TMOTOR VL1032 Drone Power System Kit

Description

VL1032 Power System for VTOL Drones

Core Overview

The VL1032 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, in a quadrotor configuration, is recommended for a takeoff weight of 50~55kg, with a maximum single-axis thrust of 31.7kg. 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.

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 50~55kg to match its single-axis maximum thrust of 31.7kg 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) 220A” and “Maximum Continuous Current 120A” 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	VL1032
Magnet Temperature Rating	180
Motor Dimensions	109.6 * 56mm
Wire Gauge * Length	Enameled Wire 150mm
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	15mg
Bearing Model	Imported 6901 Bearing
Protection Level	IPX5
Centrifugal Cooling	Yes
Package Dimensions	190 * 140 * 80mm
Model	VL1032
KV (RPM/V)	180
Recommended Battery	12S
No-load Current (15V)	4.6A
Internal Resistance (25)	6.5m
Maximum Current	200A
Maximum Continuous Power	2537W
Operating Environment Temp.	-30~55
Maximum Thrust	31.7kg
Motor Weight (with wires)	1090g

ESC Parameters

Parameter Item	Parameter Value
Model	V200A
Control Method	PWM / CAN
Maximum Voltage	60V
Communication Method	DRONE CAN / UAV CAN
Maximum Current (10s)	220A (under certain cooling conditions)
Propeller Braking Method	Electronic Braking
Maximum Continuous Current	120A (under certain cooling conditions)
Encoder Wire	Shielded Wire-Black-24AWG-5C -42010mm-M6 Aviation Plug
Standby Power Consumption	50mA
Output Wire	Silicone Wire-Orange-14AWG -21010mm
Throttle Range	1100~1940us (Fixed)
Input Wire	Silicone Wire-Red/Black-12AWG -114010mm
Signal Wire	Shielded Wire-Black-OD4.2-5C -77010mm-JP-3P*2 Black White Empty Green Yellow Gray
Throttle Response Time	300ms
Weight (with wires)	49510g

Propeller Parameters

Parameter Item	Parameter Value
Model	G30 * 10.5 inch (762 * 266.7mm)
Weight	975g

VL1032 Kit Test Data Tables

VL1032 Kit Test Data (VL1032 KV180 V200A 14S + G30 * 10.5, Test Voltage 44V)

Throttle	Voltage (V)	Thrust (g)	Torque (N*m)	Current (A)	RPM	Power (W)	Efficiency (g/W)
40%	45.00	5977	2.04	15.95	2628	718	8.33
42%	44.95	6656	2.25	18.31	2754	823	8.09
44%	44.90	7338	2.48	20.85	2881	936	7.84
46%	44.86	7960	2.69	23.50	3009	1054	7.56
48%	44.81	8696	2.94	26.50	3131	1188	7.32
50%	44.78	9420	3.19	29.72	3249	1331	7.08
52%	44.75	10124	3.43	33.02	3369	1478	6.85
54%	44.71	10979	3.71	36.81	3483	1646	6.67
56%	44.66	11696	3.96	40.50	3596	1809	6.47
58%	44.61	12520	4.24	44.62	3706	1990	6.30
60%	44.55	13324	4.51	48.96	3813	2181	6.11
62%	44.49	14151	4.79	53.52	3918	2381	5.94
64%	44.43	14906	5.07	58.12	4021	2582	5.78
66%	44.36	15696	5.35	63.00	4120	2795	5.61
68%	44.31	16490	5.62	68.11	4220	3018	5.46
70%	44.25	17241	5.90	73.31	4318	3244	5.32
80%	44.11	21279	7.33	103.16	4763	4550	4.68
90%	44.63	25317	8.76	140.00	5157	6248	4.05
100%	43.32	29275	10.21	192.07	5519	8321	3.52

Note: Motor temperature 77 is the motor case temperature after running at 44.4V, 75% throttle for 10 minutes.

VL1032 Kit Test Data (VL1032 KV180 V200A 14S + G30 * 10.5, Test Voltage 50V)

Throttle (%)	Voltage (V)	Thrust (g)	Torque (Nm)	Current (A)	RPM	Power (W)	Efficiency (g/W)
40%	50.49	7686	2.61	20.02	2967	1011	7.61
42%	50.45	8540	2.90	23.03	3107	1162	7.35
44%	50.41	9311	3.16	26.11	3244	1316	7.07
46%	50.37	10181	3.46	29.60	3381	1491	6.83
48%	50.32	11078	3.76	33.33	3512	1677	6.61
50%	50.27	12003	4.07	37.34	3641	1877	6.39
52%	50.21	12854	4.37	41.44	3768	2081	6.18
54%	50.15	13784	4.69	45.93	3891	2303	5.99
56%	50.08	14711	5.01	50.66	4010	2537	5.80
58%	49.99	15689	5.36	55.84	4131	2791	5.62
60%	49.94	16654	5.67	61.00	4244	3046	5.47
62%	49.88	17561	6.00	66.40	4357	3312	5.30
64%	49.80	18478	6.32	71.95	4465	3583	5.16
66%	49.74	19373	6.65	77.78	4570	3869	5.01
68%	49.69	20350	6.99	84.05	4669	4176	4.87
70%	49.65	21251	7.31	90.37	4767	4487	4.74
80%	49.49	25745	8.93	125.79	5213	6225	4.14
90%	49.52	29924	10.46	170.12	5588	8423	3.55
100%	48.51	31766	11.11	201.10	5729	9756	3.26

Frequently Asked Questions (FAQ)

Q: What is the main application scenario for the VL1032 power system kit?

A: This kit is specifically designed for Vertical Take-Off and Landing (VTOL) unmanned aerial vehicles. It is particularly suitable for heavy-duty VTOL fixed-wing or multi-rotor drones with a takeoff weight of 50~55kg 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 120A (under certain cooling conditions)” in the ESC parameters?

A: This means the ESC can stably output 120A 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.

Q: How reliable is the VL series power system?

A: The VL series power system design emphasizes durability, with a service life exceeding 10,000 flights, aiming to ensure long-term stable and reliable performance. The VL1032, as a product of this series, inherits this high-reliability design philosophy, providing lasting power assurance for professional-level applications.