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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.

Pending Publication Date: 2021-06-08
中航西飞民用飞机有限责任公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

However, because the shipboard early warning aircraft is equipped with a disc-shaped shipboard radar on the top of the fuselage, it cannot use the upwardly folded wings. If the wings are folded too much, they will bump into the radar. If they are folded less, its footprint will not be reduced. How many
However, due to its large size, the use of non-folding carrier-based early warning aircraft will occupy the deck space of at least two carrier-based aircraft, resulting in a reduction in the total number of boarding aircraft.

Method used

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  • Folding structure and folding method of aircraft wing
  • Folding structure and folding method of aircraft wing
  • Folding structure and folding method of aircraft wing

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Embodiment Construction

[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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Abstract

The invention relates to a folding structure and folding method of an aircraft wing. The aircraft wing comprises a central wing and a folding wing, a folding mechanism is arranged between the central wing and the folding wing, the folding mechanism comprises a Z-shaped rotating shaft and a hydraulic telescopic rod, and the two ends of the Z-shaped rotating shaft and the two ends of the hydraulic telescopic rod are connected with the central wing and the folding wing respectively. The Z-shaped rotating shaft is provided with a first rotating surface and a second rotating surface which are perpendicular to each other, the first rotating surface is parallel to a rear beam of the folding wing, the second rotating surface is perpendicular to a rear beam of the central wing, and the hydraulic telescopic rod can push the folding wing to rotate around the first rotating surface and the second rotating surface, so that the folding wing is folded downwards and backwards relative to the central wing.

Description

technical field [0001] The invention relates to the technical field of aircraft structure design, in particular to an aircraft wing folding structure and a folding method. Background technique [0002] Since more fighter jets and other types of military carrier-based aircraft need to be docked on the deck of an aircraft carrier, most of the carrier-based aircraft use upwardly folded wings to save deck space, thereby docking more fighter jets. However, because the shipboard early warning aircraft is equipped with a disc-shaped shipboard radar on the top of the fuselage, it cannot use the upwardly folded wings. If the wings are folded too much, they will bump into the radar. If they are folded less, its footprint will not be reduced. How many. However, due to its large size, the non-folding carrier-based early warning aircraft will occupy the deck space of at least two carrier-based aircraft, resulting in a reduction in the total number of boarding aircraft. Contents of the...

Claims

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Application Information

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IPC IPC(8): B64C3/56
CPCB64C3/56
Inventor 李臣杨栓宝李向维朱贤明
Owner 中航西飞民用飞机有限责任公司