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A control system of aero-engine central cone flow test equipment and its application method

An aero-engine and equipment control technology, which is applied in the direction of engine testing, non-electric variable control, control/regulation system, etc., can solve the problems of low efficiency and large human factor error, so as to improve accuracy, increase pass rate, and reduce error Effect

Active Publication Date: 2017-02-15
SHENYANG LIMING AERO-ENGINE GROUP CORPORATION
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

In the past, the central cone flow detection equipment used the method of manual reading of the measuring cup for detection, which caused large errors due to human factors and low efficiency.

Method used

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  • A control system of aero-engine central cone flow test equipment and its application method
  • A control system of aero-engine central cone flow test equipment and its application method
  • A control system of aero-engine central cone flow test equipment and its application method

Examples

Experimental program
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Effect test

Embodiment 1

[0026] The aero-engine central cone flow test equipment control system and its use method use PLC as the control core to control the lubricating oil in the fuel tank, the liquid level control in the fuel tank, the temperature control in the fuel tank, the particle size detection control of the lubricating oil, and the flow rate of the lubricating oil. Detection control and central cone detection control, and data collection of the flow distribution of 10 spray points on the central cone through the computer.

[0027] The control system of the aeroengine central cone flow test equipment is composed as follows: pneumatic switch solenoid valve DT41, metering solenoid valve DT82, pipeline temperature sensor 3, particle counter 4, particle detection solenoid valve DT15, fuel supply solenoid valve DT26, flow measurement solenoid valve Valve DT37, frequency conversion motor 8, pipeline pump I9, oil consumption tank liquid level sensor 10, oil consumption tank temperature sensor 11, oi...

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PUM

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Abstract

The invention discloses an aeroengine central cone flow test equipment control system and an application method thereof. The system is composed of a pneumatic switch solenoid valve DT4 (1), a metering battery valve DT8 (2), a pipeline temperature sensor (3), a particle counter (4), a particle detection solenoid valve DT1 (5), an oil supply solenoid valve DT2 (6) and a flow measuring solenoid valve DT3 (7), wherein the pneumatic switch solenoid valve DT4 (1) is connected with an oil discharging solenoid valve DT9 (26), and the pneumatic switch solenoid valve DT4 (1) is connected with a magnetically actuated liquid level sensor (27) through the metering battery valve DT8 (2). The aeroengine central cone flow test equipment control system and the application method thereof can improve the detection accuracy of an engine central cone, reduces errors caused by manual factors and enhances the engine assembling qualification rate.

Description

technical field [0001] The invention relates to the technical field of structural design and application of a flow test equipment control system, and in particular provides a control system for an aeroengine central cone flow test equipment and a method for using the same. Background technique [0002] The central cone flow tester is mainly used to test the flow distribution of 10 spray points on the central cone of the engine. In the past, the central cone flow detection equipment used the method of manually reading the indication of the measuring cup for detection, which caused large errors due to human factors and low efficiency. With PLC as the core controller, the computer collects the magnetic sensor data to eliminate human reading errors and improve efficiency. [0003] People urgently hope to obtain a control system of aeroengine central cone flow test equipment and its application method with excellent technical effect. Contents of the invention [0004] The obj...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): G01M15/00G05D27/02
Inventor 王毓谭薇秦洪运郭旭宋伟
Owner SHENYANG LIMING AERO-ENGINE GROUP CORPORATION