Space electromagnetic docking mechanism capable of repeatedly achieving locking/unlocking, and docking method thereof

A technology of a docking mechanism and an unlocking mechanism, which is applied in the aerospace field, can solve the problems of the disturbance of the attitude and position of the target spacecraft, affecting the working life of the spacecraft, and reducing the docking speed, and achieves the effects of low power consumption, small size, and consumption avoidance.

Inactive Publication Date: 2018-10-12
NANJING UNIV OF AERONAUTICS & ASTRONAUTICS
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Problems solved by technology

One is that the propellant dose during the docking process directly affects the working life of the spacecraft; the other is that in order to reduce the docking speed, the thrust in the opposite direction must be used to brake the tracking spacecraft, which will not only cause plume pollution, but also cause the target spacecraft to Attitude and Position Perturbations

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  • Space electromagnetic docking mechanism capable of repeatedly achieving locking/unlocking, and docking method thereof
  • Space electromagnetic docking mechanism capable of repeatedly achieving locking/unlocking, and docking method thereof
  • Space electromagnetic docking mechanism capable of repeatedly achieving locking/unlocking, and docking method thereof

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Embodiment Construction

[0059] The present invention will be further described below in conjunction with accompanying drawing.

[0060] Such as figure 1 As shown, a space electromagnetic docking mechanism that can repeatedly realize locking / unlocking is installed on two spacecraft to guide the precise docking of the two spacecraft, mainly including the active docking mechanism 2 and the passive docking mechanism 1. The upper end of the active docking mechanism 2 is a trumpet-shaped guide groove 3, and the lower end is a cylindrical active docking cylinder 16. The active docking cylinder 16 is equipped with active docking teeth 5, a locking / unlocking mechanism 8, an active electromagnet 7 and a buffer device 18. There is a driven gear structure 12 and a driving system on the outside. The locking / unlocking mechanism 8 relies on the driving system to realize locking / unlocking. The driving system is composed of a driving gear 10 and a motor 9. When working, the motor 9 generates torque to drive the driven ...

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Abstract

The invention discloses a space electromagnetic docking mechanism capable of repeatedly achieving locking/unlocking, and a docking method thereof. The docking mechanism comprises an active docking mechanism and a passive docking mechanism. The active docking mechanism is mounted on a target spacecraft. The passive docking mechanism is mounted on a tracking spacecraft. In the docking task process,energizing is conducted to enable two electromagnets to attract mutually, after the active docking mechanism and the passive docking mechanism are docked, a motor drives a driven gear structure to rotate, and thus the active docking mechanism and the passive docking mechanism are locked through a locking mechanism; and during a separating task, the driven gear structure is driven reversely by themotor firstly, unlocking is completed, then energizing is conducted to enable the two electromagnets to repel mutually, and thus separating is completed. According to the space electromagnetic dockingmechanism capable of repeatedly achieving locking/unlocking, and the docking method thereof, docking of the two spacecrafts is achieved through the electromagnetic action principle, consumption of apropellant and plume flow contamination can be avoided, the impact speed can be controlled to be zero theoretically through continuity and reversible controllability of electromagnetic force, and thuscollision-free docking between the two spacecrafts is achieved.

Description

technical field [0001] The invention relates to the field of aerospace technology, in particular to a space electromagnetic docking mechanism capable of repeatedly realizing locking / unlocking. Background technique [0002] With the continuous exploration, development and utilization of outer space by humans, space docking technology will play a key role in the fields of spacecraft supply, repair, maintenance, and on-orbit assembly, and has become a new research hotspot in the current aerospace field. Using thrusters based on recoil to control the position and speed of spacecraft is the mainstream method of docking technology at present, and this technology is mature, reliable, and widely used in engineering practice. 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 spacecraft; the other is that in order to reduce the docking speed, the thrust in the opposite dir...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64G1/64
CPCB64G1/646
Inventor 徐兴念文浩成龙
Owner NANJING UNIV OF AERONAUTICS & ASTRONAUTICS
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