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Effects of Freeplay on Dynamic Stability of an Aircraft Main Landing Gear

机译:自由活动对飞机主起落架动态稳定性的影响

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摘要

A study is made into the occurrence of shimmy oscillations in a dual-wheel main landing gear. Nonlinear equations of motion are developed for the system, and various effects are considered, including gyroscopic coupling, nonlinear tire properties, geometric nonlinearities, and fluid shock 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 physical 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. The parameter plane of forward velocity and loading force is then further subdivided into areas of different types of dynamics. With the inclusion of freeplay one observes the appearance of low-frequency and high-frequency shimmy oscillations, bistable behavior, and stationary solutions of nonzero yaw. Considering the desirable case in which no shimmy occurs, the set of allowable freeplay profiles that satisfy a conservative stability criteria is defined.
机译:对双轮主起落架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,并考虑了各种影响,包括陀螺耦合,轮胎非线性特性,几何非线性和流体冲击阻尼。在这项研究中特别感兴趣的是自由游隙的存在:这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,发现该系统在其物理操作范围内是稳定的,而仅在极高的加载力和速度下才会出现摆振。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线性变化。然后将前进速度和加载力的参数平面进一步细分为不同类型的动力学区域。通过包含免费播放,您可以观察到低频和高频摆振,双稳态行为以及非零偏航的固定解的出现。考虑到不发生摆线的理想情况,定义了满足保守稳定性标准的可允许自由播放曲线集。

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