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Electric permanent magnet butt joint and separation device and butt-joint and separation method thereof

A separation device and separation method technology, applied in the docking device of aerospace vehicles, transportation and packaging, aerospace equipment, etc., can solve the problems of complex locking device structure, increased docking distance, plume pollution, etc., and achieve no plume Effects of pollution, strong docking magnetic force and long working life

Active Publication Date: 2021-01-05
NINGBO INST OF MATERIALS TECH & ENG CHINESE ACADEMY OF SCI
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  • Abstract
  • Description
  • Claims
  • Application Information

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Problems solved by technology

[0004] The purpose of the present invention is to provide an electro-permanent magnet docking separation device and a docking separation method for the above-mentioned problems in the prior art. The device and method utilize the principle of electro-permanent magnetism to repeatedly realize docking, locking, Separation can effectively avoid propellant consumption and plume pollution, and at the same time save energy and increase the docking distance, thereby effectively solving the existing defects in the prior art such as plume pollution, high energy consumption, and complex locking device structure

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  • Electric permanent magnet butt joint and separation device and butt-joint and separation method thereof
  • Electric permanent magnet butt joint and separation device and butt-joint and separation method thereof
  • Electric permanent magnet butt joint and separation device and butt-joint and separation method thereof

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[0043] The technical solutions in the embodiments of the present invention will be described in detail below in conjunction with the accompanying drawings in the embodiments of the present invention. Obviously, the described embodiments are only some of the embodiments of the present invention, not all of them. Based on the embodiments of the present invention, all other embodiments obtained by persons of ordinary skill in the art without making creative efforts belong to the protection scope of the present invention.

[0044] Here, it should also be noted that, in order to avoid obscuring the present invention due to unnecessary details, only the structures and / or processing steps closely related to the solution according to the present invention are shown in the drawings, and the related Other details are not relevant to the invention.

[0045] Such as figure 1 , an electro-permanent magnet docking and separating device, comprising a first electro-permanent magnet docking m...

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Abstract

The invention discloses an electric permanent magnet butt joint and separation device and a butt joint and separation method thereof. The device comprises a first electric permanent magnet butt jointmechanism and a second electric permanent magnet butt joint mechanism, and each of the first electric permanent magnet butt joint mechanism and the second electric permanent magnet butt joint mechanism comprises yokes, a permanent magnet, an excitation coil and a control power supply. The magnet exciting coil is arranged on the periphery of the permanent magnet, the yokes are arranged at the two ends of the permanent magnet, and the control power supply is electrically connected with the magnet exciting coil. The problems that in the prior art, plume pollution exists in a butt joint mechanism,energy consumption is high, and a locking device is complex in structure are solved.

Description

technical field [0001] The invention relates to the technical field of docking, in particular to a precise electro-permanent magnetic docking and separating device and a docking and separating method that can repeatedly realize docking, separation and locking. Background technique [0002] In the technical fields of long-distance docking and controllable speed at the end of the large-tolerance docking mechanism, the use of thrusters based on recoil to achieve docking is the mainstream method of docking technology. This technology is mature, reliable, and has been widely used in engineering practice. application. However, there are still two main problems with this approach. One is that the propellant dose during the docking process directly affects the working life of the docking mechanism; the other is that in order to reduce the docking speed, the thrust in the opposite direction must be used for braking, which will not only cause plume pollution, but also cause disturban...

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64G1/64
CPCB64G1/646B64G1/645
Inventor 许珍林旻李金恩闫阿儒
Owner NINGBO INST OF MATERIALS TECH & ENG CHINESE ACADEMY OF SCI