Aircraft foot control mechanism for preventing misoperation of brake

The invention belongs to the field of aircraft control system design, in particular to an aircraft foot control mechanism for preventing the misoperation of a brake. Generally designed to control therudder deflection with left and right foot pedals on the soles of the feet, and to control the wheel...

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Bibliographic Details
Main Authors YANG XI, LYU MING, XU JIAN, CHENG XINGHONG, YANG TAO, HE ZHIGUO, CHE YIBIN, SHI QIANGJUN, HE SONGQING, SHI ZHENLIANG
Format Patent
LanguageChinese
English
Published 18.01.2019
Subjects
AEROPLANES
AIRCRAFT
AVIATION
COSMONAUTICS
HELICOPTERS
PERFORMING OPERATIONS
TRANSPORTING
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Summary:The invention belongs to the field of aircraft control system design, in particular to an aircraft foot control mechanism for preventing the misoperation of a brake. Generally designed to control therudder deflection with left and right foot pedals on the soles of the feet, and to control the wheel brakes with foot pedals on the tips of the feet. Ideally, the brake mechanism and the rudder pedalmechanism operate independently and do not interfere with each other. An aircraft foot control mechanism capable of preventing misoperation of a brake, An upper rock arm of that brake, a pedal rockerarm, a brake tie rod and a low rocker arm of the brake form a parallel four-bar linkage mechanism on the bracket, the lower rocker arm of the brake also has a pullback arm, a pullback spring is arranged between the end of the lower rocker arm of the brake and the bracket, and a torque opposite to the brake direction is applied to the pedal plate during the rotation of the pedal rocker arm; The pedal plate has a pedal plate
Bibliography:Application Number: CN201811114894