it is necessary to minimize profile drag to reduce power consumption, achieving "stealthy" low-drag efficiency
Transition Stability: Resisting Complex Flow Field Interference
The extreme challenges posed by high angle of attack, low speed and unsteady flow field, coupled with the insufficient strength and poor transition stability of traditional blades, make this an accident-prone region
Unsteady Flow Fields at High Angle of Attack
The aircraft operates at high angles of attack and low speeds within an extremely complex flow environment
Asymmetric Airflow
Significant angle between incoming flow and the rotation axis causes asymmetric airflow entering the propeller disc
Severe Periodic Variations
Local forces on the blade fluctuate drastically per rotation, inducing flutter and causing significant thrust fluctuation
To address the challenges of traditional propellers in VTOL (Vertical Takeoff and Landing mode) applications
we introduce the VZ Series Propellers
Technical Features of the VZ Series Propellers
Advanced composite materials and exceptional aerodynamic design work in synergy to ensure consistently efficient, reliable, and controllable power output
Bending & Torsion Resistant Layup Design
Optimized fiber orientation and ratio maximize strength and stiffness
Prepreg Compression Molding for Integrated Forming
Product porosity below 1%, ensuring stable and reliable quality
PMI Foam Core
Lightweight, high-strength core material effectively increases stiffness while controlling total weight
30%
Flexural Strength
Significantly enhanced impact resistance and deformation resistance for greater durability in complex operating conditions
20%
Torsional Stiffness
Optimized power transmission efficiency reduces energy loss during operation
Blade Root Optimization: Safety Redundancy Design
The blade root thickness is optimized to provide structural redundancy while reducing loads on the connecting bolts
V30 Propeller
VZ30 Propeller
Aerodynamic Priority: Engineered for High VTOL Thrust
Dedicated High Lift-to- Drag Ratio Airfoil
Optimized for VTOL conditions to enhance maximum lift coefficient
Low-Drag Cruise Blade Shape
Improved aerodynamic blade boundaries reduce cruise drag
Specialized Blade Tip
Optimized tip design weakens vortex strength and enhances flight quality
Custom VTOL Propeller Service: 10 to 100 Inches
Supports precise matching with various pitch specifications and motors Full in-house R&D ensures stable and controllable quality
Aerodynamic/Structural Design
Mold Manufacturing
Composite Molding
Testing & Validation
? The appearance diagrams and product renderings in this document are for reference only; the actual product shall prevail.
? Data regarding improvements in flexural strength and torsional stiffness are derived from comparative testing between the VZ Series propeller and the G Series propellers.
? Data regarding the reduction in bolt shear load is sourced from simulation comparisons between the installation bolts for the VZ Series propellers and those for the V Series propellers.
? The test data presented above were obtained under specific conditions, using equipment within our company's laboratory. Actual data and parameters may vary slightly depending on the test environment, platform, software, and other factors.
Technical Drawing
Specification Export to Excel
Diameter (Inch)
30(275.5mm)
Material
Resin-basedCarbonFiberComposite+PMIFoamCore
Pitch (Inch)
10.5(266.7mm)
Surface Treatment
Matte
AverageSingleblade Weight (g)
98
Type
One-Piece Straight Propeller
RecommendedMax RPM (RPM)
5600
Application
VTOL Fixed-Wing UAVs, Multicopter Mode
RecommendedMax Thrust (kg)
32
Connections & Dimensions
Flange Mount, Ø10 mm Center Hole, Ø20 mm Bolt Circle, with 4x Ø3 mm Mounting Holes
Limit RPM (RPM)
6200
Recommendations
Recommended Solution：VL1032+KV180+V200A
Limit Thrust (kg)
40
Test Data Export to Excel
Ambient Temperature 22 °C Altitude 25 m
RPM (RPM)
Torque （N·m)
RecommendedThrust （gf）
Output Power （W）
力Effciency （gf/W）
vz30x10.5-draw.png
2000
1.45
3972
304.72
13.04
2300
1.80
5075
434.30
11.69
2600
2.24
6406
610.05
10.50
2900
2.77
7964
840.35
9.48
3200
3.38
9749
1133.63
8.60
3500
4.09
11761
1498.27
7.85
3800
4.88
14000
1942.69
7.21
4100
5.77
16467
2475.29
6.65
4400
6.74
19161
3104.46
6.17
4700
7.80
22083
3838.63
5.75
5000
8.95
25231
4686.18
5.38
5300
10.19
28607
5655.52
5.06
5600
11.52
32211
6755.06
4.77
5900
12.94
36041
7993.20
4.51
6200
14.44
40099
9378.34
4.28
Important Notes
Data may vary under different testing standards due to factors such as equipment, methodology, and environment. Ensure compatibility between the propeller mounting holes and motors. Refer to the drawing above for details.
Packing List
T-Motor VZ30x12 VTOL 30 Zoll Carbon Propeller 1x CW 1x CCW
Artikelnr.: PM-7269 | HAN: VZ30x12
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VZ SERIES -VTOL PROPELLERS
Break through the performance limitations of traditional multi-rotor propellers. VZ series propellers deliver superior power, durability, and lightweight design for VTOL applications
What Does a VTOL Propeller Need?
