Dynamic Analysis of Aircraft Landing Gear Wheel

被引：0
|
作者：
Jozwik, Jerzy [1 ]
Pytka, Jaroslaw [1 ]
Tofil, Arkadiusz [2 ]
机构：
[1] Lublin Univ Technol, Fac Mech Engn, Lublin, Poland
[2] State Sch Higher Educ, Inst Tech Sci & Aviat, Chelm, Poland
来源：
2018 5TH IEEE INTERNATIONAL WORKSHOP ON METROLOGY FOR AEROSPACE (METROAEROSPACE) | 2018年
关键词：
landing gear; wheel dynamics; oproelectronic methods; TIRES; MODEL;
D O I：
暂无
中图分类号：
V [航空、航天];
学科分类号：
08 ; 0825 ;
摘要：
The paper is devoted to a new method of dynamic analysis of an aircraft landing gear wheel. The method includes a drop ramp as well as an optoelectronic setup. The aircraft wheel and landing gear can be tested in the laboratory as well as in field conditions. Results from the analysis include kinematics of selected points on the tyre: displacements, velocities and accelerations measured in real time. The main goal of the analysis is to provide experimental data for verification of model simulation results. Another application is determination of loads on aircraft landing gear.
引用
收藏
页码：462 / 467
页数：6
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