Force measurement, pressure measurement, angle measurement and vibration inhibition multi-functional model

A technology of vibration suppression and angle measurement, which is applied in the field of wind tunnel testing, can solve the problems of unsatisfactory model cost economy, high test efficiency, high model processing cost, and waste of time occupying the hole, and achieves simple structure, convenient disassembly and assembly, and Effect of suppressing vibration situations

Inactive Publication Date: 2018-01-26
AVIC SHENYANG AERODYNAMICS RES INST
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  • Abstract
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  • Claims
  • Application Information

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Problems solved by technology

[0003] If models with different functions are designed for different research needs, the cost of model processing is bound to be high
And in a test project, different models are used for research, and because the replacement of the model will cause a waste of time in occupying the hole
Therefore, models with single functions such as force measurement or pressure measurement can no longer meet the requirements of model cost economy and test efficiency.

Method used

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  • Force measurement, pressure measurement, angle measurement and vibration inhibition multi-functional model
  • Force measurement, pressure measurement, angle measurement and vibration inhibition multi-functional model
  • Force measurement, pressure measurement, angle measurement and vibration inhibition multi-functional model

Examples

Experimental program
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Effect test

Embodiment 1

[0012] Such as Figure 1-3 As shown, a multifunctional model of force measurement, pressure measurement, angle measurement, and vibration suppression includes an aircraft model 1, an angle measurement device 3, a scanning valve 4, a balance 6, a vibration suppressor 7 and a tail strut 8;

[0013] One end of the balance 6 is connected with the aircraft model 1, and the other end of the balance 6 is connected with the tail strut 8 through the vibration suppressor 7 to realize the measurement of the model aerodynamic force;

[0014] There is a pressure measuring section on the wing 9 of the model airplane, and its pressure measuring pipeline is led to the abdominal cavity of the airplane model, and then introduced into the nose of the airplane model to connect to the scanning valve 4, and the scanning valve cable passes through the center hole of the balance and the center hole of the tail support Lead out the aircraft model to realize the pressure measurement on the wing surface...

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Abstract

The invention relates to a force measurement, pressure measurement, angle measurement and vibration inhibition multi-functional model. The model comprises an airplane model, angle measurement equipment, a scanning valve, a scale, a vibration inhibition device and a tail sting, wherein one end of the scale is connected with the airplane model, the other end of the scale is connected with the tail sting through the vibration inhibition device, wings of the airplane model are provided with pressure measurement cross sections, a pressure measurement pipeline is led to a belly cavity of the airplane model and is then led into an internal portion of a head of the airplane model to connect with the scanning valve, a scanning valve cable is led out of the airplane model through a scale center holeand a tail sting center hole to realize wing surface pressure measurement, the angle measurement equipment is arranged in the head of the airplane model, the cable is led out through the scale centerhole and the tail sting center hole, model attitude angle measurement is realized, and model vibration can be effectively inhibited through the vibration inhibition device. The model is advantaged inthat multiple types of measurement components are reasonably designed and distributed, force measurement, pressure measurement and angle measurement are synchronously carried out, the structure is simple, and the model is convenient to dismount.

Description

technical field [0001] The invention relates to wind tunnel test technology, in particular to a multifunctional model for force measurement, pressure measurement, angle measurement and vibration suppression. Background technique [0002] The wind tunnel model is the key equipment for wind tunnel experiments. Conventional dynamometric phantoms are used for dynamometric test studies, or manometry phantoms are used for manometric test studies. At present, a test project often has various requirements, that is, to measure force and pressure, and may also require consideration of other test studies. [0003] If models with different functions are designed for different research needs, the cost of model processing is bound to be high. And in a test project, different models are used for research, and because the replacement of the model will cause a waste of time in occupying the hole. Therefore, models with single functions such as force measurement or pressure measurement can...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G01M9/08G01M9/06
Inventor 韩松梅李兴龙王世红王彤
Owner AVIC SHENYANG AERODYNAMICS RES INST
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