High Strength High Stiffness & Lightweight Design
High Strength
Withstands immense centrifugal loads and maneuver-induced alternating loads at high RPM, preventing structural failure
High Stiffness
Ensures safe blade-tip clearance in compact layouts, suppresses aeroelastic deformation, and prevents flutter
Lightweight Design
Reduce the moment of inertia to achieve rapid thrust response and higher attitude control bandwidth for the flight control system
Superior Aerodynamic Design
The unique dual operational modes of VTOL—vertical takeoff/landing and cruise—demand new propeller capabilities
Vertical Takeoff & Landing Phase
Requiring high thrust and power, demanding maximum lift output from the propeller disk within a limited blade area
Cruise Phase
When the propeller stops rotating, it is necessary to minimize profile drag to reduce power consumption, achieving "stealthy" low-drag efficiency
Transition Stability: Resisting Complex Flow Field Interference
The extreme challenges posed by high angle of attack, low speed and unsteady flow field, coupled with the insufficient strength and poor transition stability of traditional blades, make this an accident-prone region
Unsteady Flow Fields at High Angle of Attack
The aircraft operates at high angles of attack and low speeds within an extremely complex flow environment
Asymmetric Airflow
Significant angle between incoming flow and the rotation axis causes asymmetric airflow entering the propeller disc
Severe Periodic Variations
Local forces on the blade fluctuate drastically per rotation, inducing flutter and causing significant thrust fluctuation
To address the challenges of traditional propellers in VTOL (Vertical Takeoff and Landing mode) applications
we introduce the VZ Series Propellers
Technical Features of the VZ Series Propellers
Advanced composite materials and exceptional aerodynamic design work in synergy to ensure consistently efficient, reliable, and controllable power output
Bending & Torsion Resistant Layup Design
Optimized fiber orientation and ratio maximize strength and stiffness
Prepreg Compression Molding for Integrated Forming
Product porosity below 1%, ensuring stable and reliable quality
PMI Foam Core
Lightweight, high-strength core material effectively increases stiffness while controlling total weight
30%
Flexural Strength
Significantly enhanced impact resistance and deformation resistance for greater durability in complex operating conditions
20%
Torsional Stiffness
Optimized power transmission efficiency reduces energy loss during operation
Blade Root Optimization: Safety Redundancy Design
The blade root thickness is optimized to provide structural redundancy while reducing loads on the connecting bolts
V30 Propeller
VZ30 Propeller
Aerodynamic Priority: Engineered for High VTOL Thrust
Dedicated High Lift-to- Drag Ratio Airfoil
Optimized for VTOL conditions to enhance maximum lift coefficient
Low-Drag Cruise Blade Shape
Improved aerodynamic blade boundaries reduce cruise drag
Specialized Blade Tip
Optimized tip design weakens vortex strength and enhances flight quality
Custom VTOL Propeller Service: 10 to 100 Inches
Supports precise matching with various pitch specifications and motors Full in-house R&D ensures stable and controllable quality
Aerodynamic/Structural Design
Mold Manufacturing
Composite Molding
Testing & Validation
? The appearance diagrams and product renderings in this document are for reference only; the actual product shall prevail.
? Data regarding improvements in flexural strength and torsional stiffness are derived from comparative testing between the VZ Series propeller and the G Series propellers.
? Data regarding the reduction in bolt shear load is sourced from simulation comparisons between the installation bolts for the VZ Series propellers and those for the V Series propellers.
? The test data presented above were obtained under specific conditions, using equipment within our company's laboratory. Actual data and parameters may vary slightly depending on the test environment, platform, software, and other factors.
Technical Drawing
Specification Export to Excel
Diameter (Inch)
30(275.5mm)
Material
Resin-basedCarbonFiberComposite+PMIFoamCore
Pitch (Inch)
12(304.8mm)
Surface Treatment
Matte
AverageSingleblade Weight (g)
99
Type
One-Piece Straight Propeller
RecommendedMax RPM (RPM)
5400
Application
VTOL Fixed-Wing UAVs, Multicopter Mode
RecommendedMax Thrust (kg)
32
Connections & Dimensions
Flange Mount, Ø10 mm Center Hole, Ø20 mm Bolt Circle, with 4x Ø3 mm Mounting Holes
Limit RPM (RPM)
6000
Recommendations
Recommended Solution：VL1032+KV180+V200A
Limit Thrust (kg)
40
Test Data Export to Excel
Ambient Temperature 22 °C Altitude 25 m
RPM (RPM)
Torque （N·m)
RecommendedThrust （gf）
Output Power （W）
力Effciency （gf/W）
vz30x12-draw.png
1800
1.38
3734
259.85
14.37
2100
1.71
4745
375.90
12.62
2400
2.14
6005
537.22
11.18
2700
2.66
7515
753.00
9.98
3000
3.29
9276
1032.44
8.98
3300
4.01
11286
1384.71
8.15
3600
4.83
13546
1819.01
7.45
3900
5.74
16057
2344.51
6.85
4200
6.75
18817
2970.41
6.33
4500
7.86
21827
3705.89
5.89
4800
9.07
25088
4560.14
5.50
5100
10.38
28598
5542.34
5.16
5400
11.78
32358
6661.68
4.86
5700
13.28
36369
7927.34
4.59
6000
14.88
40629
9348.52
4.35
Important Notes
Data may vary under different testing standards due to factors such as equipment, methodology, and environment. Ensure compatibility between the propeller mounting holes and motors. Refer to the drawing above for details.
Packing List
T-Motor VZ32x12 VTOL 32 Zoll Carbon Propeller 1x CW 1x CCW
Artikelnr.: PM-7270 | HAN: VZ32x12
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transform: none !important; transition: none !important; } .scaleInit { opacity: 1 !important; transform: none !important; transition: none !important; } #parameter { display: block !important; padding: 20px 5%; background: #fff; color: #333; } #parameter .mainBox { margin-bottom: 30px; } #parameter .tableTitle { font-size: 20px; font-weight: bold; padding: 15px 0; border-bottom: 2px solid #333; } #parameter table { width: 100%; border-collapse: collapse; margin: 10px 0; } #parameter td, #parameter th { border: 1px solid #ddd; padding: 8px; font-size: 14px; } #parameter img { max-width: 100%; height: auto; }
VZ SERIES -VTOL PROPELLERS
Break through the performance limitations of traditional multi-rotor propellers. VZ series propellers deliver superior power, durability, and lightweight design for VTOL applications
What Does a VTOL Propeller Need?
