According to the technical scheme, the buffer is characterized in that the buffer comprises an outer ring, and the outer ring is used for being connected with a wheel axle frame; the inner ring is coaxially arranged in the outer ring and is used for being connected with a machine body; the elastic body is arranged between the inner ring and the outer ring in a vulcanization mode so that the axle frame can be compressed to rotate during landing, and the inner ring and the outer ring are driven to rotate relatively so as to compress the elastic body for buffering and vibration isolation. The buffer of the aircraft landing gear has the advantages that the structure is simple, and the effect of full buffering and damping can be achieved when the buffer is applied to a small aircraft.
本发明公开了一种飞机起落架的缓冲器,其技术方案要点是包括外圈,所述外圈用于与轮轴架连接;内圈,所述内圈同轴设置于外圈内,并用于与机身连接;弹性体,所述弹性体硫化设置于内圈与外圈之间,以使在着陆时所述轮轴架被压缩转动,带动内圈和外圈相对转动以压缩所述弹性体缓冲隔振。本发明一种飞机起落架的缓冲器,具有结构简单,且应用于小型飞行器上时能够起到充分缓冲减震的效果。
Buffer of aircraft landing gear
一种飞机起落架的缓冲器
2024-12-20
Patent
Electronic Resource
Chinese
IPC: | B64C AEROPLANES , Flugzeuge |
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