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Separation mechanism unlocked based on rotating pressing ring

A technology of separation mechanism and rotary pressure, which is applied in the direction of motor vehicles, space navigation equipment, space navigation aircraft, etc., can solve the problems of large unlocking envelope space, large impact, heavy weight, etc., and achieve the limitation of reducing space usage, The effect of reducing the unlocking shock and reducing the space for unlocking movement

Active Publication Date: 2017-05-31
AEROSPACE DONGFANGHONG SATELLITE
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0006] The technical problem of the present invention is: to overcome the deficiencies of the prior art, and provide a separation mechanism based on the unlocking of the rotating pressure ring, which solves the problems of the existing separation mechanism, such as large volume, heavy weight, large unlocking envelope space, and large impact. It is especially suitable for the fields of star rockets, star separation and payload release of micro-nano satellites with a weight of only tens or even a few kilograms

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  • Separation mechanism unlocked based on rotating pressing ring
  • Separation mechanism unlocked based on rotating pressing ring
  • Separation mechanism unlocked based on rotating pressing ring

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Embodiment Construction

[0026] Such as Figure 1-6 As shown, a separation mechanism based on rotating the pressing ring to unlock, including: upper docking ring 1, lower docking ring 2, pressing ring 3, pressing block 4, locking lever 5, locking screw 7, locking hook 9, locking hook Base 10, pressure ring leaf spring 11, lock hook leaf spring 12, pin puller 13, separation spring support 17, separation guide cylinder 18, separation spring 19, separation guide rod 20, rotation spring 23; the upper docking ring 1 One end face is provided with an upper butt ring bevel flange 24, and the other end face is provided with a flange. The upper butt ring 1 is rigidly and fixedly connected to the separated object through the flange. An upper butt ring boss 30 and an upper butt ring gap 31; one end face of the lower butt ring 2 is provided with a lower butt ring bevel flange 25, and the other end face is provided with a flange, and the lower butt ring 2 passes through the flange and The launch vehicle or the sat...

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Abstract

The invention provides a separation mechanism unlocked based on rotating a pressing ring. An upper butt joint ring is rigidly and fixedly connected with an object to be separated; each of the upper butt joint ring and a lower butt joint ring is provided with an inclined plane flange; the upper and lower butt joint rings are tightly pressed together through retracting the pressing ring with a pressing block; a pre-tightening force is applied to the pressing ring through screwing a locking screw, so that a separation surface is tightly pressed. In an unlocking process, a pin of a pin puller is pulled out, and a lock hook rotates under the action of a pushing force of a lock hook leaf spring; one end of a locking lever is released, and the locking lever rotates under the action of a pulling force of the locking screw, so that two ends of the pressing ring are in free states and the pre-tightening force disappears; the pressing ring rotates under the action of the lock hook leaf spring and a rotary spring, and the upper butt joint ring is in a free state and then is pushed out through a separation spring, so that the upper butt joint ring is separated from the lower butt joint ring. The separation mechanism provided by the invention has the advantages that a product has small size, light weight, a small unlocking enveloping space and small impact, and is especially suitable for the fields of satellite-launcher and satellite-satellite separation, and effective load releasing of micro / nano-satellites with the weight of only dozens of, even a few of kilograms, and the like.

Description

technical field [0001] The invention relates to a separation mechanism, in particular to a separation mechanism unlocked based on a rotating pressure ring. Background technique [0002] In the research field of spacecraft separation technology, the development of separation device occupies an important position. The separation device, also known as the separator, is a mechanism for connecting and separating spacecraft, and is widely used in satellite and rocket separation, rocket stage separation, payload release and other fields. As an important part of the spacecraft, the separation device completes two different functions in the working process: during the flight process before separation, the separation device connects the two connected parts into one under the action of a certain load; performs the separation task , to ensure that the two parts being connected can complete the separation action safely and reliably. [0003] In today's aerospace field, most of the sepa...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64G1/64
CPCB64G1/645
Inventor 杨天光马灵犀张红亮扈勇强单悌磊
Owner AEROSPACE DONGFANGHONG SATELLITE