High Strength High Stiffness & Lightweight Design
High Strength
Withstands immense centrifugal loads and maneuver-induced alternating loads at high RPM, preventing structural failure
High Stiffness
Ensures safe blade-tip clearance in compact layouts, suppresses aeroelastic deformation, and prevents flutter
Lightweight Design
Reduce the moment of inertia to achieve rapid thrust response and higher attitude control bandwidth for the flight control system
Superior Aerodynamic Design
The unique dual operational modes of VTOL—vertical takeoff/landing and cruise—demand new propeller capabilities
Vertical Takeoff & Landing Phase
Requiring high thrust and power, demanding maximum lift output from the propeller disk within a limited blade area
Cruise Phase
When the propeller stops rotating, it is necessary to minimize profile drag to reduce power consumption, achieving "stealthy" low-drag efficiency
Transition Stability: Resisting Complex Flow Field Interference
The extreme challenges posed by high angle of attack, low speed and unsteady flow field, coupled with the insufficient strength and poor transition stability of traditional blades, make this an accident-prone region
Unsteady Flow Fields at High Angle of Attack
The aircraft operates at high angles of attack and low speeds within an extremely complex flow environment
Asymmetric Airflow
Significant angle between incoming flow and the rotation axis causes asymmetric airflow entering the propeller disc
Severe Periodic Variations
Local forces on the blade fluctuate drastically per rotation, inducing flutter and causing significant thrust fluctuation
To address the challenges of traditional propellers in VTOL (Vertical Takeoff and Landing mode) applications
we introduce the VZ Series Propellers
Technical Features of the VZ Series Propellers
Advanced composite materials and exceptional aerodynamic design work in synergy to ensure consistently efficient, reliable, and controllable power output
Bending & Torsion Resistant Layup Design
Optimized fiber orientation and ratio maximize strength and stiffness
Prepreg Compression Molding for Integrated Forming
Product porosity below 1%, ensuring stable and reliable quality
PMI Foam Core
Lightweight, high-strength core material effectively increases stiffness while controlling total weight
30%
Flexural Strength
Significantly enhanced impact resistance and deformation resistance for greater durability in complex operating conditions
20%
Torsional Stiffness
Optimized power transmission efficiency reduces energy loss during operation
Blade Root Optimization: Safety Redundancy Design
The blade root thickness is optimized to provide structural redundancy while reducing loads on the connecting bolts
V30 Propeller
VZ30 Propeller
Aerodynamic Priority: Engineered for High VTOL Thrust
Dedicated High Lift-to- Drag Ratio Airfoil
Optimized for VTOL conditions to enhance maximum lift coefficient
Low-Drag Cruise Blade Shape
Improved aerodynamic blade boundaries reduce cruise drag
Specialized Blade Tip
Optimized tip design weakens vortex strength and enhances flight quality
Custom VTOL Propeller Service: 10 to 100 Inches
Supports precise matching with various pitch specifications and motors Full in-house R&D ensures stable and controllable quality
Aerodynamic/Structural Design
Mold Manufacturing
Composite Molding
Testing & Validation
? The appearance diagrams and product renderings in this document are for reference only; the actual product shall prevail.
? Data regarding improvements in flexural strength and torsional stiffness are derived from comparative testing between the VZ Series propeller and the G Series propellers.
? Data regarding the reduction in bolt shear load is sourced from simulation comparisons between the installation bolts for the VZ Series propellers and those for the V Series propellers.
? The test data presented above were obtained under specific conditions, using equipment within our company's laboratory. Actual data and parameters may vary slightly depending on the test environment, platform, software, and other factors.
Technical Drawing
Specification Export to Excel
Diameter (Inch)
32(812.8mm)
Material
Resin-basedCarbonFiberComposite+PMIFoamCore
Pitch (Inch)
12(304.8mm)
Surface Treatment
Matte
AverageSingleblade Weight (g)
133
Type
One-Piece Straight Propeller
RecommendedMax RPM (RPM)
5100
Application
VTOL Fixed-Wing UAVs, Multicopter Mode
RecommendedMax Thrust (kg)
34.4
Connections & Dimensions
Flange Mount, Ø10 mm Center Hole, Ø23 mm Bolt Circle, with 4x Ø4.1 mm Mounting Holes
Limit RPM (RPM)
5600
Recommendations
Recommended Solution：VL1035 KV150+V200A/VL1040 KV150+VL248A
Limit Thrust (kg)
43
Test Data Export to Excel
Ambient Temperature 22 °C Altitude 25 m
RPM (RPM)
Torque （N·m)
RecommendedThrust （gf）
Output Power （W）
力Effciency （gf/W）
vz32x12-draw.png
1400
0.98
2454
143.61
17.09
1700
1.39
3596
247.84
14.51
2000
1.91
5008
400.71
12.50
2300
2.54
6691
612.45
10.93
2600
3.28
8645
893.28
9.68
2900
4.13
10869
1253.42
8.67
3200
5.08
13364
1703.11
7.85
3500
6.15
16129
2252.56
7.16
3800
7.32
19165
2911.99
6.58
4100
8.60
22472
3691.63
6.09
4400
9.99
26049
4601.71
5.66
4700
11.48
29897
5652.44
5.29
5000
13.09
34016
6854.05
4.96
5300
14.80
38405
8216.77
4.67
5600
16.63
43065
9750.82
4.42
Important Notes
Data may vary under different testing standards due to factors such as equipment, methodology, and environment. Ensure compatibility between the propeller mounting holes and motors. Refer to the drawing above for details.
Packing List
T-Motor VZ34x13 VTOL 34 Zoll Carbon Propeller 1x CW 1x CCW
Artikelnr.: PM-7271 | HAN: VZ34x13
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VZ SERIES -VTOL PROPELLERS
Break through the performance limitations of traditional multi-rotor propellers. VZ series propellers deliver superior power, durability, and lightweight design for VTOL applications
What Does a VTOL Propeller Need?
High Strength High Stiffness & Lightweight Design
High Strength
Withstands immense centrifugal loads and maneuver-induced alternating loads at high RPM, preventing structural failure
High Stiffness
Ensures safe blade-tip clearance in compact layouts, suppresses aeroelastic deformation, and prevents flutter
Lightweight Design
Reduce the moment of inertia to achieve rapid thrust response and higher attitude control bandwidth for the flight control system
Superior Aerodynamic Design
The unique dual operational modes of VTOL—vertical takeoff/landing and cruise—demand new propeller capabilities
Vertical Takeoff & Landing Phase
Requiring high thrust and power, demanding maximum lift output from the propeller disk within a limited blade area
Cruise Phase
When the propeller stops rotating, it is necessary to minimize profile drag to reduce power consumption, achieving "stealthy" low-drag efficiency
Transition Stability: Resisting Complex Flow Field Interference
The extreme challenges posed by high angle of attack, low speed and unsteady flow field, coupled with the insufficient strength and poor transition stability of traditional blades, make this an accident-prone region
Unsteady Flow Fields at High Angle of Attack
The aircraft operates at high angles of attack and low speeds within an extremely complex flow environment
Asymmetric Airflow
Significant angle between incoming flow and the rotation axis causes asymmetric airflow entering the propeller disc
Severe Periodic Variations
Local forces on the blade fluctuate drastically per rotation, inducing flutter and causing significant thrust fluctuation
To address the challenges of traditional propellers in VTOL (Vertical Takeoff and Landing mode) applications
we introduce the VZ Series Propellers
Technical Features of the VZ Series Propellers
Advanced composite materials and exceptional aerodynamic design work in synergy to ensure consistently efficient, reliable, and controllable power output
Bending & Torsion Resistant Layup Design
Optimized fiber orientation and ratio maximize strength and stiffness
Prepreg Compression Molding for Integrated Forming
Product porosity below 1%, ensuring stable and reliable quality
PMI Foam Core
Lightweight, high-strength core material effectively increases stiffness while controlling total weight
30%
Flexural Strength
Significantly enhanced impact resistance and deformation resistance for greater durability in complex operating conditions
20%
Torsional Stiffness
Optimized power transmission efficiency reduces energy loss during operation
Blade Root Optimization: Safety Redundancy Design
The blade root thickness is optimized to provide structural redundancy while reducing loads on the connecting bolts
V30 Propeller
VZ30 Propeller
Aerodynamic Priority: Engineered for High VTOL Thrust
Dedicated High Lift-to- Drag Ratio Airfoil
Optimized for VTOL conditions to enhance maximum lift coefficient
Low-Drag Cruise Blade Shape
Improved aerodynamic blade boundaries reduce cruise drag
Specialized Blade Tip
Optimized tip design weakens vortex strength and enhances flight quality
Custom VTOL Propeller Service: 10 to 100 Inches
Supports precise matching with various pitch specifications and motors Full in-house R&D ensures stable and controllable quality
Aerodynamic/Structural Design
Mold Manufacturing
Composite Molding
Testing & Validation
? The appearance diagrams and product renderings in this document are for reference only; the actual product shall prevail.
