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Temporary impulse type sub-transonic wind tunnel control system

A control system, supersonic technology, applied in general control systems, control/regulation systems, program control, etc., can solve the problems of not achieving very high control accuracy, scattered control parts, and many types of signals, and achieve convenient operation and observation. Test situation, ensure reliability and real-time performance, solve the effect of scattered control parts

Active Publication Date: 2020-04-10
CHINA ACAD OF AEROSPACE AERODYNAMICS
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AI Technical Summary

Problems solved by technology

The manual adjustment of the wind tunnel flow field has the following disadvantages: the adjustment accuracy of the flow field is easily affected by the pressure fluctuation of the source airflow; the manual adjustment cannot achieve high control accuracy and takes too long, and the energy loss is large
In addition, the structure of the wind tunnel is complex, the control parts are scattered, the types and quantities of ground signals involved are large, and the reliability and real-time performance of signal transmission are high, all of which put forward high requirements for the establishment of a wind tunnel control system

Method used

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  • Temporary impulse type sub-transonic wind tunnel control system
  • Temporary impulse type sub-transonic wind tunnel control system

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Embodiment Construction

[0034] Specific embodiments of the present invention will be further described in detail below in conjunction with the accompanying drawings.

[0035] Such as figure 1 The shown invention proposes a temporary subtransonic wind tunnel control system for controlling the temporary subtransonic wind tunnel. The structural composition of the temporary subtransonic wind tunnel is as follows: figure 2 As shown, it includes honeycomb 1, damping net 2, exhaust throttle 3, front chamber 4, nozzle 5, test section 6, supersonic diffusion section 7, suction ejector 8, subsonic diffusion section 9, 2 #Pressure regulating valve 10, bypass valve 11, 1# pressure regulating valve 12, starting valve 13, incremental injector (ie 2# injector) 14, main valve 15, air source 16, silencer tower 17.

[0036] The wind tunnel control system includes console master control computer, console simulation display computer, console operation display area, video monitoring computer, Ethernet switch, Mach num...

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Abstract

The invention relates to a temporary impulse type sub-transonic wind tunnel control system. The system comprises a console general control computer, a console analog display computer, a console operation display area, a video monitoring computer, an ethernet switch, a Mach number monitoring computer system, a data acquisition computer system, an equipment management computer system, a diffusion section control computer system, an Ethernet switch, a 2# valve driving unit, an attack angle mechanism driving unit, a safety interlocking PLC unit, a 1# valve and 2# ejector driving unit, a diffusionsection driving unit and a data acquisition unit. According to the invention, a distributed layout is adopted, so that an operator can operate and observe the test condition conveniently, the problemsof scattered control parts, various signal types and large quantity are effectively solved, and the reliability and real-time performance of signal transmission can be well ensured. Ethernet communication is used among the nodes, so that the system nodes are not limited by geographic positions and can be conveniently expanded and moved.

Description

technical field [0001] The invention relates to a temporary subtransonic wind tunnel control system, which belongs to the technical field of subtransonic wind tunnels. Background technique [0002] The wind tunnel is the main equipment for aerodynamic tests. It is a special pipeline designed according to specific requirements. In this special pipeline, the power device is used to generate an adjustable airflow, so that the model flow field obtained in the test section can be simulated or Partial simulation of the prototype flow field. Wind tunnel flow field is a major indicator of wind tunnel performance. In the previous flow field control, the opening of the pressure regulating valve was manually adjusted by the operator to control the flow of compressed air entering the wind tunnel. The manual adjustment of the wind tunnel flow field has the following disadvantages: the adjustment accuracy of the flow field is easily affected by the pressure fluctuation of the source air...

Claims

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Application Information

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IPC IPC(8): G05B19/05G01M9/02
CPCG01M9/02G05B19/058G05B2219/14006
Inventor 张娜宋法振侯逸青刘书伟
Owner CHINA ACAD OF AEROSPACE AERODYNAMICS
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