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提出飞机起落架连续变行程疲劳试验实施方案；设计了试验装置；并通过时歼数五主起落架减震器模拟试验验证了本文方案的合理性、可行性。
Proposed the landing gear continuous variable stroke fatigue test implementation plan; design of the test device; and through the F-five main landing gear shock absorber simulation test to verify the rationality of the program, feasibility.