The present invention discloses a helicopter undercarriage having a vibration reduction function. The helicopter undercarriage comprises a base plate and a support plate connected to the base plate, wherein an included angle is formed between the planes of the base plate and the support plate, and the base plate and the support plate are made from carbon fibers. According to the present invention, the included angle is arranged between the planes of the base plate and the support plate, and the base plate and the support plate are made from the carbon fibers, such that the buffer effect can be provided when the helicopter lands, and the impact force generated during the helicopter landing can be subtracted so as to effectively prevent the helicopter from damage caused by the undercarriage or prevent the equipment or instruments arranged inside the helicopter body from damage.
Helicopter undercarriage having vibration reduction function
2016-01-20
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |