Folding structure and folding method of aircraft wing
A folding structure and folding mechanism technology, which is applied to the folding structure and folding field of aircraft wings, can solve the problems of occupation, collision with radar, and large size, etc.
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[0020] Referring to accompanying drawing, the folding structure of the aircraft wing of the present application, described aircraft wing contains central wing 1 and folding wing 2, and described central wing is fixed on the fuselage, and described folding wing can be relative to by folding mechanism The central wing performs the movement. The folding mechanism is located between the central wing 1 and the folding wing 2. The folding mechanism contains a Z-shaped rotating shaft 4, a hydraulic telescopic rod 10 and an electromagnetic lock 15. The two ends of the Z-shaped rotating shaft 4 and the hydraulic telescopic rod 10 are respectively connected to the central wing 1 and the folding Wings 2 are connected, and there are two mutually perpendicular first rotating surfaces 5 and second rotating surfaces 6 on the Z-shaped rotating shaft 4, the first rotating surface 5 is parallel to the folded wing rear beam 8, and the second rotating surface 6 is connected to the central wing Th...
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