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Electromagnetic-triggered pressing and releasing device and using method

A release device and electromagnetic triggering technology, applied in the aerospace field, can solve the problems of short actuation time, impact load, potential safety hazards that can only be used once, large impact load, etc., and achieve reliable locking method, space and weight saving. Effect

Active Publication Date: 2021-09-21
深圳市魔方卫星科技有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] Although the traditional pyrotechnic trigger method is reliable in separation and short in actuation time, it also has the disadvantages of large impact load after triggering, obvious safety hazards and only one-time use; the invention solves the problem of pyrotechnic device-based When the compression and release device works, it will produce a large impact load, obvious safety hazards and technical problems that can only be used once. It has the advantages of simple structure, safety and reliability, low impact, no pollution and reusability.

Method used

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  • Electromagnetic-triggered pressing and releasing device and using method
  • Electromagnetic-triggered pressing and releasing device and using method
  • Electromagnetic-triggered pressing and releasing device and using method

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Embodiment Construction

[0026] Preferred embodiments of the present invention will be described in detail with reference to the accompanying drawings, so that those of ordinary skill in the art to which the invention pertains can easily realize these embodiments, but the present invention can also be realized in various forms, The present invention is therefore not limited to the embodiments described hereinafter.

[0027] Such as figure 1 , 2 As shown, an electromagnetically triggered compression release device includes: a support 1, a pin shaft 2, a spring 3, a spring retaining ring 4, and a limiting element 5;

[0028] The support 1 is fixedly connected with the outer part, the inside of the pin shaft 2 is a hollow structure and the pin shaft 2 passes through the pin shaft hole 12 and is inserted into the outer part when it is in a compressed state, and the spring one 3 is arranged on the retaining ring 4 and the pin shaft 2 Inside, the left and right ends are fixedly connected with the pin shaf...

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Abstract

The invention relates to the technical field of spaceflight, in particular to a using method of an electromagnetically-triggered pressing and releasing device which comprises a support, a pin shaft hole is formed in the support, and a pin shaft is arranged in the pin shaft hole; a spring retainer ring is arranged in the pin shaft; and a first spring is arranged on the inner side of the spring check ring. The locking mode is more reliable, the pin shaft is manually pushed to be inserted into the external fixed part until the limiting block is in contact with the support seam, and at the moment, the external part is completely pressed; meanwhile, the spring check ring is pulled out of the pin shaft without limitation, and the spring check ring is driven by the insertion rod to expand to abut against the left end of the pin shaft at the moment, so that the pin shaft is limited, the pin shaft and the spring check ring form a rigid pin, and it is guaranteed that an external component is completely pressed and fixed; compared with a single-pull-pin release mode in the prior art, more space is saved through a mode that the spring retainer ring and the pin shaft are sleeved, shrunk and released.

Description

technical field [0001] The invention relates to the field of aerospace technology, in particular to a method for using an electromagnetically triggered compression release device. Background technique [0002] In the field of aerospace technology, spacecraft compression release devices are widely used. The spacecraft compression release device is used to provide compression constraints for the spacecraft accessories during the launch phase of the spacecraft; after the spacecraft enters orbit, release the constraints on the accessories according to the instructions. [0003] Although the traditional pyrotechnic trigger method is reliable in separation and short in actuation time, it also has the disadvantages of large impact load after triggering, obvious safety hazards and only one-time use; the invention solves the problem of pyrotechnic device-based When the compression release device works, it will produce a large impact load, obvious safety hazards and technical problem...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64G1/64
CPCB64G1/645
Inventor 丁强强滕浩廖祥张浩翔
Owner 深圳市魔方卫星科技有限公司
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