? Data regarding improvements in flexural strength and torsional stiffness are derived from comparative testing between the VZ Series propeller and the G Series propellers.
? Data regarding the reduction in bolt shear load is sourced from simulation comparisons between the installation bolts for the VZ Series propellers and those for the V Series propellers.
? The test data presented above were obtained under specific conditions, using equipment within our company's laboratory. Actual data and parameters may vary slightly depending on the test environment, platform, software, and other factors.
Technical Drawing
Specification Export to Excel
Diameter (Inch)
34(863.6mm)
Material
Resin-basedCarbonFiberComposite+PMIFoamCore
Pitch (Inch)
13(330.2mm)
Surface Treatment
Matte
AverageSingleblade Weight (g)
151
Type
One-Piece Straight Propeller
RecommendedMax RPM (RPM)
4800
Application
VTOL Fixed-Wing UAVs, Multicopter Mode
RecommendedMax Thrust (kg)
37.6
Connections & Dimensions
Flange Mount, Ø10 mm Center Hole, Ø23 mm Bolt Circle, with 4x Ø4.1 mm Mounting Holes
Limit RPM (RPM)
5300
Recommendations
Limit Thrust (kg)
47
Test Data Export to Excel
Ambient Temperature 22 °C Altitude 25 m
RPM (RPM)
Torque （N·m)
RecommendedThrust （gf）
Output Power （W）
力Effciency （gf/W）
vz34x13-draw.png
1800
2.03
5042
383.48
13.15
2050
2.61
6535
560.82
11.65
2300
3.29
8261
791.43
10.44
2550
4.05
10220
1082.81
9.44
2800
4.92
12411
1442.46
8.60
3050
5.88
14834
1877.87
7.90
3300
6.93
17490
2396.56
7.30
3550
8.09
20379
3006.02
6.78
3800
9.33
23500
3713.75
6.33
4050
10.67
26853
4527.25
5.93
4300
12.11
30440
5454.02
5.58
4550
13.65
34258
6501.57
5.27
4800
15.27
38309
7677.40
4.99
5050
17.00
42593
8989.00
4.74
5300
18.82
47109
10443.88
4.51
Important Notes
Data may vary under different testing standards due to factors such as equipment, methodology, and environment. Ensure compatibility between the propeller mounting holes and motors. Refer to the drawing above for details.
Packing List
T-Motor VZ38x15 VTOL 38 Zoll Carbon Propeller 1x CW 1x CCW
Artikelnr.: PM-7272 | HAN: VZ38x15
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VZ SERIES -VTOL PROPELLERS
Break through the performance limitations of traditional multi-rotor propellers. VZ series propellers deliver superior power, durability, and lightweight design for VTOL applications
What Does a VTOL Propeller Need?
High Strength High Stiffness & Lightweight Design
High Strength
Withstands immense centrifugal loads and maneuver-induced alternating loads at high RPM, preventing structural failure
High Stiffness
Ensures safe blade-tip clearance in compact layouts, suppresses aeroelastic deformation, and prevents flutter
Lightweight Design
Reduce the moment of inertia to achieve rapid thrust response and higher attitude control bandwidth for the flight control system
Superior Aerodynamic Design
The unique dual operational modes of VTOL—vertical takeoff/landing and cruise—demand new propeller capabilities
Vertical Takeoff & Landing Phase
Requiring high thrust and power, demanding maximum lift output from the propeller disk within a limited blade area
Cruise Phase
When the propeller stops rotating, it is necessary to minimize profile drag to reduce power consumption, achieving "stealthy" low-drag efficiency
Transition Stability: Resisting Complex Flow Field Interference
The extreme challenges posed by high angle of attack, low speed and unsteady flow field, coupled with the insufficient strength and poor transition stability of traditional blades, make this an accident-prone region
Unsteady Flow Fields at High Angle of Attack
The aircraft operates at high angles of attack and low speeds within an extremely complex flow environment
Asymmetric Airflow
Significant angle between incoming flow and the rotation axis causes asymmetric airflow entering the propeller disc
Severe Periodic Variations
Local forces on the blade fluctuate drastically per rotation, inducing flutter and causing significant thrust fluctuation
To address the challenges of traditional propellers in VTOL (Vertical Takeoff and Landing mode) applications
we introduce the VZ Series Propellers
Technical Features of the VZ Series Propellers
Advanced composite materials and exceptional aerodynamic design work in synergy to ensure consistently efficient, reliable, and controllable power output
Bending & Torsion Resistant Layup Design
Optimized fiber orientation and ratio maximize strength and stiffness
Prepreg Compression Molding for Integrated Forming
Product porosity below 1%, ensuring stable and reliable quality
PMI Foam Core
Lightweight, high-strength core material effectively increases stiffness while controlling total weight
30%
Flexural Strength
Significantly enhanced impact resistance and deformation resistance for greater durability in complex operating conditions
20%
Torsional Stiffness
Optimized power transmission efficiency reduces energy loss during operation
Blade Root Optimization: Safety Redundancy Design
The blade root thickness is optimized to provide structural redundancy while reducing loads on the connecting bolts
V30 Propeller
VZ30 Propeller
Aerodynamic Priority: Engineered for High VTOL Thrust
Dedicated High Lift-to- Drag Ratio Airfoil
Optimized for VTOL conditions to enhance maximum lift coefficient
Low-Drag Cruise Blade Shape
Improved aerodynamic blade boundaries reduce cruise drag
Specialized Blade Tip
Optimized tip design weakens vortex strength and enhances flight quality
Custom VTOL Propeller Service: 10 to 100 Inches
Supports precise matching with various pitch specifications and motors Full in-house R&D ensures stable and controllable quality
Aerodynamic/Structural Design
Mold Manufacturing
Composite Molding
Testing & Validation
? The appearance diagrams and product renderings in this document are for reference only; the actual product shall prevail.
