Investigation of Landing Gear Wheel Shimmy Taking into Account Damper Frequency Characteristics

V. S. Metrikin; M. A. Peisel

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Investigation of Landing Gear Wheel Shimmy Taking into Account Damper Frequency Characteristics

机译：考虑减振器频率特性的起落架轮摆振研究

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摘要

A mathematical model and a technique for calculating the rolling motion stability of the damper-equipped landing gear wheel are presented; the dependence of dynamic damper rigidity on frequency found experimentally is used in the investigation. The results of calculating the shimmy boundaries with and without regard for the dependence indicated are given.

机译：提出了一种数学模型和计算装备有减震器的起落架的滚动运动稳定性的技术;在实验中使用了动态阻尼器刚度对频率的依赖关系。给出了考虑或不考虑所示依赖性的匀场边界的计算结果。

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《Russian Aeronautics》 |2009年第2期|共5页
作者
V. S. Metrikin; M. A. Peisel;
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原文格式 PDF
正文语种 eng
中图分类航空;
关键词
Landing gear; Shimmy; Stability; Damper; Amplitude; Frequency; Dynamic rigidity; Wheel rolling;

机译：起落架;摆轮;稳定性;减振器;振幅;频率;动态刚度;车轮滚动;

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专利

1. Investigation of Landing Gear Wheel Shimmy Taking into Account Damper Frequency Characteristics [J] . V. S. Metrikin, M. A. Peisel Russian Aeronautics . 2009,第2期

机译：考虑减振器频率特性的起落架轮摆振研究
2. Experimental characterization of a novel nose landing gear shimmy damper using a small-scale test rig [J] . Mustashin Mir Sakib, Rahmani Mohsen, Behdinan Kamran Aerospace science and technology . 2021,第May期

机译：采用小型试验台新型鼻落齿轮散热器的实验表征
3. On the effectiveness of shimmy dampers in stabilizing nose landing gears [J] . Rahmani Mohsen, Behdinan Kamran Aerospace science and technology . 2019,第Auga期

机译：关于闪光阻尼器在稳定鼻落着陆齿轮的有效性
4. PERFORMANCE ANALYSIS AND PARAMETRIC STUDIES OF NOSE LANDING GEAR SHIMMY DAMPERS [C] . Mohsen Rahmani, Kamran Behdinan ASME international mechanical engineering congress and exposition . 2019

机译：鼻翼起落架减震器的性能分析和参数研究
5. Time Response Simulation for Nose Landing Gear Shimmy Damper Design [D] . Chen, Yang. 2018

机译：鼻落齿轮散流器设计的时间响应仿真
6. Determining Wheel Forces and Moments on Aircraft Landing Gear with a Dynamometer Sensor [O] . Jaroslaw Pytka, Piotr Budzyński, Tomasz Łyszczyk, 2020

机译：使用测力计传感器确定飞机起落架上的车轮力和力矩
7. Influence of Variable Side-Stay Geometry on the Shimmy Dynamics of an Aircraft Dual-Wheel Main Landing Gear [O] . Howcroft, Chris, Krauskopf, Bernd, Lowenberg, Mark H, 2013

机译：可变边撑几何形状对飞机双轮主起落架摆线动力学的影响
8. Reduction of the shimmy tendency of tail and nose-wheel landing gears by installation of specially designed tires [R] . Schrode, H 1955

机译：通过安装专门设计的轮胎，减少尾翼和前轮起落架的摆振趋势

Investigation of Landing Gear Wheel Shimmy Taking into Account Damper Frequency Characteristics

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