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Space floating type fast follow-up device

A follower, floating technology, applied in the field of space vehicles, can solve the problem of no space floating fast follower report, etc.

Inactive Publication Date: 2013-12-25
ENG DESIGN & RES INST OF GENERAL ARMAMENTS DEPT
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0002] In the prior art, there is no report of space floating fast follower

Method used

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  • Space floating type fast follow-up device

Examples

Experimental program
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Effect test

Embodiment Construction

[0019] Such as figure 1 As shown, the space floating fast follower device of the present invention comprises: a floating disc 18, six swing wheel sets 19, six horizontal traction ropes 20, six vertical traction ropes 21 and a power unit 22, the floating disc 18 is a regular hexagon, Two swing wheel sets 19 are installed on the outer sides of each frame of the three separated frames of the regular hexagon, and a horizontal traction rope 20 is fixed on the horizontal support after passing through the swing wheel sets 19 respectively. 18 exerts a horizontal force, and the pulling force direction of the horizontal traction rope 20 is perpendicular to the frame of the floating disc 18 at its place. One end of the vertical traction rope 21 is fixed on the focal point of the two frames of the floating disc 18, and the other end of the vertical traction rope 21 is fixed on the vertical support to apply a vertical force to the floating disc 18. The pulling force method of the vertical ...

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Abstract

The invention relates to a space floating type fast follow-up device, which comprises a floating disc, six swinging wheel groups, six horizontal traction ropes, six vertical traction ropes and a motive power device, wherein the floating disc is in a regular hexagon, the outer side of each side frame in three separated side frames of the regular hexagon is respectively provided with two swinging wheel groups, one horizontal traction rope is fixedly arranged on a horizontal support frame after passing through the respective swinging wheel group, the horizontal force is exerted on the floating disc, one end of the vertical traction rope is fixedly arranged at the focus point part of two side frames of the floating disc, the other end of the vertical traction rope is fixedly arranged on a vertical support frame, the vertical force is exerted on the floating disc, and the bottom of the floating disc is provided with the motive power device. The space floating type fast follow-up device is mainly used for the flight testing of the space aircrafts in the microgravity environment, in order to adapt to the flight action of a target aircraft, the device can be suspended in the air in a hanging mode, and in addition, certain horizontal stiffness is maintained, so the characteristic of high-speed flight of the target aircraft is met.

Description

technical field [0001] The invention relates to a space vehicle for flight test in a microgravity environment, in particular to a space floating fast follow-up device, which adapts to the characteristics of high-speed flight of the target vehicle. Background technique [0002] In the prior art, there is no report of space floating fast follower. Contents of the invention [0003] The purpose of the invention of this application is to provide a space floating fast follow-up device, which can adapt to the target aircraft [0004] Fly at high speed. In order to accomplish the purpose of the present invention, the present invention adopts the following technical solutions: [0005] A space floating fast follow-up device of the present invention comprises: a floating disc, six oscillating wheel sets, six horizontal traction ropes, six vertical traction ropes and a power device, wherein the floating disc is a regular hexagon, and Two swing wheel sets are installed on the oute...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64G7/00
Inventor 程刚万全智浩刘建斌龚奎成王迎东李利王超杨世才郑志荣陈威
Owner ENG DESIGN & RES INST OF GENERAL ARMAMENTS DEPT
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