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An Improved Wind Tunnel Inlet Test Model Support System

A technology of support system and test model, applied in the field of wind tunnel test, can solve the problems of integration, multiple instruments, multiple operations of pipelines, etc., and achieve the effect of good test effect, compact device, convenient and quick operation

Active Publication Date: 2021-08-13
AVIC SHENYANG AERODYNAMICS RES INST
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0008] In order to solve the problem that the traditional model support system in the prior art cannot realize the integration of ventilation and wiring, and the problems of inconvenient operation and poor protection effect caused by many instruments and pipelines during the wind tunnel test

Method used

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  • An Improved Wind Tunnel Inlet Test Model Support System
  • An Improved Wind Tunnel Inlet Test Model Support System
  • An Improved Wind Tunnel Inlet Test Model Support System

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Embodiment Construction

[0036] The present invention will be further described below in conjunction with the accompanying drawings and specific embodiments.

[0037] An improved wind tunnel inlet test model support system, the model support system includes a ventilation arm 53-2, an angle of attack pre-bias rod 54-2, the ventilation arm 53-2 is connected to the wind tunnel angle of attack mechanism 50 The roll angle rotating shaft mechanism 52 is connected; the ventilation arm 53-2 is provided with a gas passage 53-6, a routing passage 53-10, and a ventilation cavity 53-5 in the radial direction from the inside to the outside; the gas passage 53-6 and The ventilation cavity 53-5 is arranged coaxially; the ventilation arm 53-2 is connected to the angle of attack pre-bias rod 54-2; the gas channel 54-2 is provided in the angle of attack pre-bias rod 54-2 to communicate with the gas channel 53-6. The passage extension section, the wiring passage extension section connected with the wiring passage 53-10;...

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Abstract

The invention relates to the field of wind tunnel tests, and discloses an improved wind tunnel inlet test model support system. The model support system includes a ventilation arm and an angle of attack pre-bias rod. The ventilation arm is connected to the wind tunnel angle of attack mechanism. The roll angle shaft mechanism is connected; the ventilation arm is provided with a gas passage, a routing passage, and a ventilation cavity in sequence from the inside to the outside; the gas passage and the ventilation cavity are coaxially arranged; the ventilation arm and the angle of attack pre-biased rod connection; the angle of attack pre-bias rod is provided with an extended section of the gas passage connected with the gas passage, and an extended section of the routing passage connected with the routing passage; the ventilation cavity is communicated with the ventilation pipeline, and the extended section of the gas passage is connected with the The air outlet pipeline is connected; the wall of the angle-of-attack pre-deflection rod has a wiring hole. The invention solves the problem that the traditional model support system in the prior art cannot realize the integrated setting of ventilation and routing, and the problem of inconvenient operation caused by many instruments and many pipelines in the wind tunnel test process.

Description

technical field [0001] The invention belongs to the field of wind tunnel tests, and more particularly relates to an improved wind tunnel inlet test model support system. Background technique [0002] The air intake is one of the important parts of the air-breathing aircraft power plant. In order to study and evaluate the aerodynamic performance of the aircraft inlet in the wind tunnel test, it is usually necessary to simulate the flow conditions of the aircraft inlet pipe in the wind tunnel, and measure the angle of attack and sideslip angle of the inlet at different incoming flow Mach numbers aerodynamic performance. [0003] Typically, the intake duct model is mounted in a wind tunnel by a support system. Due to the relatively low airflow velocity, small aerodynamic load, and large size of the wind tunnel, the low-speed wind tunnel generally does not have high requirements for the support system. Fixing and protection are relatively easy, and simple fixation and protect...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): G01M9/04G01M9/08
CPCG01M9/04G01M9/08
Inventor 马晓光赵效萱刘帅邓祥东季军宋孝宇袁野赵文涛
Owner AVIC SHENYANG AERODYNAMICS RES INST
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