Remote centralized system of aircraft engine hydraulic product test equipment and control method

A product test and test equipment technology, applied in the direction of electrical program control, sequence/logic controller program control, etc., can solve the problems of difficulty in editing automatic control programs and high technical level requirements for test operators, and achieve simple design, The effect of avoiding security risks and simplifying the editing process

Pending Publication Date: 2022-04-12
BEIJING HANGKE ENGINE CONTROL SYST SCI & TECH
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

In order to reduce the consumption of human resources, the remote centralized control method is usually used to carry out the test. Because the mechanical hydraulic product test equipment of the turboshaft turboprop engine is a non-standard test equipment, the functions and control methods of different equipment are quite different, and currently only the test can be realized. The remote start and stop control of the equipment, the execution of the specific working steps of the test equipment depends on the local automatic control program, the editing of the automatic control program is difficult, and the technical level of the test operators is high.

Method used

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  • Remote centralized system of aircraft engine hydraulic product test equipment and control method
  • Remote centralized system of aircraft engine hydraulic product test equipment and control method
  • Remote centralized system of aircraft engine hydraulic product test equipment and control method

Examples

Experimental program
Comparison scheme
Effect test

Embodiment 1

[0035] Example 1. A remote centralized system for Hangfa hydraulic product test equipment, which is composed of Figure 1-3 As shown, it consists of test equipment industrial computer Ⅰ1, test equipment industrial computer Ⅱ2, test equipment industrial computer Ⅲ3, centralized control system operation server 4, remote control computer Ⅰ5, remote control computer Ⅱ6, remote control computer Ⅲ7, centralized control system storage server 8 It consists of central switch 9, emergency stop PLC master station 10, emergency stop PLC slave station I11, emergency stop PLC slave station II12, emergency stop PLC slave station III13, emergency stop button I14, emergency stop button II15, and emergency stop button III16. All test equipment industrial computers, remote control computers and servers in the system are connected through the central switch 9 to realize free matching of any remote control computer to any test equipment. The remote control computers 5, 6, and 7 are equipped with ...

Embodiment 2

[0050] Example 2. A network-based remote centralized control system for turboshaft turboprop engine mechanical hydraulic product test equipment, which consists of Figure 1-3 shown, including:

[0051] The industrial control module of the test equipment is used to execute the test steps of the automated process documents;

[0052] Centralized control system operation server for system operation management;

[0053] The remote control module is used to compile the automation process file and send the command to execute the automation process file after logging in the centralized control system operation server;

[0054] The remote emergency stop button is used to realize the remote emergency stop of the test industrial control module;

[0055] The central switch is used for data interaction between the industrial control module of the test equipment, the operation server of the centralized control system and the remote control module;

[0056] The emergency stop PLC master ...

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Abstract

The invention discloses a remote centralized system of aero-engine hydraulic product test equipment. Comprising a test equipment industrial control module used for executing test steps of an automatic process file; the centralized control system operation server is used for operation management of the system; the remote control module is used for compiling an automatic process file and sending a command for executing the automatic process file after logging in the centralized control system operation server; the remote scram button is used for realizing remote scram; the central switch is used for data interaction among the test equipment industrial control module, the centralized control system operation server and the remote control module; the sudden stop PLC master station is used for realizing automatic matching of the remote control module and the sudden stop button and sending a sudden stop instruction to the sudden stop PLC slave station; and the sudden stop PLC slave station is used for receiving the sudden stop instruction and sending the sudden stop instruction to the test equipment. According to the invention, centralized and standardized control of non-standard test equipment is realized, and potential safety hazards caused by network communication faults are avoided.

Description

technical field [0001] The invention belongs to the technical field of aero-engine testing, and in particular relates to a remote centralized system and control method of aero-engine hydraulic product testing equipment. Background technique [0002] During the product development process of aero-engine fuel control system, a life test is required to verify whether its service life meets the design requirements. Each product needs to occupy one test equipment for life test, and is equipped with one test operator to operate. The structure of mechanical hydraulic products of turboshaft turboprop engine is complicated, and the test process involves the operation of various control commands such as pressure, speed, and electronic control signals. The operation steps are complicated and require high technical level of operators. With the improvement of the product design level, the life of the product has increased significantly, and the hours of life testing have also increased ...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G05B19/05
Inventor 李伟军张海明杜鑫张九象郑宁宁
Owner BEIJING HANGKE ENGINE CONTROL SYST SCI & TECH
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