? Data regarding improvements in flexural strength and torsional stiffness are derived from comparative testing between the VZ Series propeller and the G Series propellers.
? Data regarding the reduction in bolt shear load is sourced from simulation comparisons between the installation bolts for the VZ Series propellers and those for the V Series propellers.
? The test data presented above were obtained under specific conditions, using equipment within our company's laboratory. Actual data and parameters may vary slightly depending on the test environment, platform, software, and other factors.
Technical Drawing
Specification Export to Excel
Diameter (Inch)
38(965.2mm)
Material
Resin-basedCarbonFiberComposite+PMIFoamCore
Pitch (Inch)
15(381mm)
Surface Treatment
Matte
AverageSingleblade Weight (g)
188
Type
One-Piece Straight Propeller
RecommendedMax RPM (RPM)
3950
Application
VTOL Fixed-Wing UAVs, Multicopter Mode
RecommendedMax Thrust (kg)
44
Connections & Dimensions
Flange Mount, Ø12 mm Center Hole, Ø30 mm Bolt Circle, with 4x Ø5 mm Mounting Holes
Limit RPM (RPM)
4400
Recommendations
Limit Thrust (kg)
55
Test Data Export to Excel
Ambient Temperature 22 °C Altitude 25 m
RPM (RPM)
Torque （N·m)
RecommendedThrust （gf）
Output Power （W）
力Effciency （gf/W）
vz38x15-draw.png
1600
3.21
6841
538.58
12.70
1800
4.09
8724
770.09
11.33
2000
5.07
10854
1062.62
10.21
2200
6.18
13228
1423.53
9.29
2400
7.40
15849
1860.18
8.52
2600
8.74
18714
2379.93
7.86
2800
10.20
21826
2990.13
7.30
3000
11.77
25183
3698.15
6.81
3200
13.46
28786
4511.35
6.38
3400
15.27
32634
5437.09
6.00
3600
17.20
36728
6482.72
5.67
3800
19.24
41067
7655.61
5.36
4000
21.40
45652
8963.11
5.09
4200
23.67
50482
10412.59
4.85
4400
26.07
55558
12011.40
4.63
Important Notes
Data may vary under different testing standards due to factors such as equipment, methodology, and environment. Ensure compatibility between the propeller mounting holes and motors. Refer to the drawing above for details.
Packing List
T-Motor VZ40x16.1 VTOL 40 Zoll Carbon Propeller 1x CW 1x CCW
Artikelnr.: PM-7273 | HAN: VZ40x16.1
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VZ SERIES -VTOL PROPELLERS
Break through the performance limitations of traditional multi-rotor propellers. VZ series propellers deliver superior power, durability, and lightweight design for VTOL applications
What Does a VTOL Propeller Need?
High Strength High Stiffness & Lightweight Design
High Strength
Withstands immense centrifugal loads and maneuver-induced alternating loads at high RPM, preventing structural failure
High Stiffness
Ensures safe blade-tip clearance in compact layouts, suppresses aeroelastic deformation, and prevents flutter
Lightweight Design
Reduce the moment of inertia to achieve rapid thrust response and higher attitude control bandwidth for the flight control system
Superior Aerodynamic Design
The unique dual operational modes of VTOL—vertical takeoff/landing and cruise—demand new propeller capabilities
Vertical Takeoff & Landing Phase
Requiring high thrust and power, demanding maximum lift output from the propeller disk within a limited blade area
Cruise Phase
When the propeller stops rotating, it is necessary to minimize profile drag to reduce power consumption, achieving "stealthy" low-drag efficiency
Transition Stability: Resisting Complex Flow Field Interference
The extreme challenges posed by high angle of attack, low speed and unsteady flow field, coupled with the insufficient strength and poor transition stability of traditional blades, make this an accident-prone region
Unsteady Flow Fields at High Angle of Attack
The aircraft operates at high angles of attack and low speeds within an extremely complex flow environment
Asymmetric Airflow
Significant angle between incoming flow and the rotation axis causes asymmetric airflow entering the propeller disc
Severe Periodic Variations
Local forces on the blade fluctuate drastically per rotation, inducing flutter and causing significant thrust fluctuation
To address the challenges of traditional propellers in VTOL (Vertical Takeoff and Landing mode) applications
we introduce the VZ Series Propellers
Technical Features of the VZ Series Propellers
Advanced composite materials and exceptional aerodynamic design work in synergy to ensure consistently efficient, reliable, and controllable power output
Bending & Torsion Resistant Layup Design
Optimized fiber orientation and ratio maximize strength and stiffness
Prepreg Compression Molding for Integrated Forming
Product porosity below 1%, ensuring stable and reliable quality
PMI Foam Core
Lightweight, high-strength core material effectively increases stiffness while controlling total weight
30%
Flexural Strength
Significantly enhanced impact resistance and deformation resistance for greater durability in complex operating conditions
20%
Torsional Stiffness
Optimized power transmission efficiency reduces energy loss during operation
Blade Root Optimization: Safety Redundancy Design
The blade root thickness is optimized to provide structural redundancy while reducing loads on the connecting bolts
V30 Propeller
VZ30 Propeller
Aerodynamic Priority: Engineered for High VTOL Thrust
Dedicated High Lift-to- Drag Ratio Airfoil
Optimized for VTOL conditions to enhance maximum lift coefficient
Low-Drag Cruise Blade Shape
Improved aerodynamic blade boundaries reduce cruise drag
Specialized Blade Tip
Optimized tip design weakens vortex strength and enhances flight quality
Custom VTOL Propeller Service: 10 to 100 Inches
Supports precise matching with various pitch specifications and motors Full in-house R&D ensures stable and controllable quality
Aerodynamic/Structural Design
Mold Manufacturing
Composite Molding
Testing & Validation
? The appearance diagrams and product renderings in this document are for reference only; the actual product shall prevail.
? Data regarding improvements in flexural strength and torsional stiffness are derived from comparative testing between the VZ Series propeller and the G Series propellers.
? Data regarding the reduction in bolt shear load is sourced from simulation comparisons between the installation bolts for the VZ Series propellers and those for the V Series propellers.
? The test data presented above were obtained under specific conditions, using equipment within our company's laboratory. Actual data and parameters may vary slightly depending on the test environment, platform, software, and other factors.
