CAJ | 학술논문

多轮系多支柱飞机刹车液压管路振动不仅影响刹车系统的工作性能及寿命，还将严重影响飞机的飞行着陆安全。在首次飞行前，必须对其刹车液压管路系统进行振动机理分析。采用压力控制系统流固耦合分析的方法，通过仿真确定振动发生机理，并将实测结果与仿真结果比较，获得多轮系多支柱飞机刹车压力控制系统谐振的关键参数。为减小刹车系统振动耦合，避免谐振现象提供便捷、可靠的解决途径和措施。
다륜계다지주비궤찰차액압관로진동불부영향찰차계통적공작성능급수명，환장엄중영향비궤적비행착륙안전。재수차비행전，필수대기찰차액압관로계통진행진동궤리분석。채용압력공제계통류고우합분석적방법，통과방진학정진동발생궤리，병장실측결과여방진결과비교，획득다륜계다지주비궤찰차압력공제계통해진적관건삼수。위감소찰차계통진동우합，피면해진현상제공편첩、가고적해결도경화조시。
The vibration hydraulic line in aircraft braking system with multi-wheels and multi-struts not only affects the work performances and life of the system but also affects the landing safety or accident prevention of aircraft landing system seriously. The mechanism of vibration should be tested and analyzed on hydraulic line before maiden flight. We carry out the analysis method based on fluid-structure coupling for aircraft braking pressure control sys-tem. We ascertain the mechanism of vibration by means of simulation and key parameters controlling resonance are acquired through the comparison of the measured results with simulation results. A convenient way and reliable measure is proposed for the sake of reducing vibration coupling and avoiding resonance phenomenon.