A low power consumption, high integration and high reliability space adhesion device

Abstract

The present invention provides a space adhesion device with low power consumption, high integration and high reliability. The device includes: a connecting component for docking with an active platform; a buffer mechanism for alleviating the normal impact of the device on the target, and connection; the load-bearing structure is connected with the buffer mechanism; the front-end motor drive mechanism is connected with the buffer mechanism and is in contact with the end transmission mechanism; the end transmission mechanism for adhering the target is connected with the load-bearing structure, It is also in contact with the front-end motor driving mechanism; the sensing and electric control part is arranged on the buffer mechanism to control the entire adhesion device. Its advantages are: the device combines various parts, realizes the integration of compaction, separation and buffering of the space adhesion device on the active platform, and can realize tangential loading during collision preloading, and can be combined with two dual The differential mechanism composed of the slider mechanism realizes the flattening and centripetal loading of the spatial four-bar mechanism.

Description

technical field [0001] The invention relates to the field of space manipulation research, in particular to a space-adhesive claw device with low power consumption, high integration and high reliability for precise space manipulation. Background technique [0002] In recent years, with the increase in the number of spacecraft used, on-orbit maintenance of spacecraft, on-orbit control, recovery of invalid satellites, and controlled fall of medium and large space debris have become or will become research hotspots. The traditional capture methods of space targets mainly include mechanical arm grabbing and net capturing. The use of the above methods has its limitations, especially the requirement that the target volume should not be too large. However, spacecraft such as failed satellites, medium and large space debris, or their wreckage are often large in size, so traditional actuators are not suitable for this target. Contents of the invention [0003] The purpose of the pr...

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Problems solved by technology

[0003] The purpose of the present invention is to provide a low power consumption, high integration and high reliability space adhesion device, which combines the connection assembly, buffer mechanism, load-bearing structure, front-end motor drive mechanism, end transmission mechanism, and sensing and electric control parts. Realized the structural integration of the compaction, separation and buffering of the spatial adhesion device on the active platform, and realized the precise spatial control of the tangential loading during the collision preload, and can be combined with two double-slider mechanisms and the loading and unloading ring The spatial four-bar mechanism of differential motion improves the flattening force of the adhesive surface structure; and the space four-bar mechanism based on dry adhesive material is used in the present invention, which can well overcome the shortcomings of traditional actuators such as poor connection adaptability and insufficient precise control ability

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