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Mechatronic universal butt joint device

A docking device, electromechanical technology, applied in the direction of the docking device of the spacecraft, the parts of the connecting device, the coupling device, etc. The effect of low motion control accuracy, improved docking reliability, and simple control

Inactive Publication Date: 2013-05-08
NORTHWESTERN POLYTECHNICAL UNIV
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] In order to overcome the shortcomings of existing technologies that cannot simultaneously complete mechanical connection and electrical connection and do not have universality, the present invention provides a universal docking device for mechatronics, which unifies and generalizes the interfaces of different modules, and has the functions of energy transmission, electrical Universal docking and connecting mechanism for functions such as transmission

Method used

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Embodiment Construction

[0023] The purpose of the present invention is to aim at the shortcomings and deficiencies in the prior art, on the basis of analyzing the task function requirements of the general interface system, to unify and generalize the interfaces of different modules, and to have functions such as energy transmission and electrical transmission The universal docking and connecting mechanism is an important component in future combined mechanical mechanisms (such as large combined spacecraft).

[0024] The technical solution adopted by the present invention to solve its technical problems is: based on the design ideas of universality, maneuverability, capture, buffering and shock absorption, locking (unlocking), and tensioning (separation), a design with generality, fault tolerance, and reliability is provided. , maneuverability, soft capture capability, locking capability, and interface design scheme for electrical data transmission capability. Adopt "taper rod-hole" symmetrical struct...

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Abstract

The invention discloses a mechatronic universal butt joint device. On one side of a central disk, a taper hole and a taper rod are arranged symmetrically along the original point of the central disk; the head part of the taper rod is a mushroom head; data joints and power joints are arranged on the same side as the taper rod on the central disk; and a coil is wound in the outer frame of the central disk. On the other side of the central disk, a central rod is fixed at the position of the original point along the direction of the normal line of the central disk; the central disk is connected with two chucks which are parallel to the central disk on the central rod; a bar-shaped clamping hole which has a thick end and a thin end is formed on each chuck; when the thick ends of the clamping holes on the two chucks are superposed, the thin ends are faced to opposite directions; and a cambered guide hole from which the distance to the central rod is unequal is formed on each chuck. Under the drive of a motor, a driving rod which passes through the guide holes moves along a lead screw which is vertical to the central rod, the two chucks are driven to move through the guide holes, and themoving directions of the two chucks are opposite all the time. The mechatronic universal butt joint device has a few driving elements and high reliability in the butt joint, and is easy to control and quick in the butt joint.

Description

technical field [0001] The invention relates to a combined electrical and mechanical universal docking device. Background technique [0002] At present, the mechanical connection and electrical connection between various mechanical and electrical product components are realized through different connectors, and there is no cooperation between them. [0003] Space docking is the basis for on-orbit operations such as assembly and maintenance between unmanned spacecraft, and it is also a prerequisite for on-orbit service and maintenance of spacecraft. The interface system can not only realize the modular design of the aircraft, the on-orbit assembly and on-orbit replacement of different modules, but also realize the transmission of the overall information of the modular aircraft. Therefore, a reasonable interface system is a problem that must be solved in the design of modular aircraft. The existing spacecraft docking mechanisms are mostly active and passive structures, which...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B64G1/64H01R13/629
Inventor 岳晓奎袁建平罗建军马卫华李曙光李鹏
Owner NORTHWESTERN POLYTECHNICAL UNIV
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