A synchronous unlocking and releasing mechanism and a distributed locking and separating device

A separation device and release mechanism technology, applied in space vehicle docking devices, motor vehicles, transportation and packaging, etc., can solve the problem of satellite separation speed and separation attitude, inconsistency of independent unlocking of multi-point distribution, lack of synchronous release and unlocking mechanism and other problems, to achieve the effect of short synchronous unlocking and releasing operation time, high synchronization and high reliability

Active Publication Date: 2022-08-05
北京微纳星空科技有限公司
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  • Application Information

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Problems solved by technology

[0002] At present, the satellite-rocket separation process of micro-satellites mostly adopts multi-point distributed locking and separation devices. For multi-point distributed locking satellite-rocket separation devices, multi-point independent locking and release operations are mostly used. Due to the multi-point

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  • A synchronous unlocking and releasing mechanism and a distributed locking and separating device
  • A synchronous unlocking and releasing mechanism and a distributed locking and separating device
  • A synchronous unlocking and releasing mechanism and a distributed locking and separating device

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[0048] In order to make the purposes, technical solutions and advantages of the embodiments of the present application clearer, the technical solutions in the embodiments of the present application will be described clearly and completely below with reference to the drawings in the embodiments of the present application. Obviously, the described embodiments It is a part of the embodiments of the present application, but not all of the embodiments. The components of the embodiments of the present application generally described and illustrated in the drawings herein may be arranged and designed in a variety of different configurations.

[0049] Thus, the following detailed description of the embodiments of the application provided in the accompanying drawings is not intended to limit the scope of the application as claimed, but is merely representative of selected embodiments of the application. Based on the embodiments in the present application, all other embodiments obtained...

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Abstract

The present application relates to a synchronous unlocking and releasing mechanism and a distributed locking and separating device. The synchronous unlocking and releasing mechanism includes a base, a trigger and a release module; a sliding rod is fixedly arranged on the base, and a cover is fixedly connected to the upper end of the sliding rod; A trigger spring is arranged between the covers; the sliders are respectively connected with several release components, and the slider can drive several release components to perform the same action at the same time; the trigger is in contact with the slider. The structure of the distributed locking and separating device is as follows: the synchronous unlocking and releasing mechanism is arranged on the base, and several locking components are scattered around the synchronous unlocking and releasing mechanism. each locking assembly. In the present application, the release module drives several of the release components to perform the same action at the same time, thereby realizing the synchronous unlocking and releasing operation between the large-span multi-point locking components, with high synchronization and quick response.

Description

technical field [0001] The present application relates to the technical field of synchronous release, and in particular, to a synchronous unlocking and releasing mechanism and a distributed locking and separating device. Background technique [0002] At present, the star-arrow separation process of microsatellites mostly adopts multi-point distributed locking and separation devices. For multi-point distributed locking star-arrow separation devices, multi-point independent locking and releasing operations are mostly used. The inconsistency of the satellite will have a great impact on the separation process of the satellite and the arrow, and affect the separation speed and attitude of the satellite. Especially when the distance between the locking components is large, the synchronous release and unlocking mechanism is more lacking. SUMMARY OF THE INVENTION [0003] Application content [0004] The first objective of the present application is to provide a synchronous unlo...

Claims

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Application Information

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IPC IPC(8): B64G1/64
CPCB64G1/645
Inventor 叶强高恩宇姜秀鹏阎凯
Owner 北京微纳星空科技有限公司
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