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Dropout containment system for launch vehicle fueling connectors

A carrier rocket and connector technology, which is used in transportation and packaging, space navigation ground equipment, space navigation equipment, etc., can solve damage, reduce the safety and reliability of rocket launch, and the connector is prone to hang or free fall, etc. problem, achieve the effect of preventing hanging or free falling, improving safety and reliability

Active Publication Date: 2020-09-15
BEIJING LANDSPACETECH CO LTD
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] In the existing technology, when the rocket receives the take-off command from the ground control center and takes off in 0 seconds, the filling connector is prone to hang or free fall, which will cause unpredictable damage and reduce the safety and reliability of rocket launch. sex

Method used

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  • Dropout containment system for launch vehicle fueling connectors
  • Dropout containment system for launch vehicle fueling connectors
  • Dropout containment system for launch vehicle fueling connectors

Examples

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Embodiment Construction

[0044] In order to make the purposes, technical solutions and advantages of the embodiments of the present application clearer, the following will clearly illustrate the spirit of the content disclosed in the application with the accompanying drawings and detailed descriptions. After any person skilled in the art understands the embodiments of the content of the application , when it can be changed and modified by the technology taught in the content of the application, it does not depart from the spirit and scope of the content of the application.

[0045] The exemplary embodiments and descriptions of the present application are used to explain the present application, but not to limit the present application. In addition, elements / members with the same or similar numbers used in the drawings and embodiments are used to represent the same or similar parts.

[0046] The terms "first", "second", ... etc. used herein do not specifically refer to a sequence or order, nor are they...

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PUM

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Abstract

The invention provides a fall-off hold-down system for a carrier rocket and an injection connector. The fall-off hold-down system for the carrier rocket and the injection connector comprises an activerecovery unit and a passive hold-down unit, wherein the active recovery unit is used for actively withdrawing the injection connector and a pipeline thereof when the rocker takes off within 0 secondso that the injection connector and the pipeline thereof fall off from a rocket body or are far away from the rocket body; the active recovery unit is also used for pulling the injection connector andthe pipeline thereof; and the passive hold-down unit is used for pulling the injection connector and the pipeline thereof to prevent the injection connector and the pipeline thereof from overhangingor freely falling. According to the fall-off hold-down system for the carrier rocket and the injection connector, by arranging the active recovery unit and the passive hold-down unit, the injection connector and the pipeline thereof are pulled down from the rocket body or are pulled away from the rocket body first, and then the injection connector and the pipeline thereof are pulled to be locked at a preset height. The fall-off hold-down system for the carrier rocket and the injection connector can prevent the injection connector and the pipeline thereof from overhanging or freely falling whenthe rocket takes off within 0 second so that the rocket launching safety and reliability are enhanced.

Description

technical field [0001] The application belongs to the technical field of launch vehicles, and in particular relates to a fall-off containment system for a filling connector of a launch vehicle. Background technique [0002] A filling connector is provided on the launch vehicle, for example, a ground propellant storage device can fill the rocket body with fuel through the filling connector. In some launch scenarios, minutes before the rocket takes off, the rocket body is parked vertically on the launch pad, and all restrictions are lifted. The vertical arm and the filling main pipe are opened to a preset avoidance angle, and the filling connector is connected to the rocket body with the help of the restraining rope to complete the fuel replenishment before the rocket launch. [0003] In the existing technology, when the rocket receives the take-off command from the ground control center and takes off in 0 seconds, the filling connector is prone to hang or free fall, which wi...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B64G5/00
CPCB64G5/00
Inventor 韩召洋吴雪李永俊杨俊韦银利张瑜张彦杰
Owner BEIJING LANDSPACETECH CO LTD
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