Technical Drawing
Specification Export to Excel
Diameter (Inch)
40.1(1018.5mm)
Material
Resin-basedCarbonFiberComposite+PMIFoamCore
Pitch (Inch)
16.1(408.9mm)
Surface Treatment
Matte
AverageSingleblade Weight (g)
205
Type
One-Piece Straight Propeller
RecommendedMax RPM (RPM)
3900
Application
VTOL Fixed-Wing UAVs, Multicopter Mode
RecommendedMax Thrust (kg)
48
Connections & Dimensions
Flange Mount, Ø12 mm Center Hole, Ø30 mm Bolt Circle, with 4x Ø5 mm Mounting Holes
Limit RPM (RPM)
4350
Recommendations
Recommended Solution：VL1155 KV65+VL200A
Limit Thrust (kg)
60
Test Data Export to Excel
Ambient Temperature 22 °C Altitude 25 m
RPM (RPM)
Torque （N·m)
RecommendedThrust （gf）
Output Power （W）
Effciency （gf/W）
vz40x16.1-draw.png
1550
3.45
7219
560.23
12.89
1750
4.43
9244
811.21
11.40
1950
5.53
11551
1129.87
10.22
2150
6.77
14141
1524.47
9.28
2350
8.14
17013
2003.27
8.49
2550
9.64
20167
2574.53
7.83
2750
11.27
23603
3246.50
7.27
2950
13.04
27322
4027.45
6.78
3150
14.93
31324
4925.64
6.36
3350
16.96
35607
5949.31
5.99
3550
19.12
40174
7106.74
5.65
3750
21.41
45022
8406.17
5.36
3950
23.83
50153
9855.88
5.09
4150
26.38
55566
11464.10
4.85
4350
29.06
61261
13239.12
4.63
Important Notes
Data may vary under different testing standards due to factors such as equipment, methodology, and environment. Ensure compatibility between the propeller mounting holes and motors. Refer to the drawing above for details.
Packing List
T-Motor VZ41.5x15.2 VTOL 41.5 Zoll Carbon Propeller 1x CW 1x CCW
Artikelnr.: PM-7274 | HAN: VZ41.5x15.2
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VZ SERIES -VTOL PROPELLERS
Break through the performance limitations of traditional multi-rotor propellers. VZ series propellers deliver superior power, durability, and lightweight design for VTOL applications
What Does a VTOL Propeller Need?
High Strength High Stiffness & Lightweight Design
High Strength
Withstands immense centrifugal loads and maneuver-induced alternating loads at high RPM, preventing structural failure
High Stiffness
Ensures safe blade-tip clearance in compact layouts, suppresses aeroelastic deformation, and prevents flutter
Lightweight Design
Reduce the moment of inertia to achieve rapid thrust response and higher attitude control bandwidth for the flight control system
Superior Aerodynamic Design
The unique dual operational modes of VTOL—vertical takeoff/landing and cruise—demand new propeller capabilities
Vertical Takeoff & Landing Phase
Requiring high thrust and power, demanding maximum lift output from the propeller disk within a limited blade area
Cruise Phase
When the propeller stops rotating, it is necessary to minimize profile drag to reduce power consumption, achieving "stealthy" low-drag efficiency
Transition Stability: Resisting Complex Flow Field Interference
The extreme challenges posed by high angle of attack, low speed and unsteady flow field, coupled with the insufficient strength and poor transition stability of traditional blades, make this an accident-prone region
Unsteady Flow Fields at High Angle of Attack
The aircraft operates at high angles of attack and low speeds within an extremely complex flow environment
Asymmetric Airflow
Significant angle between incoming flow and the rotation axis causes asymmetric airflow entering the propeller disc
Severe Periodic Variations
Local forces on the blade fluctuate drastically per rotation, inducing flutter and causing significant thrust fluctuation
To address the challenges of traditional propellers in VTOL (Vertical Takeoff and Landing mode) applications
we introduce the VZ Series Propellers
Technical Features of the VZ Series Propellers
Advanced composite materials and exceptional aerodynamic design work in synergy to ensure consistently efficient, reliable, and controllable power output
Bending & Torsion Resistant Layup Design
Optimized fiber orientation and ratio maximize strength and stiffness
Prepreg Compression Molding for Integrated Forming
Product porosity below 1%, ensuring stable and reliable quality
PMI Foam Core
Lightweight, high-strength core material effectively increases stiffness while controlling total weight
30%
Flexural Strength
Significantly enhanced impact resistance and deformation resistance for greater durability in complex operating conditions
20%
Torsional Stiffness
Optimized power transmission efficiency reduces energy loss during operation
Blade Root Optimization: Safety Redundancy Design
The blade root thickness is optimized to provide structural redundancy while reducing loads on the connecting bolts
V30 Propeller
VZ30 Propeller
Aerodynamic Priority: Engineered for High VTOL Thrust
Dedicated High Lift-to- Drag Ratio Airfoil
Optimized for VTOL conditions to enhance maximum lift coefficient
Low-Drag Cruise Blade Shape
Improved aerodynamic blade boundaries reduce cruise drag
Specialized Blade Tip
Optimized tip design weakens vortex strength and enhances flight quality
Custom VTOL Propeller Service: 10 to 100 Inches
Supports precise matching with various pitch specifications and motors Full in-house R&D ensures stable and controllable quality
Aerodynamic/Structural Design
Mold Manufacturing
Composite Molding
Testing & Validation
? The appearance diagrams and product renderings in this document are for reference only; the actual product shall prevail.
? Data regarding improvements in flexural strength and torsional stiffness are derived from comparative testing between the VZ Series propeller and the G Series propellers.
? Data regarding the reduction in bolt shear load is sourced from simulation comparisons between the installation bolts for the VZ Series propellers and those for the V Series propellers.
? The test data presented above were obtained under specific conditions, using equipment within our company's laboratory. Actual data and parameters may vary slightly depending on the test environment, platform, software, and other factors.
