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Erecting device for rocket launching and rocket launching auxiliary system

A technology of rocket launch and auxiliary system, applied in the field of rocket launch, can solve the problems of large mass and volume of erection device, low working reliability, difficult design of driving system, etc., and achieve the effect of improving reliability

Active Publication Date: 2019-09-24
BEIJING LANDSPACETECH CO LTD
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  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

Usually, the mass and volume of the erecting device are usually large, so the design of the drive system is difficult and the work reliability is not high

Method used

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  • Erecting device for rocket launching and rocket launching auxiliary system
  • Erecting device for rocket launching and rocket launching auxiliary system
  • Erecting device for rocket launching and rocket launching auxiliary system

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Embodiment Construction

[0027] Various exemplary embodiments of the present invention will now be described in detail. The detailed description should not be considered as a limitation of the present invention, but rather as a more detailed description of certain aspects, features and embodiments of the present invention.

[0028] It will be apparent to those skilled in the art that various modifications and changes can be made in the specific embodiments of the present invention described herein without departing from the scope or spirit of the present invention. Other embodiments will be apparent to the skilled person from the description of the present invention. The specification and examples in this application are exemplary only.

[0029] The invention provides an erecting device for launching a rocket. see figure 1 with figure 2 The erecting device includes: an erecting arm 1, an umbilical rod 2 arranged on one side of the erecting arm 1, and a power cylinder 3 for rotating the umbilical r...

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Abstract

The invention provides an erecting device for rocket launching and a rocket launching auxiliary system. The erecting device comprises an erecting arm, an umbilical cord rod arranged on one side of the erecting arm and a power cylinder used for enabling the umbilical cord rod to rotate relative to the erecting arm; and one end of a erecting arm is connected with one end of the umbilical cord rod through a rotating shaft, one end of the power cylinder is fixedly connected to the part, close to the rotating shaft, of the umbilical cord rod, and the other end of the power cylinder is used for fixedly connecting with a fixing part arranged at the other side of the erecting arm. According to the erecting device and the rocket launching auxiliary system, the erecting arm can be pre-leveled by enabling the umbilical cord rod to be coaxially connected with the erecting arm, so that the umbilical cord rod can fall back quickly at a moment when the rocket took off, the structure of the erecting device is simplified, and the reliability of backward fall of the umbilical cord rod is improved.

Description

technical field [0001] The invention relates to the technical field of rocket launch, in particular to an erecting device for rocket launch and a rocket launch auxiliary system. Background technique [0002] Before the rocket is launched, it usually needs to be erected from a horizontal state to a vertical state by an erecting device. When the rocket is in a vertical state, a certain supporting force can be assisted by, for example, an erecting device to prevent the rocket from rolling over before launch. [0003] Before the rocket is ignited, in order to prevent the rocket from touching the erecting device during take-off, the erecting device needs to give up the rocket's flight space immediately before the rocket is ignited and taken off. Usually, the mass and volume of the erecting device are usually very large, so the design of the drive system is relatively difficult and the working reliability is not high. [0004] It is urgent to design an erecting device with high ...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): F41F3/04
CPCF41F3/04
Inventor 李永俊吴雪杨俊张彦杰张瑜韩召洋韦银利
Owner BEIJING LANDSPACETECH CO LTD
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