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Spacecraft part assembly level ordinary pressure thermal test control system

A control system and thermal test technology, applied in the testing of machine/structural components, mechanical component testing, instruments, etc., can solve problems such as restricting the business expansion of the test center, improve data package management, reduce human intervention, and achieve visualization Effect

Active Publication Date: 2019-02-19
BEIJING INST OF SPACECRAFT ENVIRONMENT ENG
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Problems solved by technology

The previous management status and service level seriously restricted the business expansion of the test center

Method used

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  • Spacecraft part assembly level ordinary pressure thermal test control system
  • Spacecraft part assembly level ordinary pressure thermal test control system

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Embodiment Construction

[0021] The present invention will be described in further detail below in conjunction with the accompanying drawings, but this is only exemplary and not intended to limit the protection scope of the present invention.

[0022] see figure 1 , figure 1 It shows the module relationship diagram of the control system of the atmospheric pressure thermal test at the component level of the spacecraft part of the present invention; it includes a flow management module, a test preparation module, an independent alarm module, a test report processing module, a data processing module, a data acquisition module, an equipment control module, Resource management module and information display module; Among them, the process management module is responsible for the management and configuration of the test process, responsible for the automatic execution of the test according to the process of test preparation, independent alarm and report processing, and synchronizing the progress status of e...

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Abstract

The invention discloses a spacecraft part assembly level ordinary pressure thermal test control system. According to the spacecraft part assembly level ordinary pressure thermal test control system, aprocess management module and a data processing module are used as cores. The spacecraft part assembly level ordinary pressure thermal test control system comprises the process management module, a test preparation module, an independent alarm module, a test report processing module, a data processing module, a data collecting module, an equipment control module, a resource management module andan information exhibition module. Relevant test data of tasks are collected through the data collecting module, test equipment is controlled through the equipment control module, test preparation, independent alarm and report processing processes are dispatched through the process management module, and various information is released through the information exhibition module. After the spacecraftpart assembly level ordinary pressure thermal test control system operates, manpower is reduced, the number of managed ordinary pressure test equipment is greatly reduced, and digitization and intelligence levels of test management are improved.

Description

technical field [0001] The invention belongs to the technical field of spacecraft atmospheric pressure thermal test. Specifically, the invention relates to a control system of atmospheric pressure thermal test. The control system realizes the test resource, test process, test data, test Unified control and management of reports, unified management of various data collection and storage, real-time viewing of curves, automatic process monitoring, and automatic generation of test reports. Background technique [0002] In order to ensure the success of the space launch, the spacecraft and its components need to complete a series of environmental tests on the ground to verify the environmental adaptability of the spacecraft in orbit and during launch. The spacecraft component-level test is a general term for a series of test items carried out before the components are delivered to the final assembly, including spacecraft component-level thermal tests (vacuum thermal test and norm...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G01M99/00G01M13/00
CPCG01M13/00G01M99/002
Inventor 郑会明孙兴华李树鹏马腾飞杨力坡刘毅李丹丹
Owner BEIJING INST OF SPACECRAFT ENVIRONMENT ENG
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