The invention belongs to the technical field of aviation, and discloses an aircraft foot control mechanism assembling method. A process separation surface is designed through a rotating rocker arm anda pedal stand column, the problem of assembling error accumulation between the rotating rocker arm and the pedal stand column is compensated by adjusting the length of an adjustable connector on a rotating pull rod, the adjusting period is greatly shortened, the adjusting time is greatly shortened, and the adjusting efficiency is improved; the wedge-shaped cushion block is added to the rotating rocker arm, so that the adjusting efficiency is greatly improved; through installation and adjustment of the pedal stand column and the foot control fixing support, the axial distance of the structureis guaranteed, the problem that secondary or multiple adjustment of the system is caused by rotation of assemblies such as the pedal stand column around a point is solved, and the adjustment efficiency is greatly improved. In comparison before and after the method is applied, the general adjustment and assembly period can be shortened, and the installation and adjustment efficiency of the foot control mechanism is greatly improved.
本发明属于航空技术领域,公开了一种飞机脚操纵机构装配方法,通过转动摇臂和脚蹬立柱设计了工艺分离面,采取调整转动拉杆上的可调接头长短,补偿转动摇臂与脚蹬立柱之间装配误差累积问题,大幅度减少了调整周期和调整时间,提高了调整效率;通过转动摇臂增加楔形垫块,大幅度提高了调整的效率;通过脚蹬立柱和脚操纵固定支架安装、调整保证结构轴线距离,解决了脚蹬立柱等组合件绕点转动从而引起系统二次或多次调整问题,大幅度提高了调整效率;方法应用前后对比中可以减少一般以上的调整和装配周期,大幅度提高了脚操纵机构的安装、调整效率。
Aircraft foot control mechanism assembling method
一种飞机脚操纵机构装配方法
2020-10-02
Patent
Electronic Resource
Chinese
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / 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 |