Airborne Electromechanical – Helicopter Hoisting Mechanism
Scope of Application
Designed to meet the requirements of the hoist motor system for the lifting machine project.
Technical Data
The technical solution involves:
1. A brushless DC motor with an encoder; 2. An electrostatic brake with a status switch; 3. A cycloidal gearbox; 4.A cycloidal gearbox;
| Clutch Actuator | Main Motor/Generator | Auxiliary Motor |
| DC Motor | DC Motor | AC Motor |
| Embedded Electronics | Power Supply 200V ~ 400Hz | DALHANDER Winding |
| Hall Effect Sensor | Integrated Resolver | Transmission Ratio 1 / 2.6 |
| Ball Screw Direct Drive Transmission | Epicyclic Gear Ratio 1/3 | Fault - Safe Brake (No Current) |
| Power Supply 24 VDC - 1A | Flywheel | Power Supply 200V ~ 400Hz |
| Stroke 8.6 mm | 2000rpm ~ 8.6N.m ~ 1.8kW | 4000rpm ~ 4.5 N.m ~ 1.9kW |
| Force 1000 N | 4400rpm ~ 2.2N.m ~ 1kW | 1800rpm ~ 4.5N.m 0.9kW |
| Full - stroke Duration 0.5 Seconds | Torque (Static Rotor) = 20N.m | 115×229×267 (mm) |
| 76×76×93 mm | 108×108×193 (mm) | 6.1 kg |
| 1.1 kg | 4.9 kg |
Contact Information
Tel: 18515136109 / 18500199966
Landline: 400 006 2299 ext. 1
Address:Jiayue Plaza, Daxing District, Beijing
