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A rubber winding molding pressure control device and method

A pressure control and winding forming technology, applied in the field of rubber winding forming, can solve problems such as the inability to meet the requirements of rubber winding forming of solid rocket motor insulation layer, and achieve the effect of avoiding overloading of winding pressure and constant winding pressure

Active Publication Date: 2021-08-06
DALIAN UNIV OF TECH
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] Existing pressure control methods and devices cannot meet the requirements of rubber winding molding for solid rocket motor insulation

Method used

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  • A rubber winding molding pressure control device and method
  • A rubber winding molding pressure control device and method

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Embodiment Construction

[0019] The present invention will be described in further detail below with reference to the accompanying drawings and embodiments.

[0020] This embodiment relates to a pressure control device and method for automatic winding and forming of a solid rocket motor rubber thermal insulation layer, such as figure 1 , figure 2 As shown, it mainly includes: winding roller 1, winding roller support shaft 2, thrust block 3, half worm wheel 4, worm 5, translation mechanism 6, translation guide 7, coupling 8, relay platform 9, cylinder 10. Coupling 11, servo motor 12.

[0021] The wrapping roller 1 is mounted on the wrapping roller support shaft 2, which is mounted on the translation mechanism 6 through the bearing, the left end cover and the right end cover; the thrust block 3 is mounted on one end of the relay platform 9, and the relay The other end of the platform 9 is installed with a cylinder 10; the half worm wheel disc 4 is installed on the winding roller support shaft 2, the ...

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Abstract

A rubber winding molding pressure control device and method belong to the technical field of rubber winding molding. The winding pressure roller in the device is installed on the winding pressure roller support shaft, which is installed on the translation mechanism; the thrust block is installed on one end of the relay platform; the half worm wheel is installed on the winding pressure roller support shaft, and the worm, servo motor Installed in the translation mechanism. The translation mechanism is installed on the translation guide rail, and the translation mechanism translates along the translation guide rail under the drive of the cylinder, and stops at the position of the thrust block. During the winding process, the relay platform is controlled by the numerical control mechanism to move in translation, combined with other kinematic mechanisms of the winding equipment, to ensure the winding position and posture of the winding pressure roller. The invention can ensure the required winding pressure in the rubber winding process and at the same time avoid winding pressure overload; it is suitable for the circumferential winding requirements of the solid rocket motor barrel section and the transition part at both ends of the heat insulation layer, and at the same time meets the requirements of other different types of solid rocket motor barrel sections Automatic winding pressure requirements for rubber insulation.

Description

technical field [0001] The invention relates to the technical field of rubber winding molding, in particular to a pressure control device and method for winding and molding a solid rocket motor thermal insulation layer. Background technique [0002] At present, the solid rocket motor casing is generally manufactured by the method of EPDM rubber thermal insulation inner layer and composite material wrapping the outer casing. The EPDM rubber insulation layer forming methods mainly include manual patch method and winding forming method. The winding pressure directly affects the shape of the solid rocket motor thermal insulation layer and the bonding strength and density of the thermal insulation layer, and is one of the key factors affecting the winding quality of the solid rocket motor thermal insulation layer. If the winding pressure is too small, it will directly affect the bonding strength of the thermal insulation layer; if the winding pressure is too large, the rubber de...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B29C53/80B29C53/58B29K23/00B29L9/00
CPCB29C53/581B29C53/8041B29K2023/16B29L2009/00
Inventor 侯增选苏金辉段鹏轩赵有航张迪婧李楠楠张伟超廉继杰
Owner DALIAN UNIV OF TECH