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Effects of Freeplay on Aircraft Main Landing Gear Stability

机译:自由活动对飞机主起落架稳定性的影响

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A study is made into the occurrence of shimmy oscillations in a dual-wheel main landing gear system. Nonlinear equations of motion are developed for the system and various nonlinear effects are considered including gyroscopic coupling, nonlinear tyre properties, geometric nonlinearities and fluid damping. Of particular interest in this study is the presence of freeplay - this is introduced as a lateral play at the apex of the torque link joints. Using bifurcation analysis methods, the dynamics of this system are explored as the forward velocity and loading force acting on the gear are varied. For the zero freeplay case the system is found to be stable over its realistic operating range with shimmy oscillations appearing only for extreme loading forces and speed. However, with the introduction of freeplay, shimmy may be observed over more typical operating conditions and the resulting oscillations are found to scale linearly with freeplay magnitude. Using numerical continuation, the (V, F_z) parameter plane is further subdivided into areas of different shimmy dynamics. With the inclusion of freeplay the variety of observed behaviour is shown to increase with the appearance of low and high frequency shimmy, bi-stable behaviour and stationary solutions of non-zero yaw.
机译:对双轮主起落架系统中摆振的发生进行了研究。为该系统开发了非线性运动方程,并考虑了各种非线性影响,包括陀螺耦合,轮胎非线性特性,几何非线性和流体阻尼。在这项研究中特别感兴趣的是自由游隙的存在-这种自由游隙是作为扭矩游隙接头顶点处的横向游隙引入的。使用分叉分析方法,随着前进速度和作用在齿轮上的加载力的变化,探索了该系统的动力学特性。对于零自由运行的情况,发现该系统在其实际工作范围内是稳定的,仅在极高的加载力和速度下才会出现颤动振荡。然而,随着自由播放的引入,在更典型的工作条件下可能会观察到摆振现象,并且发现产生的振荡随自由播放幅度成线性比例变化。使用数值连续性,(V,F_z)参数平面可进一步细分为具有不同摆振动力学的区域。随着自由播放的加入,所观察到的行为的多样性随着低频和高频摆线,双稳态行为以及非零偏航的固定解的出现而增加。

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