A Digital Sampling Manufacturing Method for Catheters Based on Actual Assembly Space on Arrows

A technology of actual assembly and manufacturing methods, applied in the direction of manufacturing tools, assembly machines, auxiliary devices, etc., can solve the problem that the waiting time of final assembly affects the efficiency of model final assembly, does not adapt to the development trend of digital manufacturing of launch vehicles, and cannot meet the requirements of the development of new models of heavy-duty vehicles. Demand and other issues, to achieve the effect of eliminating the waiting time for final assembly, improving the efficiency of final assembly, and efficient manufacturing

Active Publication Date: 2020-09-18
CAPITAL AEROSPACE MACHINERY +1
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

The waiting time for final assembly caused by the traditional "serial manufacturing" of on-site physical sampling and manufacturing has seriously affected the efficiency of final assembly of models, and it is no longer suitable for the development trend of digital manufacturing of launch vehicles, and can no longer meet the needs of the development of new models such as heavy-duty vehicles. The disadvantages of the "serial manufacturing" mode are becoming increasingly prominent, and it is urgent to adopt effective methods to realize the precise and efficient manufacturing of such sampling catheters

Method used

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  • A Digital Sampling Manufacturing Method for Catheters Based on Actual Assembly Space on Arrows
  • A Digital Sampling Manufacturing Method for Catheters Based on Actual Assembly Space on Arrows
  • A Digital Sampling Manufacturing Method for Catheters Based on Actual Assembly Space on Arrows

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Embodiment Construction

[0042] The present invention will be further elaborated below in conjunction with embodiment.

[0043] In the separate state where the engine and the fuel tank 1 have not yet been docked, the spatial position of the tank flange is measured; first, the model of the fuel tank 1 must be established, such as figure 1 , the fuel tank 1 is a cylindrical structure placed vertically in the axial direction; four fuel tank conduit installation flanges 3 are installed around the center of the bottom of the fuel tank 1; the bottom outer ring of the fuel tank 1 is provided with a fuel tank installation docking ring 2; Then build the model of the engine mounting plate and the engine mounting docking ring, such as figure 2 , the engine mounting plate 5 is an annular plate structure; the engine mounting plate 5 is placed horizontally; the engine mounting docking ring 6 is also a ring structure; the frame 7 is a plurality of rod-shaped structures; the frame 7 is arranged on the engine mountin...

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Abstract

The invention relates to a guide pipe digitization sampling and manufacturing method based on an actual assembly space on a rocket, and belongs to the technical field of advanced manufacturing of carrier rockets. The method includes the steps of installing four fuel tank guide pipe mounting flanges on the bottom of a fuel tank; installing four engine start valve guide pipe mounting flanges; conducting butt jointing on fuel tank mounting butt rings and engine mounting butt joint rings; measuring coordinates of the corresponding fuel tank guide pipe mounting flanges in a reference coordinate system o3x3y3z3 and vectors in three directions; simulating the relative positions of the engine start valve guide pipe mounting flanges and the fuel tank guide pipe mounting flanges; installing a firstto-be-installed guide pipe; repeatedly executing the step four to the step six three times to obtain the other three to-be-installed guide pipes; and judging assembly gaps. The guide pipe digitizationsampling and manufacturing method solves the problem that the requirement for final precise butt assembling on the rocket can be met only when the guide pipes are produced according to the actual assembly space on the rocket.

Description

technical field [0001] The invention belongs to the technical field of advanced manufacturing of carrier rockets, and relates to a digital sampling manufacturing method for conduits based on the actual assembly space on the rocket. Background technique [0002] Due to the manufacturing error of the rocket body, the manufacturing and assembly error of the engine, and the cumulative assembly error of each component, some tailor-welded ducts must be manufactured according to the actual assembly space on the rocket body to meet the requirements of precise docking assembly. In active launch vehicles, this kind of tailor-welded duct usually adopts the production mode of on-site physical sampling and manufacturing. After the final assembly reaches the corresponding section, the on-site physical sampling of the duct is carried out, and then returned to the manufacturing workshop for duct manufacturing, and then to the final assembly workshop. Trial assembly, after meeting the assemb...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B23P21/00B23K31/00B23K37/00
CPCB23K31/00B23K37/00B23P21/002
Inventor 李金全安立辉白景彬刘景铎孙伟宁肖长源潘建华张伟陈振华秦添
Owner CAPITAL AEROSPACE MACHINERY
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