Technical Drawing
Specification Export to Excel
Diameter (Inch)
41.5(1054.1mm)
Material
Resin-basedCarbonFiberComposite+PMIFoamCore
Pitch (Inch)
15.2(386.1mm)
Surface Treatment
Matte
AverageSingleblade Weight (g)
268
Type
One-Piece Straight Propeller
RecommendedMax RPM (RPM)
4000
Application
VTOL Fixed-Wing UAVs, Multicopter Mode
RecommendedMax Thrust (kg)
51
Connections & Dimensions
Flange Mount, Ø12 mm Center Hole, Ø30 mm Bolt Circle, with 4x Ø5 mm Mounting Holes
Limit RPM (RPM)
4460
Recommendations
Limit Thrust (kg)
64
Test Data Export to Excel
Ambient Temperature 22 °C Altitude 25 m
RPM (RPM)
Torque （N·m)
RecommendedThrust （gf）
Output Power （W）
力Effciency （gf/W）
vz41.5x15.2-draw.png
1660
4.06
8692
705.75
12.32
1860
5.07
10877
988.08
11.01
2060
6.21
13333
1340.71
9.94
2260
7.49
16061
1771.75
9.07
2460
8.89
19061
2289.32
8.33
2660
10.42
22333
2901.53
7.70
2860
12.08
25876
3616.51
7.15
3060
13.86
29691
4442.36
6.68
3260
15.78
33777
5387.20
6.27
3460
17.83
38135
6459.16
5.90
3660
20.00
42765
7666.33
5.58
3860
22.31
47667
9016.85
5.29
4060
24.74
52841
10518.83
5.02
4260
27.30
58286
12180.38
4.79
4460
30.00
64002
14009.62
4.57
Important Notes
Data may vary under different testing standards due to factors such as equipment, methodology, and environment. Ensure compatibility between the propeller mounting holes and motors. Refer to the drawing above for details.
Packing List
T-Motor VZ42x16.5 VTOL 42 Zoll Carbon Propeller 1x CW 1x CCW
Artikelnr.: PM-7275 | HAN: VZ42x16.5
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VZ SERIES -VTOL PROPELLERS
Break through the performance limitations of traditional multi-rotor propellers. VZ series propellers deliver superior power, durability, and lightweight design for VTOL applications
What Does a VTOL Propeller Need?
High Strength High Stiffness & Lightweight Design
High Strength
Withstands immense centrifugal loads and maneuver-induced alternating loads at high RPM, preventing structural failure
High Stiffness
Ensures safe blade-tip clearance in compact layouts, suppresses aeroelastic deformation, and prevents flutter
Lightweight Design
Reduce the moment of inertia to achieve rapid thrust response and higher attitude control bandwidth for the flight control system
Superior Aerodynamic Design
The unique dual operational modes of VTOL—vertical takeoff/landing and cruise—demand new propeller capabilities
Vertical Takeoff & Landing Phase
Requiring high thrust and power, demanding maximum lift output from the propeller disk within a limited blade area
Cruise Phase
When the propeller stops rotating, it is necessary to minimize profile drag to reduce power consumption, achieving "stealthy" low-drag efficiency
Transition Stability: Resisting Complex Flow Field Interference
The extreme challenges posed by high angle of attack, low speed and unsteady flow field, coupled with the insufficient strength and poor transition stability of traditional blades, make this an accident-prone region
Unsteady Flow Fields at High Angle of Attack
The aircraft operates at high angles of attack and low speeds within an extremely complex flow environment
Asymmetric Airflow
Significant angle between incoming flow and the rotation axis causes asymmetric airflow entering the propeller disc
Severe Periodic Variations
Local forces on the blade fluctuate drastically per rotation, inducing flutter and causing significant thrust fluctuation
To address the challenges of traditional propellers in VTOL (Vertical Takeoff and Landing mode) applications
we introduce the VZ Series Propellers
Technical Features of the VZ Series Propellers
Advanced composite materials and exceptional aerodynamic design work in synergy to ensure consistently efficient, reliable, and controllable power output
Bending & Torsion Resistant Layup Design
Optimized fiber orientation and ratio maximize strength and stiffness
Prepreg Compression Molding for Integrated Forming
Product porosity below 1%, ensuring stable and reliable quality
PMI Foam Core
Lightweight, high-strength core material effectively increases stiffness while controlling total weight
30%
Flexural Strength
Significantly enhanced impact resistance and deformation resistance for greater durability in complex operating conditions
20%
Torsional Stiffness
Optimized power transmission efficiency reduces energy loss during operation
Blade Root Optimization: Safety Redundancy Design
The blade root thickness is optimized to provide structural redundancy while reducing loads on the connecting bolts
V30 Propeller
VZ30 Propeller
Aerodynamic Priority: Engineered for High VTOL Thrust
Dedicated High Lift-to- Drag Ratio Airfoil
Optimized for VTOL conditions to enhance maximum lift coefficient
Low-Drag Cruise Blade Shape
Improved aerodynamic blade boundaries reduce cruise drag
Specialized Blade Tip
Optimized tip design weakens vortex strength and enhances flight quality
Custom VTOL Propeller Service: 10 to 100 Inches
Supports precise matching with various pitch specifications and motors Full in-house R&D ensures stable and controllable quality
Aerodynamic/Structural Design
Mold Manufacturing
Composite Molding
Testing & Validation
? The appearance diagrams and product renderings in this document are for reference only; the actual product shall prevail.
? Data regarding improvements in flexural strength and torsional stiffness are derived from comparative testing between the VZ Series propeller and the G Series propellers.
? Data regarding the reduction in bolt shear load is sourced from simulation comparisons between the installation bolts for the VZ Series propellers and those for the V Series propellers.
? The test data presented above were obtained under specific conditions, using equipment within our company's laboratory. Actual data and parameters may vary slightly depending on the test environment, platform, software, and other factors.
Technical Drawing
Specification Export to Excel
Diameter (Inch)
42.2(1071.9mm)
Material
Resin-basedCarbonFiberComposite+PMIFoamCore
Pitch (Inch)
16.5(419.1mm)
Surface Treatment
Matte
AverageSingleblade Weight (g)
273
Type
One-Piece Straight Propeller
RecommendedMax RPM (RPM)
3970
Application
VTOL Fixed-Wing UAVs, Multicopter Mode
RecommendedMax Thrust (kg)
52.8
Connections & Dimensions
Flange Mount, Ø12 mm Center Hole, Ø30 mm Bolt Circle, with 4x Ø5 mm Mounting Holes
Limit RPM (RPM)
4460
Recommendations
Recommended Solution：V13L KV65+THUNDER 200A 24S/VL1165 KV60+VL200A
Limit Thrust (kg)
66
Test Data Export to Excel
Ambient Temperature 22 °C Altitude 25 m
RPM (RPM)
Torque （N·m)
RecommendedThrust （gf）
Output Power （W）
力Effciency （gf/W）
vz42x16.5-draw.png
1660
4.66
9375
810.21
11.57
1860
5.75
11852
1120.44
10.58
2060
6.98
14572
1505.47
9.68
2260
8.34
17535
1973.76
8.88
2460
9.84
20742
2533.78
8.19
2660
11.47
24192
3194.00
7.57
2860
13.23
27886
3962.90
7.04
3060
15.13
31823
4848.92
6.56
3260
17.17
36003
5860.55
6.14
3460
19.34
40427
7006.25
5.77
3660
21.64
45094
8294.49
5.44
3860
24.08
50005
9733.74
5.14
4060
26.65
55159
11332.46
4.87
4260
29.36
60556
13099.12
4.62
4460
32.21
66197
15042.19
4.40
Important Notes
Data may vary under different testing standards due to factors such as equipment, methodology, and environment. Ensure compatibility between the propeller mounting holes and motors. Refer to the drawing above for details.
