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Aeroengine ground stand test state monitoring system

An aero-engine and bench test technology, which is applied in general control systems, control/adjustment systems, computer control, etc., can solve the problems that manual records cannot meet the requirements of aero-engine experiments, and achieve communication stability and prevent data packet loss , Measurement and control accuracy and high speed effect

Inactive Publication Date: 2016-01-06
SHENYANG AEROSPACE XINGUANG GRP
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  • Description
  • Claims
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Problems solved by technology

[0003] The present invention aims at the problems existing in the above-mentioned prior art, and provides a labview-based aero-engine ground bench test state monitoring system, which solves the problem that manual records in the prior art cannot meet the requirements of aero-engine experiments

Method used

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  • Aeroengine ground stand test state monitoring system
  • Aeroengine ground stand test state monitoring system
  • Aeroengine ground stand test state monitoring system

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Embodiment Construction

[0020] Specific embodiments of the present invention will be described in detail below in conjunction with the accompanying drawings, so as to define the protection scope of the present invention more clearly.

[0021] figure 1 The overall structure diagram of the aero-engine ground bench test status monitoring system of the present invention is given. The system includes a serially connected field data acquisition terminal, an electronic controller, and a computer with a labview development platform as a host computer.

[0022] The on-site data acquisition terminal includes at least one speed sensor, at least one temperature sensor, and at least one pressure sensor, wherein the speed sensor detects the engine rotor speed, the temperature sensor detects the intake air temperature of the engine inlet port and the outlet temperature of the tail nozzle, and the pressure sensor detects the engine rotor speed. Check the inlet and outlet pressure of the compressor.

[0023] figur...

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Abstract

The invention relates to a labview-based aeroengine ground stand test monitoring system, used for monitoring states in an aeroengine stand test, and comprises setting control parameters, sending control instructions, receiving and displaying state parameters in real time, and storing and analyzing experiment data. The system comprises a data collector and a computer with a labview exploitation platform. The system utilizes a serial port communication method to avoid data loss in high speed collection and data transmission processes, reliably controls an engine, and can store and analyze experiment data. The system can be used for state monitoring and performance analysis in an aeroengine preresearch phase ground green test process, and is an aeroengine ground green test monitoring system with complete functions.

Description

technical field [0001] The invention designs a host computer monitoring system, in particular to a labview-based aero-engine ground bench test state monitoring system, which is used for state monitoring and control during the aero-engine bench test. Background technique [0002] Testing is a basic method for people to understand the objective world through experiments to obtain qualitative or quantitative information about the subjects. In the development process of contemporary science and technology, testing work is the guarantee of the performance and quality of modern equipment systems. With the continuous improvement of the performance of aero-engines, more and more parameters are obtained in the engine bench test, and the requirements for the accuracy and speed of measurement and control are also getting higher and higher. The traditional method of manually recording test data can no longer meet the needs of modern aero-engines. Experimental requirements. Contents o...

Claims

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Application Information

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IPC IPC(8): G05B19/048G01M15/05G08C19/00
CPCG05B19/048G01M15/05G08C19/00
Inventor 申春艳韩冬倪瑞林张景峰张春艳王惠
Owner SHENYANG AEROSPACE XINGUANG GRP
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