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...
Saved in:
Main Authors | , , , , , , |
---|---|
Format | Patent |
Language | Chinese English |
Published |
31.05.2017
|
Subjects | |
Online Access | Get full text |
Cover
Loading…
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 |