还包括一次起落架收放系统的故障分析。
It also states a troubleshooting analysis of the undercarriages retractile system.
对以铰链连接为主的某型飞机前起落架收放机构的磨损可靠性进行了全面的计算。
The wear reliability on extending-retracting mechanism of nose landing gear of a military aircraft is analysesed and calculated.
无人机起落架设计所涉及的相关构件、机构通常包括：缓冲支柱、机轮、轮胎、刹车防滑系统、操纵减摆机构、收放机构等。
The relevant organizations involved usually include absorbing system, undercarriage tyre, brake slip resistance system, landing gear shimmy dampers, retracting-lowering system, etc.
飞机的所有主要的部件位于桶状机身的前部，燃料箱和可收放的起落架位于飞行员下面。
All the main parts of the airplane were located in the front part of the tubby fuselage, the fuel tank and retractable landing gear were right under the pilot.
对运七飞机起落架外筒收放作动筒连接摇臂的断裂损伤失效进行了分析。
Abstract: Fracture failure of junction crank arm of external cylinder retraction-extension actuator of landing gear of Y-7 aircraft is analyzed in this paper.
对运七飞机起落架外筒收放作动筒连接摇臂的断裂损伤失效进行了分析。
Abstract: Fracture failure of junction crank arm of external cylinder retraction-extension actuator of landing gear of Y-7 aircraft is analyzed in this paper.
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