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- W2400121504 abstract "In this paper dynamic analysis of aircraft landing gear during landing impact and taxiing with typical dual-chamber shock absorbers are conducted. A simplified model for the dynamic analysis is developed by assuming a three-masses system, i.e. sprung, unspurng and rotating masses. Kinematic equations are given, in which stroke, stroke velocity, tire deflection, the slip velocity between the tire surface and the ground are considered. Force relations are discussed dealt with internal shock shrut force, hydraulic force, bearing friction, tire vertical reaction and tire drag force fer single dual-chamber shock absorber. The analytical results for the three typical types of shock-absorber are obtained under design impact and taxiing conditions. Some main characteristics describing dynamic behavior of dual-chamber shock-absorbers, such as, overlaod, unsprung displacement, absorbed energy and tire deflection are presented. It demonstrates that there are respectively advantages and disadvantages for different types of dual-chamber shock absorbers, which is helpful far aircraft landing gear design." @default.
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- W2400121504 date "1997-08-01" @default.
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- W2400121504 title "Dynamic Behavior of Aircraft Landing Gear with Typical Dual-Chamber Shock-Absorbers" @default.
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