CAJ | 학술논문

飞机刹车系统在其地面试验时，为使得试验状态与实际飞机刹车时状态尽可能接近，刹车系统需要真实的飞机机轮速度传感器输出的速度信号。本设计在不改变机轮速度传感器工作环境、不破坏原有机载设备结构的前提下，为刹车系统提供真实的轮速信号，还原真实的刹车系统工作状态，达到模拟飞机在各种跑道条件下起飞、滑行、着陆、中止起飞过程中机轮转速状态的功能。
비궤찰차계통재기지면시험시，위사득시험상태여실제비궤찰차시상태진가능접근，찰차계통수요진실적비궤궤륜속도전감기수출적속도신호。본설계재불개변궤륜속도전감기공작배경、불파배원유궤재설비결구적전제하，위찰차계통제공진실적륜속신호，환원진실적찰차계통공작상태，체도모의비궤재각충포도조건하기비、활행、착륙、중지기비과정중궤륜전속상태적공능。
The brake system needs speed signal that is input by real wheel speed transducer of aircraft, when it is conducted that ground test of aircraft brake system. The test condition should be similar to condition of actual aircraft brake. This design would not change working condition of wheel speed transducer and structure of original airborne equipment. It provides real wheel speed signal and returns to original working condition of brake system, which simulates function of wheel speed condition during taking-off, taxing, landing and RTO of aircraft in various kinds of runway.