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Single-side fast opening and closing control system of large double-top-cover mechanism of launching platform

A launch platform and control system technology, applied in the control/regulation system, rocket launcher, non-electric variable control, etc., can solve the problems of prolonging the launch preparation time, damage to the front and rear top cover mechanisms, and large inertia, so as to shorten the launch preparation Time, relative position constant, smooth switching effect

Active Publication Date: 2014-08-27
BEIJING INST OF SPACE LAUNCH TECH +1
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] The double top cover of the launch platform is a large mechanical structure with large mass and large inertia. When the top cover is opened and closed to the cut-off angle, there will be relatively severe shaking, which will affect the normal operation of the launch platform.
[0004] Existing launch platforms use an open-loop method to implement the top cover mechanism action, and the front and rear top cover action speeds are inconsistent, resulting in mutual interference between the front and rear top cover mechanisms, resulting in damage to the front and rear top cover mechanisms, and the top cover The opening and closing speed is slow , extending the launch preparation time

Method used

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  • Single-side fast opening and closing control system of large double-top-cover mechanism of launching platform
  • Single-side fast opening and closing control system of large double-top-cover mechanism of launching platform
  • Single-side fast opening and closing control system of large double-top-cover mechanism of launching platform

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Embodiment Construction

[0018] The present invention is described in detail below with reference to accompanying drawing and embodiment:

[0019] In the accompanying drawings, the front top cover is referred to as the front cover for short; the rear top cover is referred to as the back cover for short.

[0020] attached Figure 1-5 It can be seen that a large-scale double roof mechanism unilateral fast switch control system on the launch platform includes a front roof and a rear roof, and a front roof hydraulic cylinder and a rear roof hydraulic cylinder that drive the movement of the front roof and the rear roof. The top cover hydraulic cylinder and the rear top cover hydraulic cylinder are respectively connected to the hydraulic pump station through hydraulic pipelines, and the hydraulic pipelines connected to the front top cover hydraulic cylinder and the rear top cover hydraulic cylinder are respectively provided with proportional flow valves and proportional overflow valves. Valve and electroma...

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PUM

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Abstract

A single-side fast opening and closing control system of a large double-top-cover mechanism of a launching platform comprises a front top cover, a rear top cover, a front top cover hydraulic oil cylinder for driving the front top cover to move, and a rear top cover hydraulic oil cylinder for driving the rear top cover to move. Hydraulic pipelines connected with the front top cover hydraulic oil cylinder and the rear top cover hydraulic oil cylinder are respectively provided with a proportional flow valve, a proportional overflow valve and an electromagnetic directional valve. A valve micro-processing controller is connected with the proportional flow valves, the proportional overflow valves and the electromagnetic directional valves. A main controller is connected with the valve micro-processing controller and photoelectric encoders through a CAN bus. The photoelectric encoders are arranged on a front top cover mechanism and a rear top cover mechanism respectively. Double-loop individual control is performed on the front top cover and the rear top cover, and the flow of a front top cover loop and the flow of a rear top cover loop are controlled through the proportional flow valves respectively; the movement speed of the front top cover and the movement speed of the rear top cover are kept consistent, the front top cover mechanism and the rear top cover mechanism do not interfere with each other, damage to the front top cover mechanism and the rear top cover mechanism is prevented, the top covers are fast opened and closed in a double top cover linkage mode when the launching platform carries out movements of the top cover mechanism, and the launching preparation time is shortened.

Description

technical field [0001] The invention relates to a motion control system, in particular to a single-side rapid switch control system for a large-scale double top cover mechanism of a launching platform. Background technique [0002] With the continuous development of information technology, the requirements for the launch preparation time of the launch platform are getting higher and higher. Short launch preparation time, strong environmental adaptability, and high degree of intelligence have become important development directions for launch platforms in the future. [0003] The double top cover of the launch platform is a large mechanical structure with large mass and large inertia. When the top cover is opened and closed to the cut-off angle, there will be relatively violent shaking, which will affect the normal operation of the launch platform. [0004] Existing launch platforms use an open-loop method to implement the top cover mechanism action, and the front and rear to...

Claims

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Application Information

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IPC IPC(8): F41F3/077G05D27/02
Inventor 陆晶李德忠刘云秋吴齐才闫红宾卢邵伟王忻刘海阳
Owner BEIJING INST OF SPACE LAUNCH TECH
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