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Wind tunnel angle-of-attack adjusting device

A technology for adjusting the device and angle of attack, which is applied in the field of aerospace and aviation, can solve the problems of the limited range of attitude adjustment of the angle of attack mechanism and the narrow range of the angle of attack, and achieve the effect of enriching the adjustment of the attitude, solving the narrow range of the angle of attack, and increasing the adjustment range

Active Publication Date: 2016-04-06
HUBEI SANJIANG AEROSPACE GRP HONGYANG ELECTROMECHANICAL
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  • Claims
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Problems solved by technology

[0003] The application provides a wind tunnel angle of attack adjustment device, which solves the technical problems in the prior art that the angle of attack range of the wind tunnel angle of attack mechanism is narrow in a limited space, and the attitude adjustment range of the angle of attack mechanism is limited.

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  • Wind tunnel angle-of-attack adjusting device

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Embodiment Construction

[0030] The embodiments of the present application provide a wind tunnel angle-of-attack adjustment device, which solves the technical problems in the prior art that the angle-of-attack mechanism of the wind tunnel has a narrow range of angle of attack in a limited space and the attitude adjustment range of the angle-of-attack mechanism is limited.

[0031] The technical solution in the embodiment of the present application is to solve the above-mentioned technical problems, and the general idea is as follows:

[0032] A wind tunnel angle of attack adjustment device, said wind tunnel angle of attack adjustment device comprising:

[0033] The X-axis moving mechanism includes a base one, two linear guide rails one relatively arranged on the base one, a screw pair one arranged on the base one, a motor one, connecting the motor one and the screw rod The gear pair 1 of the pair 1, the motor 1 drives the screw pair 1 through the gear pair 1 to move along the linear guide rail 1 on th...

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Abstract

The invention discloses a wind tunnel angle-of-attack adjusting device, which comprises an X-shaft mobile mechanism, a Y-shaft mobile mechanism, a yaw angle adjusting mechanism, and a pitch angle adjusting mechanism. By arranging the X-shaft mobile mechanism, the Y-shaft mobile mechanism, the yaw angle adjusting mechanism, and the pitch angle adjusting mechanism, the adjusting in four degrees of freedom is realized; and the pitch angle adjusting scope is greatly increased by loading a motor on a machete plate to revolute with a model pole in a limited test section space. The pitch angle adjusting scope is -10DEG-40 DEG, and is increased by nearly 10 DEG compared with that of a traditional way, therefore, the adjusting attitude of the angle-of-attack mechanism is added; the adjusting scope of the integral angle-of-attack mechanism is greatly increased; and the problems of small angle-of-attack scope of the wind tunnel angle-of-attack mechanism in a limited space and limited attitude adjusting scope of the angle-of-attack mechanism are solved.

Description

technical field [0001] The invention relates to the field of aerospace technology, in particular to a device for adjusting the angle of attack of a wind tunnel. Background technique [0002] At present, most of the existing wind tunnel angle-of-attack mechanisms have three degrees of freedom or less. In a limited space, the range of the angle of attack is narrow and the accuracy is relatively low. The attitude adjustment range of the angle-of-attack mechanism is limited. With the rapid development of my country's aerospace industry, an angle-of-attack mechanism suitable for large-scale wind tunnel tests, with a large variable range, many degrees of freedom, high precision levels, and a high structural strength and safety factor needs to be developed urgently. Contents of the invention [0003] The present application provides a device for adjusting the angle of attack of a wind tunnel, which solves the technical problems in the prior art that the angle of attack range of t...

Claims

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Application Information

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IPC IPC(8): G01M9/04
Inventor 严山王毅李辰
Owner HUBEI SANJIANG AEROSPACE GRP HONGYANG ELECTROMECHANICAL
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