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Method and device for integrating multiple upper computers in aeroengine control system

An aero-engine and control system technology, applied in geometric CAD, design optimization/simulation, special data processing applications, etc., can solve the problems of confusion of the upper computer, different versions, and increased labor maintenance costs, so as to solve the problem of confusion in use and avoid The effect of controlling risk

Active Publication Date: 2021-09-03
中国航发控制系统研究所
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  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] At present, there are many personnel involved in the use of ground maintenance equipment for aero-engine control systems. When different staff members cannot determine which version of software to use, they will reinstall the software they think is appropriate, and there will be multiple identical functions on the device desktop. The host computer software, but the version is different, and there will be more and more, the host computer is more and more chaotic, which indirectly leads to the increase of manpower maintenance cost
[0004] Therefore, how to avoid the risk caused by the confusion of the use of multiple upper computers has become a technical problem to be solved urgently by those skilled in the art

Method used

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  • Method and device for integrating multiple upper computers in aeroengine control system
  • Method and device for integrating multiple upper computers in aeroengine control system
  • Method and device for integrating multiple upper computers in aeroengine control system

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Embodiment Construction

[0043] Specific embodiments of the present invention will be described in detail below in conjunction with the accompanying drawings. It should be understood that the specific embodiments described here are only used to illustrate and explain the present invention, and are not intended to limit the present invention.

[0044] As a first aspect of the present invention, a method for integrating various upper computers in an aeroengine control system is provided, wherein, such as figure 1 As shown, the aero-engine control system includes a control device and various host computers connected to the control device, each of which is used to send control commands to the control device, and the control commands sent by the various host computers are different from each other. Similarly, each host computer includes configuration information, and the integration method includes:

[0045] S110. Obtain the configuration information of each upper computer, and form the configuration info...

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Abstract

The invention discloses an integration method of multiple upper computers in an aero-engine control system, which includes: acquiring configuration information of each upper computer, and forming configuration files from the configuration information of multiple upper computers; judging whether the configuration file is Empty; when the configuration file is not empty, obtain the installation path of each upper computer in the configuration file; determine whether the installation path of each upper computer in the configuration file is successful; When the installation path is successful, the function button of each host computer is dynamically generated according to the installation path of the host computer; the left-click function and right-click function of the function button are created for each function button of the host computer. The invention also discloses an integrated device of various upper computers in the aeroengine control system. The method for integrating multiple upper computers in the aero-engine control system provided by the invention solves the problem of confusion in the use of multiple upper computers in the aero-engine control system.

Description

technical field [0001] The invention relates to the technical field of aero-engine control systems, in particular to an integration method of multiple upper computers in the aero-engine control system and an integration device for multiple upper computers in the aero-engine control system. Background technique [0002] The normal operation of the aero-engine control system requires the support of a large number of auxiliary operation software. According to different usage conditions and different functions, different host computer tools are developed to meet the data monitoring, parameter modification, sensor calibration, and software of the aero-engine control system. For operations such as burning and historical data reading, it is necessary to install and update management of so many supporting software. [0003] At present, there are many personnel involved in the use of ground maintenance equipment for aero-engine control systems. When different staff members cannot det...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): G06F30/17G06F30/20
CPCG06F30/17G06F30/20
Inventor 顾鸣祺顾春峰刘珍爽高征陈超朱帅琦
Owner 中国航发控制系统研究所
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