Adaptive bulging air inlet channel deformation driving device based on flexible skin

A driving device and air intake technology, which is applied to the combustion, transportation and packaging, airframe and other directions of the air intake of the power device. Effects of insufficient out-of-plane stiffness, good engineering suitability, optimal advance matching characteristics

Active Publication Date: 2015-03-11
沈阳飞机设计研究所扬州协同创新研究院有限公司
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  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0006] The technical problem to be solved by the present invention is to provide a flexible skin-based self-adaptive bulging inlet deformation drive device. The problem of not being able to carry large loads out of the plane

Method used

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  • Adaptive bulging air inlet channel deformation driving device based on flexible skin
  • Adaptive bulging air inlet channel deformation driving device based on flexible skin
  • Adaptive bulging air inlet channel deformation driving device based on flexible skin

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Embodiment Construction

[0016] The specific implementation manners of the present invention will be further described in detail below.

[0017] The present invention is a flexible skin-based self-adaptive bulging air inlet deforming drive device, the drive device: adopts the method of gas charging, uses an air pump to pressurize the sealed cavity to deform the flexible skin; uses the skin connection belt Realize the coordinated change of the volume of the inner and outer sealing chambers; use valves and pipelines to control the flow of gas; use pressure sensors and flow sensors to obtain pressure and flow information, and use them as parameters to control the deformation of the flexible skin to any design surface; use sealing gas Provide sufficient out-of-plane stiffness for the flexible skin;

[0018] The driving device includes an air pump 1, an inflation pipeline 2, an inflation valve 3, a deflation pipeline 4, a deflation valve 5, an inner sealing cavity 6, an outer sealing cavity 7, a pressure s...

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Abstract

The invention belongs to the technical field of aviation structural design, and relates to an adaptive bulging air inlet channel deformation driving device based on flexible skin. The driving device comprises an inflation pump (1), an inflation pipeline (2), an inflation valve (3), a deflation pipeline (4), a deflation valve (5), an inner-side sealing cavity (6), an outer-side sealing cavity (7), a pressure sensor (8), a flow sensor (9), a skin connecting belt (10) and a basic profile mounting region (11). According to the driving device, shape change of the bulging profile of an air inlet channel in a large range is realized by using a gas pressurizing way, and the shape of the bulging profile is controlled by using pressure and flow information, so that the throat area of the air inlet channel is changed, and the problem of non-adjustability of the profile of the bulging air inlet channel is solved.

Description

technical field [0001] The invention belongs to the technical field of aeronautical structure design, and relates to a flexible-skin-based self-adaptive bulging inlet deformation drive device. Background technique [0002] In the process of designing the inlet of a supersonic fighter, the contradiction between high and low-speed aerodynamic configurations is often faced, and the stealth requirements of the aircraft also restrict the design and performance of the aerodynamic configuration of the inlet. Therefore, during the design process of the supersonic inlet, it is difficult to maintain the high performance of the inlet throughout the flight envelope. [0003] In order to solve the above design problems, the design concept of adaptive bulging inlet is proposed. The adaptive bulge inlet can adaptively change the structural shape of the pipe (bulge) in the inlet through active control technology according to the different flight states of the aircraft, and adjust the throa...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64D33/02
CPCB64D33/02B64C2001/009
Inventor 邱涛王鄢周翌勋
Owner 沈阳飞机设计研究所扬州协同创新研究院有限公司
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