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A telescopic wing deployment device based on shape memory alloy

A memory alloy and memory alloy wire technology, which is applied in directions such as wing adjustment, can solve the problems of a large telescopic wing drive mechanism and cannot achieve multiple expansion and contraction, and achieves the effect of solving the huge driving mechanism.

Active Publication Date: 2019-06-18
BEIJING LINJIN SPACE AIRCRAFT SYST ENG INST +1
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0005] The purpose of the present invention is to overcome the above-mentioned deficiencies in the prior art, and provide a telescopic wing expansion device based on shape memory alloys, which adopts shape memory alloys as the driving source, and adjusts the stretching of shape memory alloy wires by changing the size of the shape memory alloy power supply current. Length, by cooperating with ordinary springs, the telescopic movement of the telescopic wing is realized, which solves the problem that the drive mechanism of the telescopic wing is huge and cannot be expanded and contracted multiple times

Method used

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  • A telescopic wing deployment device based on shape memory alloy
  • A telescopic wing deployment device based on shape memory alloy
  • A telescopic wing deployment device based on shape memory alloy

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Embodiment Construction

[0023] The present invention will be further described in detail below in conjunction with the drawings and specific embodiments:

[0024] Such as figure 1 Shown is a schematic diagram of a shape memory alloy telescopic wing deployment device. It can be seen from the figure that a shape memory alloy-based telescopic wing deployment device includes inner wing root 1, fixed inner wing 2, inner wing beam 3, spring 4, and outer wing Beam 5, pulley 6, retractable outer wing 7 and shape memory alloy wire 8; wherein the inner wing root 1 is arranged on the edge of the fixed inner wing 2, and the fixed inner wing 2 is fixedly installed on the outer surface of the outer aircraft through the inner wing root 1; The inner spar 3, the spring 4, the outer spar 5, the pulley 6, the retractable outer wing 7, and the shape memory alloy wire 8 are fixedly installed inside the fixed inner wing 2; among them, the inner spar 3 is fixedly installed on the inner wing root 1. On the inner side, the cros...

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Abstract

The invention discloses a shape memory alloy based extension wing unfolding device, and relates to the field of flight adaptability of an aircraft in the complex airflow environment. An inner wing root is arranged on the edge of a fixed inner wing, the fixed inner wing is fixedly installed on the outer surface of the outer aircraft through the inner wing root; an inner wing beam is fixedly installed on the inner side of the inner wing root; the inner wing beam is fixedly connected with an outer wing beam; the outer wing beam is sleeved on the outer wall of the inner wing beam; a pulley is fixedly installed at one end of the outer wing beam; an extension outer wing is fixedly connected with the pulley; the two ends of a shape memory alloy wire are respectively fixedly connected with the two ends of the inner wing root, and are sleeved on the edge of the pulley. The shape memory alloy is used as a drive source, the elongation of the shape memory alloy wire is adjusted by changing the supply current of the shape memory alloy, the extension movement of an extension wing is realized through the match of the common spring and the shape memory alloy wire, and the problems that the current extension wing drive mechanism is huge and cannot be unfolded and shrunk for a plurality of times are solved.

Description

Technical field [0001] The invention relates to the field of flight adaptability of an aircraft in a complex aerodynamic environment, in particular to a telescopic wing deployment device based on a shape memory alloy. Background technique [0002] More and more aircraft are striving to achieve multi-speed and multi-airspace missions. Therefore, the aircraft faces a complex aerodynamic environment and needs to solve different flight adaptability issues such as high altitude and high speed, low altitude and low speed. [0003] Therefore, in order to achieve the multi-airspace and multi-speed domain flight targets of the aircraft, the use of retractable wing variant technology has a good application prospect. At the same time, the traditional telescopic mechanism driven by a turbine worm and a motor has a complicated mechanical structure, a bulky volume and a heavy weight, and cannot be applied to thinner wings. [0004] There is currently no similar product design for domestic aircra...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B64C3/56
CPCB64C3/56
Inventor 申泽帆苏丙未何春全米滨黄兴李苏立超谢雪明李元生廖沫姜宏杰
Owner BEIJING LINJIN SPACE AIRCRAFT SYST ENG INST
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