Cockpit control system and method

The invention discloses a cockpit control system and method and belongs to the technical field of helicopters. The system comprises a dustproof device, a balance device, a friction device, a control damper, a parallel steering engine, a support assembly, a joystick, an action command transmission de...

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Bibliographic Details
Main Authors SUN CHONG, HE CHENFEI, ZHAO LIANG, FENG HANG, DENG HAIXIA, XU YOUSONG, WANG XIAOYANG
Format Patent
LanguageChinese
English
Published 31.05.2017
Subjects
AEROPLANES
AIRCRAFT
AVIATION
COSMONAUTICS
HELICOPTERS
PERFORMING OPERATIONS
TRANSPORTING
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Summary:The invention discloses a cockpit control system and method and belongs to the technical field of helicopters. The system comprises a dustproof device, a balance device, a friction device, a control damper, a parallel steering engine, a support assembly, a joystick, an action command transmission device, a command sensor and a flight control computer. The action command transmission device is composed of a linkage twisting shaft, a pull rod assembly and a rocker arm assembly. The linkage twisting shaft is sleeved with the balance device and the friction device in a connected manner. The control damper and the parallel steering engine are connected to the linkage twisting shaft through first pull rods and first rocker arms. The joystick is fixed to the support assembly through one end of an input end rocker arm. The other end of the input end rocker arm is connected with the linkage twisting shaft through a first pull rod. The command sensor is connected with the linkage twisting shaft through an output end pu
Bibliography:Application Number: CN201611083124