Method for verifying bird strike resistance performance of pitch link of main blade of helicopter
Patent Information
- Authority / Receiving Office
- CN · China
- Current Assignee / Owner
- CHINA HELICOPTER RES & DEV INST
- Publication Date
- 2015-07-15
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Abstract
Description
technical field
[0001] The invention belongs to the field of helicopter structural strength tests, and mainly relates to a method for determining the performance of a main blade pitch-variable tie rod of a helicopter after bird strike damage occurs in flight. Background technique
[0002] As a special low-altitude aircraft, helicopters are mainly used in the range of 0 to 1000 meters. For example, the use time ratio of a certain type of aircraft in the range of 0 to 600 meters is as high as 40%. This range is the main activity of flying birds. Therefore, the accidents of bird strikes on helicopters worldwide have remained high. Although a helicopter is a low-speed aircraft, its flight speed is generally within 300km / h, but compared with a fixed-wing aircraft, it has a high-speed rotating rotor system. Generally, the speed of the main rotor system of a helicopter is between 200 rpm and 400 rpm. , the speed of the tail rotor is higher, so if the bird strike occurs in the roto...