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TMOTOR VL8015 Drone Power System Kit

  • $115.00
  • $1,346.00
  • Availibility: In Stock

VL8015 Power System for VTOL Drones Core Overview The VL8015 is a member of the T-MOTOR VL series power system, specifically designed for the rotor power needs of Vertical Take-Off and Landing (VTOL) unmanned aerial vehicles. The kit includes the VL8015 mo

SKU:  MVX3196055070 Category:
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VL8015 Power System for VTOL Drones

Core Overview

The VL8015 is a member of the T-MOTOR VL series power system, specifically designed for the rotor power needs of Vertical Take-Off and Landing (VTOL) unmanned aerial vehicles. The kit includes the VL8015 motor, V80A ESC, and G26 * 8.5-inch propellers, and is recommended for a takeoff weight of 25kg in a quadrotor configuration, with a maximum single-axis thrust of 14.8kg. It provides stable, intelligent vertical takeoff and landing power for VTOL fixed-wing or multi-rotor drones, ensuring flight safety throughout all phases from takeoff, mode transition, to landing.

Core Technology Advantages

Built for VTOL Fixed-Wing: Mag-Coded Prop Braking, Energy-Saving, Reliable

Fast (Second-Level Braking): Supports 360 customizable angle propeller braking, effectively avoiding airflow disturbance caused by rotor rotation, ensuring the aerodynamic layout of the fixed-wing aircraft is unaffected, thereby enhancing flight safety.

Economical (Adaptive Braking): According to changes in external force, the ESC automatically adjusts the current to control the braking torque, reducing power consumption and heat generation, achieving energy-saving effects.

FOC Vector Control

Adopts FOC (Field-Oriented Control) technology, achieving more delicate and precise control, thereby ensuring highly stable power output, offering comprehensive advantages of responsive, precise control, efficient drive, and low-noise operation.

Small Thrust Drop Ratio Under Voltage Drop

In the face of voltage drop, it can maintain small thrust fluctuations, demonstrating excellent stability. This keeps the throttle increase amplitude at a lower level, thus providing larger control redundancy, significantly improving safety during landing.

Supports CAN2.0 Protocol, Intelligent and Convenient

Plug and Play: This ESC supports the DroneCAN/CAN2.0 protocol, fully compatible with the PX4 flight control system, offering plug-and-play convenience.

Remote Monitoring: Remote real-time monitoring of the ESC’s working status through the flight control system ensures the system is always in optimal working condition.

Easy Setup: Users do not need to perform complicated settings, saving time and effort, making the device easier to operate.

Usage Recommendations

  • Accurate Model and Weight Matching: This kit is designed for VTOL drones. In a quadrotor configuration, strictly control the entire aircraft’s takeoff weight within the recommended range of 25kg to match its single-axis maximum thrust of 14.8kg and ensure a safety margin.
  • Must Use CAN Bus Connection: To obtain all intelligent functions such as remote monitoring and fast propeller braking, it is necessary to use the CAN bus to connect to a flight controller (such as PX4) that supports the DroneCAN/CAN2.0 protocol. PWM mode can be used as a backup.
  • Pay Attention to Cooling Conditions: Both the “Maximum Current (10s) 80A” and “Maximum Continuous Current 40A” in the ESC parameters are marked as achieved “under certain cooling conditions.” Ensure the power system is installed in a well-ventilated location within the aircraft; otherwise, continuous performance will be compromised, and lifespan will be affected.
  • Make Good Use of Propeller Braking: For VTOL fixed-wing aircraft, make full use of its 360 propeller braking function. After transitioning to fixed-wing mode, locking the propellers in the direction of least drag can significantly improve aerodynamic efficiency and endurance.

Product Parameters

Basic Parameters

Parameter Item Parameter Value
Motor Model VL8015
Magnet Temperature Rating 180
Motor Dimensions 88.8 * 42mm
Wire Gauge * Length Silicone Wire 14# 1000mm
Stator Process 150 High-Temperature Coating
Enameled Wire Temp. Rating 220
Slot/Pole Count 24N28P
Coil Withstand Voltage 1000V/5s
Shaft Diameter IN:12mm OUT:10mm
Rotor Dynamic Balance Standard 10mg
Bearing Model Imported 6901 Bearing
Protection Level IPX5
Centrifugal Cooling Yes
Package Dimensions 150 * 120 * 57mm
Model VL8015
KV (RPM/V) 170
Recommended Battery 12S
No-load Current (15V) 1.9A
Internal Resistance (25) 43m
Maximum Current 74A
Maximum Continuous Power 1045W
Operating Environment Temp. -30~55
Maximum Thrust 14.8kg
Motor Weight (with wires) 610g

ESC Parameters

Parameter Item Parameter Value
Model V80A
Maximum Voltage 60V
Maximum Current (10s) 80A (under certain cooling conditions)
Maximum Continuous Current 40A (under certain cooling conditions)
Standby Power Consumption 50mA
Throttle Range 1040~1940us (Fixed)
Throttle Refresh Rate 50~500Hz
Throttle Response Time 300ms
Control Method PWM / CAN
Communication Method DRONE CAN / UAV CAN
Propeller Braking Method Electronic Braking
Encoder Wire -45010mm-M6 Aviation Plug
-45010mm-24AWG-5C
Output Wire Silicone Wire-Orange-14AWG-11010mm
Input Wire Silicone Wire-Red/Black-12AWG-18010mm
Signal Wire Silicone Wire-Black/Red-12AWG-18010mm
Shielded Wire-Black-OD4.2-5C-45010mm-JP-3P*2-Black White Green Yellow Gray
Weight (with wires) 110g

Propeller Parameters

Parameter Item Parameter Value
Model G26 * 8.5 inch (660.4 * 215.9mm)
Weight 685g

VL8015 Kit Test Data Tables

VL8015 Kit Test Data Table (Test Voltage 44V)

Throttle Voltage (V) Thrust (g) Torque (N*m) Current (A) RPM Power (W) Efficiency (g/W) Motor Temp. ()
40% 44.59 2944 0.89 6.53 2450 291 10.11
42% 44.60 3249 0.98 7.48 2575 334 9.74
44% 44.60 3558 1.07 8.50 2696 379 9.38
46% 44.60 3879 1.17 9.62 2817 429 9.04
48% 44.61 4216 1.26 10.85 2935 484 8.72
50% 44.61 4575 1.37 12.17 3052 543 8.43
52% 44.62 4962 1.47 13.62 3167 608 8.16
54% 44.62 5354 1.59 15.17 3278 677 7.91
56% 44.64 5726 1.70 16.77 3391 748 7.65
58% 44.64 6121 1.82 18.53 3503 827 7.40
60% 44.63 6509 1.93 20.32 3617 907 7.18
62% 44.62 6920 2.05 22.23 3726 992 6.98
64% 44.61 7329 2.17 24.26 3835 1082 6.77
66% 44.60 7762 2.29 26.47 3940 1180 6.58
68% 44.59 8178 2.42 28.73 4044 1281 6.38
70% 44.57 8615 2.55 31.20 4145 1391 6.20
80% 44.37 10932 3.23 45.81 4635 2032 5.38
90% 44.04 13323 3.95 65.64 5093 2891 4.61
100% 43.77 14233 4.23 84.17 5278 3684 3.86

VL8015 Kit Test Data Table (Test Voltage 50V)

Throttle Voltage (V) Thrust (g) Torque (N*m) Current (A) RPM Power (W) Efficiency (g/W)
40% 50.33 3722 1.10 7.98 2742 402 9.26
42% 50.34 4099 1.21 9.17 2876 462 8.88
44% 50.37 4499 1.33 10.48 3010 528 8.52
46% 50.39 4916 1.45 11.88 3141 599 8.21
48% 50.40 5364 1.58 13.44 3268 678 7.92
50% 50.41 5787 1.70 15.04 3398 758 7.63
52% 50.43 6228 1.83 16.80 3523 847 7.35
54% 50.43 6683 1.97 18.66 3648 941 7.10
56% 50.44 7173 2.11 20.71 3771 1045 6.87
58% 50.43 7646 2.25 22.78 3891 1149 6.65
60% 50.43 8136 2.39 25.08 4008 1265 6.43
62% 50.42 8616 2.53 27.45 4129 1384 6.23
64% 50.40 9103 2.68 29.97 4244 1511 6.03
66% 50.37 9613 2.83 32.66 4355 1645 5.84
68% 50.34 10111 2.98 35.47 4465 1785 5.66
70% 50.30 10607 3.13 38.42 4574 1933 5.49
80% 50.18 12159 3.59 48.39 4876 2428 5.01
90% 50.00 13673 4.04 60.23 5164 3012 4.54
100% 49.80 14842 4.40 73.75 5377 3673 4.04

Frequently Asked Questions (FAQ)

Q: What is the main application scenario for the VL8015 power system kit?

A: This kit is specifically designed for Vertical Take-Off and Landing (VTOL) unmanned aerial vehicles. It is particularly suitable for VTOL fixed-wing or multi-rotor drones with a takeoff weight of 25kg in a quadrotor configuration, providing core power for the vertical takeoff and landing phases.

Q: What exactly does “Mag-Coded Prop Braking” in the promotion mean, and what are the benefits?

A: “Mag-Coded Prop Braking” refers to electronic propeller braking achieved through a magnetic encoder. Its benefits are: 1) Fast: Enables second-level 360 locking at any angle, avoiding rotor airflow interference during cruise; 2) Economical: The ESC can adaptively adjust the braking current, reducing power consumption and heat generation. This enhances the safety and overall efficiency of the VTOL aircraft’s mode transition.

Q: How to understand “Maximum Continuous Current 40A (under certain cooling conditions)” in the ESC parameters?

A: This means the ESC can stably output 40A current for a long period, provided that the cooling conditions are met (e.g., installed in a well-ventilated location). If cooling is insufficient, the continuous current capability will decrease, potentially leading to overheating protection or damage. In the actual aircraft design, sufficient cooling space must be reserved for the ESC.

Q: Should I use PWM or CAN to connect to the flight controller?

A: It is strongly recommended and prioritized to use CAN (DRONE CAN/UAV CAN) connection. The CAN method enables all advanced functions such as remote monitoring, intelligent propeller braking, and provides more reliable communication. PWM mode is only a basic control backup. Using CAN requires ensuring the flight controller (e.g., PX4) supports the corresponding protocol.

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