Main landing gear of airplane
A landing gear and aircraft technology, which is applied in the field of aircraft take-off and landing systems, can solve the problems of large bending moment deformation, wheel jump, and low absorption efficiency of the landing gear buffer system.
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[0036] Such as figure 1 As shown, the main landing gear of the aircraft includes a buffer pillar 1, a foldable strut with a lock 2, a retractable actuator 3, a stabilizing buffer 4, a diagonal strut 5, a front strut 6, a wheel set 7 and Uplock 8;
[0037] The buffer strut 1 is respectively connected to the retractable actuator 3, the foldable strut with lock 2, the stable buffer 4, the front strut 6, the diagonal strut 5 and the wheel Group 7;
[0038] The upper lock 8, the retractable actuator 3, the foldable strut 2 with lock, the buffer strut 1 and the front strut 6 are all connected to the joint of the aircraft fuselage;
[0039] The stabilizing buffer 4 is connected to the wheel set 7 .
[0040] In the above embodiment, the buffer pillar 1 is provided with joints respectively connected with the retractable actuator 3 and the foldable strut 2 with lock, and the buffer pillar 1 is provided with joints connected with the diagonal brace respectively. The double-ear seat c...
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