A new type of wind tunnel test device for aeroelasticity-pressure measurement with synchronous inertial force measurement

A technology of wind tunnel test and inertial force, which is applied in the direction of measuring device, aerodynamic test, machine/structural component test, etc. It can solve the problem of inability to realize more accurate prediction of actual engineering, reduce the efficiency of wind tunnel test, and reduce the test efficiency, etc. problems, to achieve the effect of reducing test costs, avoiding waste of manpower and material resources, and meeting test requirements

Active Publication Date: 2019-11-05
CHONGQING UNIV +1
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Problems solved by technology

[0002] Existing studies have shown that the interaction between the test components and still air, that is, the fluid-solid coupling effect, will have a greater or lesser impact on the research results, which cannot achieve the purpose of more accurate prediction of the actual project, and at this stage there is no suitable A complete system for relevant research and analysis
In the traditional wind tunnel test, the test component is fixed in the wind tunnel for testing, and then the test component is forced to vibrate to make up for the shortcomings of the fixed test component, which will greatly reduce the test efficiency of the wind tunnel; when the test component stiffness is not At the same time, the test components need to be replaced, which also reduces the test efficiency and causes unnecessary waste in all aspects

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  • A new type of wind tunnel test device for aeroelasticity-pressure measurement with synchronous inertial force measurement
  • A new type of wind tunnel test device for aeroelasticity-pressure measurement with synchronous inertial force measurement
  • A new type of wind tunnel test device for aeroelasticity-pressure measurement with synchronous inertial force measurement

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Embodiment Construction

[0021] The preferred embodiments of the present invention will be described in detail below with reference to the accompanying drawings.

[0022] As shown in the figure, the comprehensive wind tunnel test device in the present invention includes a wind tunnel body 1 for testing the test component 2, a conductive component 3 for fixing the test component 2, a stiffness control subsystem 4 for changing the stiffness of the test component 2, and A data acquisition subsystem 5 for collecting test data; the conductive member 3 is mainly composed of a cross bar 33 and a rigid connecting rod 32, and the two side walls of the wind tunnel body 1 are correspondingly provided with through holes, and the rigid connecting rod 32 crosses the two through holes and the two ends of the rigid connecting rod 32 protrude from the outside of the wind tunnel, and the cross bar 33 is arranged laterally at the two ends of the rigid connecting rod 32; 43, the installation frame 41 is symmetrically arr...

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Abstract

The invention belongs to the field of structural wind engineering and specifically discloses a novel wind tunnel test device for synchronously measuring aeroelasticity-pressure of inertia force. The test device comprises a wind tunnel body for testing a test member, a conduction member for fixing the test member, a stiffness control subsystem for changing stiffness of the test member and a data acquisition subsystem for collecting test data. The novel wind tunnel test device solves the problem that conventional wind tunnel test needs extra tests when considering fluid-solid coupling effect, and realizes test of different stiffness of members on the basis of not replacing the test member, thereby preventing waste of manpower and material resources, improving use efficiency of a wind tunneland reducing test cost.

Description

technical field [0001] The invention belongs to the field of structural wind engineering, and in particular relates to a novel aeroelastic-pressure measuring wind tunnel test device for synchronous inertial force measurement. Background technique [0002] Existing studies have shown that the interaction between the test components and still air, that is, the fluid-solid coupling effect, will have a greater or lesser impact on the research results, which cannot achieve the purpose of more accurate prediction of the actual project, and at this stage there is no suitable A complete set of systems for relevant research and analysis. In the traditional wind tunnel test, the test component is fixed in the wind tunnel for testing, and then the test component is forced to vibrate to make up for the shortcomings of the fixed test component, which will greatly reduce the test efficiency of the wind tunnel; when the test component stiffness is not At the same time, the test components...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): G01M9/00G01M9/06
CPCG01M9/00G01M9/06
Inventor 陈增顺王旭李华强李勇陈星宇
Owner CHONGQING UNIV
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