Morphing wing trailing edge driven based on shape memory alloy and deflection method thereof

A technology of memory alloy and modified wing, which is applied in the field of flight control, can solve the problem of not having enough space to install motors, and achieve the effects of reducing design load, improving efficiency and improving reliability

Inactive Publication Date: 2016-08-10
NANJING UNIV OF AERONAUTICS & ASTRONAUTICS
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Problems solved by technology

[0005] The purpose of the present invention is to provide a modified wing trailing edge and its deflection method based on shape memory alloy drive, which uses a new intelligent material shape memory alloy drive to replace the traditional motor drive, and solves the problem of thin airfoils. There is not enough space to install the motor, etc.

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  • Morphing wing trailing edge driven based on shape memory alloy and deflection method thereof
  • Morphing wing trailing edge driven based on shape memory alloy and deflection method thereof
  • Morphing wing trailing edge driven based on shape memory alloy and deflection method thereof

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Embodiment Construction

[0030] The present invention provides a modified wing trailing edge driven by a shape memory alloy and its deflection method. In order to make the object, technical solution and effect of the present invention clearer and clearer, the present invention will be further described in detail with reference to the accompanying drawings and examples. It should be understood that the specific implementations described here are only used to explain the present invention, not to limit the present invention.

[0031] Such as Figure 1 to Figure 5 The shown variant trailing edge based on shape memory alloy drive has a specific structure of a drive system composed of shape memory alloy SMA and a transmission mechanism. The system includes ribs, SMA wires, insulating rods 4 and transmission mechanisms; the ribs include Several interconnected joints, one end of the SMA wire is wound and fixed on the insulating rod 4, and the other end is fixed on the wing rib; the insulating rod 4 is engage...

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Abstract

The invention provides a morphing wing trailing edge driven based on shape memory alloy and a deflection method thereof. The trailing edge is partially wound on an insulating rod by utilizing an SMA wire; through heating the SMA wire, the rotation of the insulating rod is realized by utilizing the shape memory effect of the SMA wire; the insulating rod is connected with a worm, so that a traditional motor is replaced for driving; a trailing edge flap is divided into two parts: an upper part and a lower part; according to the deflection method provided by the invention, through the rotation of one worm, two worm wheels are simultaneously driven to rotate, so that upper and lower wing ribs simultaneously deflect from equilibrium positions to limiting positions, and through changing the transmission ratios of the worm wheels and the worm, the deflection of the upper and the lower wing ribs at different angles can be realized.

Description

technical field [0001] The invention relates to the field of flight control, in particular to a design of a variant trailing edge mechanism driven by a shape memory alloy and a deflection method thereof in the case of a thinner airfoil. Background technique [0002] The traditional trailing edge flap driving method is mainly electromechanical driving, such as hydraulic driving, which has the advantages of high sensitivity and safety, and is suitable for large load requirements, but has disadvantages such as high cost and easy oil leakage; motor driving has the advantage of having Larger power-to-mass ratio and high control precision, but the drive circuit is relatively complex and requires high stability of the equipment. With the research and development of new materials and technologies, new smart materials are constantly emerging. Among them, piezoelectric ceramic materials, magnetostrictive materials and shape memory alloys (SMA) are suitable for driving components. [...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64C9/20B64C13/28
CPCB64C9/20B64C13/28Y02T50/30
Inventor 徐志伟刘阳马晶
Owner NANJING UNIV OF AERONAUTICS & ASTRONAUTICS
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