Packing List
T-Motor VZ45x18 VTOL 45 Zoll Carbon Propeller 1x CW 1x CCW
Artikelnr.: PM-7276 | HAN: VZ45x18
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VZ SERIES -VTOL PROPELLERS
Break through the performance limitations of traditional multi-rotor propellers. VZ series propellers deliver superior power, durability, and lightweight design for VTOL applications
What Does a VTOL Propeller Need?
High Strength High Stiffness & Lightweight Design
High Strength
Withstands immense centrifugal loads and maneuver-induced alternating loads at high RPM, preventing structural failure
High Stiffness
Ensures safe blade-tip clearance in compact layouts, suppresses aeroelastic deformation, and prevents flutter
Lightweight Design
Reduce the moment of inertia to achieve rapid thrust response and higher attitude control bandwidth for the flight control system
Superior Aerodynamic Design
The unique dual operational modes of VTOL—vertical takeoff/landing and cruise—demand new propeller capabilities
Vertical Takeoff & Landing Phase
Requiring high thrust and power, demanding maximum lift output from the propeller disk within a limited blade area
Cruise Phase
When the propeller stops rotating, it is necessary to minimize profile drag to reduce power consumption, achieving "stealthy" low-drag efficiency
Transition Stability: Resisting Complex Flow Field Interference
The extreme challenges posed by high angle of attack, low speed and unsteady flow field, coupled with the insufficient strength and poor transition stability of traditional blades, make this an accident-prone region
Unsteady Flow Fields at High Angle of Attack
The aircraft operates at high angles of attack and low speeds within an extremely complex flow environment
Asymmetric Airflow
Significant angle between incoming flow and the rotation axis causes asymmetric airflow entering the propeller disc
Severe Periodic Variations
Local forces on the blade fluctuate drastically per rotation, inducing flutter and causing significant thrust fluctuation
To address the challenges of traditional propellers in VTOL (Vertical Takeoff and Landing mode) applications
we introduce the VZ Series Propellers
Technical Features of the VZ Series Propellers
Advanced composite materials and exceptional aerodynamic design work in synergy to ensure consistently efficient, reliable, and controllable power output
Bending & Torsion Resistant Layup Design
Optimized fiber orientation and ratio maximize strength and stiffness
Prepreg Compression Molding for Integrated Forming
Product porosity below 1%, ensuring stable and reliable quality
PMI Foam Core
Lightweight, high-strength core material effectively increases stiffness while controlling total weight
30%
Flexural Strength
Significantly enhanced impact resistance and deformation resistance for greater durability in complex operating conditions
20%
Torsional Stiffness
Optimized power transmission efficiency reduces energy loss during operation
Blade Root Optimization: Safety Redundancy Design
The blade root thickness is optimized to provide structural redundancy while reducing loads on the connecting bolts
V30 Propeller
VZ30 Propeller
Aerodynamic Priority: Engineered for High VTOL Thrust
Dedicated High Lift-to- Drag Ratio Airfoil
Optimized for VTOL conditions to enhance maximum lift coefficient
Low-Drag Cruise Blade Shape
Improved aerodynamic blade boundaries reduce cruise drag
Specialized Blade Tip
Optimized tip design weakens vortex strength and enhances flight quality
Custom VTOL Propeller Service: 10 to 100 Inches
Supports precise matching with various pitch specifications and motors Full in-house R&D ensures stable and controllable quality
Aerodynamic/Structural Design
Mold Manufacturing
Composite Molding
Testing & Validation
? The appearance diagrams and product renderings in this document are for reference only; the actual product shall prevail.
? Data regarding improvements in flexural strength and torsional stiffness are derived from comparative testing between the VZ Series propeller and the G Series propellers.
? Data regarding the reduction in bolt shear load is sourced from simulation comparisons between the installation bolts for the VZ Series propellers and those for the V Series propellers.
? The test data presented above were obtained under specific conditions, using equipment within our company's laboratory. Actual data and parameters may vary slightly depending on the test environment, platform, software, and other factors.
Technical Drawing
Specification Export to Excel
Diameter (Inch)
45(1143mm)
Material
Resin-basedCarbonFiberComposite+PMIFoamCore
Pitch (Inch)
18(457.2mm)
Surface Treatment
Matte
AverageSingleblade Weight (g)
285
Type
One-Piece Straight Propeller
RecommendedMax RPM (RPM)
3380
Application
VTOL Fixed-Wing UAVs, Multicopter Mode
RecommendedMax Thrust (kg)
60
Connections & Dimensions
Flange Mount, Ø14 mm Center Hole, Ø34 mm Bolt Circle, with 6x Ø5 mm Mounting Holes
Limit RPM (RPM)
3780
Recommendations
Recommended Solution：VL1180 KV60+VL300A/VL1380 KV60+VL300A
Limit Thrust (kg)
75
Test Data Export to Excel
Ambient Temperature 22 °C Altitude 25 m
RPM (RPM)
Torque （N·m)
RecommendedThrust （gf）
Output Power （W）
力Effciency （gf/W）
vz45x18-draw.png
980
2.76
5122
282.97
18.10
1180
3.85
7303
475.43
15.36
1380
5.18
9919
749.17
13.24
1580
6.77
12969
1119.67
11.58
1780
8.60
16455
1602.41
10.27
1980
10.67
20375
2212.89
9.21
2180
12.99
24731
2966.58
8.34
2380
15.56
29522
3878.98
7.61
2580
18.38
34747
4965.55
7.00
2780
21.44
40408
6241.80
6.47
2980
24.75
46504
7723.20
6.02
3180
28.30
53034
9425.23
5.63
3380
32.10
60000
11363.39
5.28
3580
36.15
67400
13553.15
4.97
3780
40.45
75236
16010.00
4.70
Important Notes
Data may vary under different testing standards due to factors such as equipment, methodology, and environment. Ensure compatibility between the propeller mounting holes and motors. Refer to the drawing above for details.
Packing List
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