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Intelligent docking vehicle

A docking vehicle and intelligent technology, applied in the direction of rocket launchers, offensive equipment, weapon types, etc., can solve the problems of inaccurate position control, difficulty in docking the erection frame and the launch pad, etc.

Active Publication Date: 2020-06-23
北京中科宇航技术有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

However, in the existing technology, the transportation vehicle is generally used to directly hinge the transportation erection frame and the launching platform. Due to the large transportation vehicle, the position control is not accurate enough, and the transportation vehicle can only be adjusted in one dimension, which ultimately makes the Difficulty docking between the erection frame and the launch pad

Method used

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Embodiment Construction

[0034] Embodiments of the present invention are described in detail below, and examples of the embodiments are shown in the drawings, wherein the same or similar reference numerals denote the same or similar elements or elements having the same or similar functions throughout. The embodiments described below by referring to the figures are exemplary only for explaining the present invention and should not be construed as limiting the present invention.

[0035] Such as figure 1 and figure 2As shown, the intelligent docking vehicle provided in the embodiment of the present application is used for the docking between the erecting frame 600 and the launching platform 800, and includes a supporting shell 100, a Y-direction driving device 200, a Z-direction driving device 300, a bearing slide 400 and a bearing tackle 500. Wherein, the upper end of the support shell 100 is used to support the vertical frame 600; the first end of the Z-direction driving device 300 is fixedly conne...

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Abstract

The invention discloses an intelligent docking vehicle. The intelligent docking vehicle comprises a supporting shell, a Y-direction driving device, Z-direction driving devices, a bearing sliding plateand a bearing pulley. The supporting shell can bear an erecting frame; the Z-direction driving devices can drive the supporting shell to move in the Z direction; the Y-direction driving device can drive the supporting shell to move in the Y direction; and the bearing pulley is in sliding connection with the bearing sliding plate, and the bearing pulley can slide on the bearing sliding plate in the Y direction along with the supporting shell. According to the intelligent docking vehicle, after the erecting frame and a launching platform are initially positioned through a transport vehicle, theerecting frame and the launching platform are accurately positioned through the intelligent docking vehicle, so that the erecting frame and the launching platform can be quickly and simply hinged, erecting of the erecting frame along the launching platform is guaranteed, and the launching safety of a rocket is guaranteed.

Description

technical field [0001] The invention relates to the field of rocket launching ground support, in particular to an intelligent docking vehicle. Background technique [0002] After the rocket is transported to the launch site by the transport vehicle, it is necessary to further dock and erect the erection frame carrying the rocket with the launch pad before it can enter the launch state. In this process, the erection frame needs to be articulated with the launch pad with the erection support at the launch site. However, in the existing technology, the transportation vehicle is generally used to directly hinge the transportation erection frame and the launching platform. Due to the large transportation vehicle, the position control is not accurate enough, and the transportation vehicle can only be adjusted in one dimension, which ultimately makes the The docking between the erection frame and the launch pad is difficult. [0003] Therefore, it is a technical problem to be sol...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): F41F3/04
CPCF41F3/04
Inventor 王永刚刘金程滕瑶杨毅强王丽胡小伟刘仁昌周龙高鹏
Owner 北京中科宇航技术有限公司