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Wind tunnel aircraft model aileron angle adjusting device

An angle adjustment device and aircraft technology, applied in the direction of measuring devices, instruments, machine/structural component testing, etc., can solve problems such as lack of aerodynamic parameters, insufficient, safety hazards in aircraft design, etc., and achieve the effect of simple adjustment methods

Pending Publication Date: 2020-05-08
中国空气动力研究与发展中心超高速空气动力研究所
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  • Abstract
  • Description
  • Claims
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AI Technical Summary

Problems solved by technology

In most cases, either the aileron angle adjustment and locking devices are installed on the surface of the aircraft model for testing, resulting in "distortion" of the ground simulation test; Important aerodynamic parameters in the state of angle change
These "inadequate" wind tunnel tests have brought greater safety hazards to aircraft design

Method used

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  • Wind tunnel aircraft model aileron angle adjusting device
  • Wind tunnel aircraft model aileron angle adjusting device
  • Wind tunnel aircraft model aileron angle adjusting device

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Embodiment Construction

[0022] The present invention will be further described in detail below in conjunction with the accompanying drawings, so that those skilled in the art can implement it with reference to the description.

[0023] It should be understood that terms such as "having", "comprising" and "including" as used herein do not entail the presence or addition of one or more other elements or combinations thereof.

[0024] Such as Figure 1-3 The shown wind tunnel aircraft model aileron angle adjustment device includes:

[0025] Aircraft model main body 1, one end is connected with model support bar 2, and described aircraft model main body 1 is rotatably connected with aileron 3, and described aircraft model main body 1 is symmetrically provided with for changing aileron angle and aileron is fixed. Angle adjustment mechanism 4.

[0026] In this technical solution, according to the aileron angle required for the test, the angle of the aileron 3 is adjusted through the angle adjustment mech...

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Abstract

The invention discloses a wind tunnel aircraft model aileron angle adjusting device which comprises an aircraft model body, one end of the aircraft model body is connected with a model supporting rod,ailerons are rotatably connected to the aircraft model body, and angle adjusting mechanisms used for changing the angles of the ailerons and fixing the ailerons are symmetrically arranged in the aircraft model body. The wind tunnel aircraft model aileron angle adjusting device has the advantages that the aileron can deflect at different angles, the adjustment is simple, the operation is convenient, the aerodynamic configuration of the aircraft model is not changed, and the quality of a wind tunnel test flow field is not influenced.

Description

technical field [0001] The invention belongs to the technical field of wind tunnel test devices, in particular to a wind tunnel aircraft model aileron angle adjustment device. Background technique [0002] During the wind tunnel test, it is sometimes necessary to adjust the aileron angle of the aircraft model to obtain different aerodynamic parameters. However, it has always been difficult to adjust and lock the aircraft model ailerons: First, the wind tunnel aircraft model is designed and manufactured according to certain scaling and flow field blockage requirements, and is generally relatively small and fine, especially for hypersonic and thin transitional flow Under the conditions of the simulation test in the regional area, the aircraft model is smaller, and it is difficult to install the aileron angle adjustment and locking device on the small model; second, in the ground test of the aircraft, in order to simulate the high-altitude dynamic environment of the aircraft as...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G01M9/08G01M9/04
CPCG01M9/08G01M9/04
Inventor 李明石义雷李绪国
Owner 中国空气动力研究与发展中心超高速空气动力研究所
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