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Instrument support dynamic characteristic analysis method and system, terminal and medium

An analysis method and technology of dynamic characteristics, applied in the direction of instruments, special data processing applications, geometric CAD, etc., can solve the hazards of the effectiveness of instrument ground tests, the environmental adaptability of products, the large dependence of ground vibration tests, and the vibration environment of bulkhead instrument supports Questions about zooming in

Active Publication Date: 2021-01-05
CHINA ACAD OF LAUNCH VEHICLE TECH
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  • Description
  • Claims
  • Application Information

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Problems solved by technology

[0002] According to previous project development experience and lessons, the bulkhead instrument bracket has the problem of severe vibration environment amplification (magnification of more than 10 times). Since this problem is generally found in the system-level test in the development stage, or even ignored, it is effective for the ground test of the instrument. Performance, product environmental adaptability, etc. are all harmful, burying serious hidden dangers for project development progress and flight reliability
In related technologies, the traditional "posteriori" vibration environment control method is usually used, which is highly dependent on ground vibration tests

Method used

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  • Instrument support dynamic characteristic analysis method and system, terminal and medium
  • Instrument support dynamic characteristic analysis method and system, terminal and medium
  • Instrument support dynamic characteristic analysis method and system, terminal and medium

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Embodiment Construction

[0023] In order to make the technical solutions and advantages in the embodiments of the present application clearer, the exemplary embodiments of the present application will be further described in detail below in conjunction with the accompanying drawings. Apparently, the described embodiments are only part of the embodiments of the present application, and Not an exhaustive list of all embodiments. It should be noted that, in the case of no conflict, the embodiments in the present application and the features in the embodiments can be combined with each other.

[0024] According to previous project development experience and lessons, the bulkhead instrument bracket has the problem of severe vibration environment amplification (magnification of more than 10 times). Since this problem is generally found in the system-level test in the development stage, or even ignored, it is effective for the ground test of the instrument. Performance, product environmental adaptability, et...

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Abstract

The embodiment of the invention provides an instrument support dynamic characteristic analysis method and system, a terminal and a medium, which relate to the carrier rocket technology. The method comprises the following steps of analyzing the vibration characteristics of an instrument support to be analyzed by adopting finite element simulation to obtain an analysis result, and determining the magnification times of the instrument support according to the analysis result, and when the magnification times do not meet the corresponding requirements, triggering the structure adjustment of the instrument support until the magnification times meet the corresponding requirements.

Description

technical field [0001] The present application relates to launch vehicle technology, in particular to a dynamic characteristic analysis method, system, terminal and medium of an instrument support. Background technique [0002] According to previous project development experience and lessons, the bulkhead instrument bracket has the problem of severe vibration environment amplification (magnification of more than 10 times). Since this problem is generally found in the system-level test in the development stage, or even ignored, it is effective for the ground test of the instrument. Performance, product environmental adaptability, etc. are all relatively harmful, burying serious hidden dangers for project development progress and flight reliability. In related technologies, the traditional "posteriori" vibration environment control method is usually used, which relies heavily on ground vibration tests. Contents of the invention [0003] Embodiments of the present applicatio...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G06F30/15G06F30/17G06F30/23G06F113/28G06F119/02G06F119/14
CPCG06F30/15G06F30/17G06F30/23G06F2113/28G06F2119/02G06F2119/14Y02T90/00
Inventor 梁祖典范新中王宁陈增奎方泽平杨东生单亦姣牛飞王晓鹏王宇锐张瑾瑜雷豹丁国元夏艳程蕾姚重阳许俊伟唐念华刘鹏张东龚旻高峰任新宇王冀宁罗波于贺方平
Owner CHINA ACAD OF LAUNCH VEHICLE TECH
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