Aircraft landing gear utilizing spring buckle
A technology of aircraft landing gear and spring buckle, which is applied in the direction of landing gear, aircraft parts, wheels, etc., to achieve the effect of slow speed, fast extension and high stability
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[0016] An aircraft landing gear utilizing a spring buckle is composed of a landing gear fixing device 1, a spring support rod I2, a landing gear support rod 3, a hydraulic rod I4, a landing gear moving device 5, a hydraulic rod II6 and a connecting rod with a rotating shaft 7, the landing gear fixing device 1 is composed of landing gear fixing plate 101, hydraulic rod III 102 and rotating shaft I 103, and the landing gear moving device 5 is composed of chassis 501, landing wheels 502, rotating shaft It consists of Ⅱ503, spring support rod Ⅱ504, spring support rod Ⅲ506 and connecting shaft 505. It is characterized in that: the spring support rod Ⅰ2 is installed on the landing gear fixing device 1, the hydraulic rod Ⅲ102 is installed on the landing gear fixing device 1, and the landing gear supports One end of the rod 3 is fixed on the front end of the hydraulic rod III102, the middle point of the landing gear support rod 3 is fixed on the upper end of the spring support rod I2, ...
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