The invention belongs to the field of rotor anti-icing and de-icing systems, and discloses a helicopter rotor anti-icing and de-icing electric control system ground verification device and method, and the device comprises an icing signal simulator, a high-speed turntable, a low-speed turntable, a console, a main rotor simulation load and a tail rotor simulation load. The icing signal simulator is connected with the anti-icing and deicing electric control system controller and is used for providing an icing simulation signal; the lower rotary table is used for driving the simulation main propeller hub to rotate, and the high-speed rotary table is used for driving the simulation tail propeller hub to rotate; the console is used for controlling the high-speed turntable and the low-speed turntable; collector rings are arranged on the simulation main rotor and the tail rotor; and the main rotor simulation load and the tail rotor simulation load are connected with the collector ring and are respectively used for simulating the electric power of the main rotor heating subsystem and the tail rotor heating subsystem.
本发明属于旋翼防除冰系统领域,公开了一种直升机旋翼防除冰电控系统地面验证装置及方法,装置包括:结冰信号模拟器、高速转台、低速转台、控制台、主桨模拟负载和尾桨模拟负载;结冰信号模拟器与防除冰电控系统控制器连接,用于提供结冰模拟信号;低于转台用于带动模拟主桨毂转动,高速转台用于带动模拟尾桨毂转动;控制台用于控制高速转台和低速转台;模拟主桨和尾桨上设有集流环;主桨模拟负载和尾桨模拟负载与集流环连接,分别用于模拟主桨、尾桨加热子系统用电功率。
Ground verification device and method for helicopter rotor anti-icing and deicing electric control system
一种直升机旋翼防除冰电控系统地面验证装置及方法
2025-01-03
Patent
Electronic Resource
Chinese
IPC: | B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen |
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