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A test method for connector drop-off of space vehicle

A test method and carrier technology, which is applied in the testing of machines/structural components, testing of mechanical components, instruments, etc., can solve the problem of not performing connector drop-off test, inconsistent force direction and force intensity of umbilical connector, and inability to To verify the normal fall off of the connector and other issues

Active Publication Date: 2021-07-23
BEIJING LANDSPACETECH CO LTD
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

In some existing types of space vehicles, the disconnection of the connector is achieved by relying on external force to separate the plug before and after the space vehicle is ignited. The connector drop-off test, although there are very few aerospace companies will carry out the drop-off test before the launch of the space vehicle, but the test method is very irregular
[0003] The current test method only applies external force to pull the connector to make it fall off, which is regarded as the completion of the drop-off test. This method results in inconsistent force direction and force intensity for the umbilical cord connector to fall off during the drop-off test and when the space vehicle is launched. Therefore, the final test result is inaccurate, and cannot achieve the purpose of verifying whether the connector can fall off normally when the space vehicle is launched.

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  • A test method for connector drop-off of space vehicle
  • A test method for connector drop-off of space vehicle
  • A test method for connector drop-off of space vehicle

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Embodiment Construction

[0033] The technical solutions of the present invention will be further described below in conjunction with the accompanying drawings and through specific implementation methods. Spatially relative terms such as "below", "beneath", "under", "lower", "above", "on", "higher", etc. are used to facilitate description to explain the relative The orientation of two elements means that these terms are intended to encompass different orientations of the device in addition to orientations other than those shown in the figures. In addition, for example, "one element is on / under another element" may mean that two elements are in direct contact, or that there are other elements between the two elements. In addition, terms such as "first", "second", etc. are also used to describe various elements, regions, sections, etc. and should not be taken as limitations. Similar terms refer to similar elements throughout the description.

[0034] One aspect of the present invention provides a metho...

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Abstract

The invention provides a test method and a server for the drop-off of a connector of an aerospace vehicle. The method includes the following steps: collecting data parameters during the launching process of the first aerospace vehicle, calculating the acceleration of the space vehicle when the connector falls off during the launching process through the collected data, and obtaining the connector according to the acceleration and the collected data. Break away from the vector force of the vehicle and the force direction of the vector force, connect the space vehicle to be tested with the same specification to the connector, and apply the vector force to the connector, observe whether the connector can fall off, and then complete the test. The connector drop-off test method of the present invention can simulate the state of the connector falling off when the space vehicle is launched during the connector drop-off test process of the space vehicle to be tested, so as to realize a standardized drop-off test for the connector before the space vehicle launch , to make the test results more accurate, so as to achieve the purpose of connector drop-off test and improve the success rate of space vehicle launch.

Description

technical field [0001] The invention relates to the technical field of launch of space vehicles, in particular to a method for testing the disconnection of connectors of space vehicles. Background technique [0002] Usually, the liquid-carrying aerospace vehicle needs to be connected and refueled through the connector before take-off, and the connector needs to be separated from the vehicle after the refilling is completed. In some existing types of space vehicles, the disconnection of the connector is achieved by relying on external force to separate the plug before and after the space vehicle is ignited. Although there are very few aerospace companies that conduct drop-off tests before launch of space vehicles, the test methods are very irregular. [0003] The current test method only applies external force to pull the connector to make it fall off, which is regarded as the completion of the drop-off test. This method results in inconsistent force direction and force inte...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): G01M13/00
CPCG01M13/00
Inventor 徐畅张昌武李文拔
Owner BEIJING LANDSPACETECH CO LTD