目的 验证某型飞机从万米高空俯冲降落直至着陆滑跑过程中,在经历了环境温度从-55℃到常温快速剧烈变化后起落架性能的改变.方法 依据起落架落震试验要求,进行起落架高低温环境模拟技术研究.结果 综合考虑试验技术指标、试验件结构尺寸和试验场地限制,成功研制了专用的起落架高低温环境模拟设备.结论 为研究起落架缓冲器内敏感参数与温度的变化规律和起落架结构性能提供了验证手段.%Objective To verify the performance change of a landing gear after a rapid and severe change of ambient temper-ature from-55℃ to normal temperature in the progress of aircraft diving form high altitude to landing and taxiing.Methods High and low temperature environment simulation techniques for aircraft landing gear were researched according to require-ments on drop test of landing gear.Results Special high and low temperature simulation equipment for landing gear was suc-cessfully developed in view of indicators on test techniques and restrictions on structural size of test piece and test site.Conclu-sionIt provides a method for verifying change rules of sensitive parameters and temperature in the buffer of the landing gear and the structural performance of the landing gear.
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