Wing folding mechanism of morphing aircraft

A technology of wing folding mechanism and variant aircraft, which is applied in the direction of wing adjustment, etc., which can solve the problems of the gap between the inner section of the wing and the outer section of the wing, and the only use of the wing folding mechanism, so as to achieve the effect of improving strength and rigidity

Active Publication Date: 2016-12-07
NORTHWESTERN POLYTECHNICAL UNIV
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0006] The purpose of the present invention is to solve the problem that the existing wing folding mechanism is only used for ground folding, or there will be a gap between the inner wing and the outer wing during the folding process, and provides a wing folding mechanism for a variant aircraft

Method used

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  • Wing folding mechanism of morphing aircraft
  • Wing folding mechanism of morphing aircraft
  • Wing folding mechanism of morphing aircraft

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specific Embodiment approach 1

[0024] Specific implementation mode one: the following combination Figure 1 to Figure 11 Describe this embodiment, the wing folding mechanism of variant aircraft described in this embodiment, it comprises the wing spar 1 of inner section wing, inner reinforcement rib 2, outer reinforcement rib 8 and the wing spar 9 of outer section wing, it It also includes a fairing main body 3, a plurality of inner lugs 4, a rotary actuator 5, a plurality of outer lugs 6 and a sealing ring 7,

[0025] The inner rib 2 is fixedly arranged on the spar 1 of the inner wing, the outer rib 8 is fixedly arranged on the spar 9 of the outer wing, and the rotary actuator 5 is located between the inner rib 2 and the outer rib 8 The inner side of the rotary actuator 5 is dispersedly provided with a plurality of inner lugs 4, and the outer side of the rotary actuator 5 is dispersedly provided with a plurality of outer lugs 6, the inner lugs 4 are connected with the inner reinforcing ribs 2, and the outer...

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Abstract

The invention discloses a wing folding mechanism of a morphing aircraft, and belongs to the field of aircraft wing mechanisms. The problems that an existing wing folding mechanism is only used for ground folding, and a gap is formed between an inner wing section and an outer wing section in the folding process are solved. An inner side reinforcing rib is fixedly arranged on a wing beam of the inner wing section, an outer side reinforcing rib is fixedly arranged on a wing beam of the outer wing section, a rotary actuator is located between the inner side reinforcing rib and the outer side reinforcing rib, a fusiform fairing is composed of a fairing body and a sealing ring, and an inner side lug, the rotary actuator and the outer side lug are sealed inside the fusiform fairing. The connection end of the fairing body is connected to an outer frame of the inner side reinforcing rib in a sleeving mode, and the connection end of the sealing ring is connected to an outer frame of the outer side reinforcing rib in a sleeving mode. The wing mechanism is foldable.

Description

technical field [0001] The invention relates to a wing folding mechanism of a variant aircraft, and belongs to the field of wing mechanisms of aircraft. Background technique [0002] Wing folding can significantly change the wetted area of ​​the whole aircraft, which is a typical way for variant aircraft to change the shape of the aircraft. Especially in the case of supersonic speed, by folding the outer section of the wing downward at a certain angle, not only can the supersonic drag be greatly reduced, the directional stability can be enhanced, but also the air on the lower wing surface can be compressed to provide additional lift. Due to the above functions, the following conditions need to be met when designing the wing folding mechanism: (a) to realize the function of folding and unfolding of the wings during flight; (b) to ensure the aerodynamic and stealth performance of the aircraft, the folding and during the unfolding process, there should be no gap between the in...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64C3/56
CPCB64C3/56
Inventor 孙中超喻天翔崔卫民宋笔锋
Owner NORTHWESTERN POLYTECHNICAL UNIV
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