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Satellite and rocket separation unlocking actuator

A technology of separation of stars and arrows and actuators, which is applied in the field of aerospace, can solve the problems of demanding parts processing accuracy and processing technology, complex connection and unlocking structure, and difficult processing and manufacturing, and achieves compact structure, convenient use and maintenance, and easy work. The effect of high reliability

Active Publication Date: 2021-12-07
TIANJIN ISTAR-SPACE TECH CO LTD +1
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

The existing connection and unlocking structure is relatively complicated, and the reliability of use is also low. In particular, the requirements for the processing accuracy and processing technology of parts are very strict, the processing cost is high, and the processing and manufacturing are difficult.

Method used

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  • Satellite and rocket separation unlocking actuator
  • Satellite and rocket separation unlocking actuator
  • Satellite and rocket separation unlocking actuator

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Embodiment Construction

[0028] It should be noted that, in the case of no conflict, the embodiments of the present invention and the features in the embodiments can be combined with each other.

[0029] In describing the present invention, it should be understood that the terms "center", "longitudinal", "transverse", "upper", "lower", "front", "rear", "left", "right", The orientations or positional relationships indicated by "vertical", "horizontal", "top", "bottom", "inner", "outer", etc. are based on the orientation or positional relationships shown in the drawings, and are only for the convenience of describing the present invention Creation and simplification of description, rather than indicating or implying that the device or element referred to must have a specific orientation, be constructed and operate in a specific orientation, and therefore should not be construed as limiting the invention. In addition, the terms "first", "second", etc. are used for descriptive purposes only, and should no...

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Abstract

The invention provides a satellite and rocket separation unlocking actuator. The satellite and rocket separation unlocking actuator comprises an actuator outer cylinder and a tail end cover installed at the lower end of the actuator outer cylinder. A guide seat and a guide frame are mounted in the actuator outer cylinder, a fixed seat is mounted in the guide seat, and a pull pin is mounted in the fixed seat; the guide frame comprises a mounting part matched with the guide seat and a guide column arranged in the mounting part; an elastic piece is mounted on the guide column, and the upper end of the elastic piece is propped against the pull pin; a memory alloy wire used for driving the fixed seat to move is installed in an inner cavity of the guide frame; and an aviation plug for electrifying the memory alloy wire is mounted on the tail end cover. According to the invention, a closed integrated design is adopted, the structure is compact, the integration degree is high, the stability is excellent during pin pulling action, and meanwhile, the tolerance to a complex electromagnetic environment is good, the use and maintenance are convenient, the unlocking speed is high, and the working reliability is high.

Description

technical field [0001] The invention belongs to the field of aerospace technology, and in particular relates to a spacer and rocket separation and unlocking actuator. Background technique [0002] The star-rocket separation and unlocking drive facility is generally connected and unlocked by connecting the unlocking device, and the separation movement of the payload and the launch vehicle is realized by separating the energy device. The existing connection and unlocking structure is relatively complicated, and the reliability of use is also low. In particular, the requirements for the processing accuracy and processing technology of the parts are very strict, the processing cost is high, and the processing and manufacturing are difficult. Therefore, it is necessary to improve the separation unlocking mechanism in the existing separation unlocking device. Contents of the invention [0003] In view of this, the present invention aims to overcome the defects in the prior art,...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64G1/64
CPCB64G1/645Y02T50/40
Inventor 张亮杨浩亮孙志超张毅刘千
Owner TIANJIN ISTAR-SPACE TECH CO LTD
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