A Simple Pose Compensation Mechanism for Automatic Docking and Release Connector of Launch Vehicle

A technology of automatic docking and compensation mechanism, applied in transportation and packaging, space navigation equipment, space navigation ground equipment, etc., can solve problems such as complex structure, achieve small size, improve force performance, and light weight.

Inactive Publication Date: 2017-08-04
NANJING UNIV OF SCI & TECH
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

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Problems solved by technology

[0005] Therefore, the problems in the prior art are: there is a small misalignment between the ground docking device and the rocket body during the automatic docking and follow-up process, and the structure is complicated

Method used

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  • A Simple Pose Compensation Mechanism for Automatic Docking and Release Connector of Launch Vehicle
  • A Simple Pose Compensation Mechanism for Automatic Docking and Release Connector of Launch Vehicle

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Embodiment Construction

[0016] Such as figure 1 As shown, the simple pose compensation mechanism for the automatic docking and venting connector of the launch vehicle of the present invention includes a moving platform 1 and a ground connector panel 3 parallel thereto. The moving platform 1 and the ground connector panel 3 pass through at least four Evenly distributed elastic parts 2 are connected.

[0017] As a preference, such as figure 2 As shown, the elastic component 2 includes a mounting seat A21, an adjusting nut 22, an upper and lower compound rubber spring 23, a mounting seat B24, a front and rear compound rubber spring 25 and an adjusting screw 221;

[0018] The mounting base A21 is fixedly mounted on the rear side of the moving platform 1, the mounting base B24 is fixedly mounted on the front side of the ground connector panel 3, and the two ends of the front and rear composite rubber springs 25 are fixedly connected to the mounting base A21 and the mounting base B24 respectively, and th...

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Abstract

The invention discloses a simple pose compensation mechanism of an automatic docking and releasing connector for a carrier rocket, comprising a movable platform (1) and a ground connector panel (3) parallel to the movable platform, wherein the movable platform (1) is flexibly connected with the ground connector panel (3) by four same elastic parts (2). After the simple pose compensation mechanism is used, a ground docking device is automatically and accurately aligned with the rocket in the docking and follow-up process.

Description

technical field [0001] The invention belongs to the technical field of ground filling equipment for carrier rockets, in particular to a simple pose compensation mechanism for automatic docking, adding and releasing connectors of carrier rockets that can automatically and accurately align positions and has a simple structure. [0002] technical background [0003] The automatic docking technology of launch vehicles can greatly shorten the preparation time for fuel filling of rockets and other spacecraft, improve the launch efficiency, and at the same time eliminate the dangers to their own safety caused by the direct participation of staff. [0004] After long-term research by the United States, Russia, France and other countries, the "Arrow Habitat" docking method led by the United States and the "Rack Habitat" docking method headed by Russia have been formed. The "Arrow Habitat" cannot be re-docked after falling off, while the "Frame Habitat" is a rigid assembly, and the fil...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B64G5/00
CPCB64G5/00
Inventor 于存贵李保平赵纯玄柳吕丁李志刚
Owner NANJING UNIV OF SCI & TECH
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