Component level vacuum thermal test control system of spacecraft department

A vacuum thermal test and control system technology, applied in the testing of machines/structural components, testing of mechanical components, instruments, etc., can solve the problems that restrict the business expansion of the test center, achieve perfect data package management, reduce human intervention, and avoid The effect of work omissions

Active Publication Date: 2020-06-30
BEIJING INST OF SPACECRAFT ENVIRONMENT ENG
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  • Abstract
  • Description
  • Claims
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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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  • Component level vacuum thermal test control system of spacecraft department
  • Component level vacuum thermal test control system of spacecraft department

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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 vacuum thermal test control system at the component level of the spacecraft part of the present invention; it includes a task management module, a data acquisition module, a process management module, a resource management module, a data processing module, an operation control module, and an information display module; among them, The task management module is responsible for the creation of tasks, and converts the entered basic test information and test condition information into a language that the equipment can recognize, stores them in the data processing module, and transmits them to other modules through the instructions of the operation control module, and generates them in ot...

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Abstract

The invention discloses a control system for a component-level vacuum thermal test of a spacecraft. The system comprises a task management module, a data acquisition module, a data processing module,a flow management module, an operation control module, a resource management module, and an information display module, and is centered on the data processing module and the operation control module.The test data and the process data of each task are collected and integrated into each function by the data acquisition module. The control system can realize monitoring and control of all devices inany control terminal or integrated terminal. Since the operation of the system, the number of device has increased from 57 tables to 139 sets without increasing the personnel and the labor intensity,so that the digital and intelligent level of test management is greatly improved.

Description

technical field [0001] The invention belongs to the technical field of spacecraft vacuum thermal test. Specifically, the invention relates to a vacuum thermal test control system. Unified control and management, and 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. Component-level tests are a general term for a series of test items conducted before components are delivered to final assembly, including component-level thermal tests (vacuum thermal test and normal pressure thermal test), mechanical tests (vibration, impact, centrifugal), comprehensive environmental tests ( Force, heat, humidity), climate te...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): G01M99/00G01M13/00
CPCG01M13/00G01M99/002
Inventor 张军刘守文郭佳诚周原陈安然臧建伯张立海王浩刘大志
Owner BEIJING INST OF SPACECRAFT ENVIRONMENT ENG
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