Method and system for machining multiple holes in large-sized global shell

A hole processing method and processing system technology, applied in metal processing equipment, metal processing mechanical parts, manufacturing tools, etc., can solve the problem of lack of high-precision processing methods for large-sized spherical shells, and achieve improved processing accuracy and reliability. The effect of ensuring machining accuracy and improving accuracy

Active Publication Date: 2017-09-08
HUBEI SANJIANG AEROSPACE GRP HONGYANG ELECTROMECHANICAL
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Problems solved by technology

[0004] The invention provides a method and system for processing holes in large-scale spherical shells, which solves the technical problem of lack of high-precision processing methods for large-scale spherical shells in the prior art

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  • Method and system for machining multiple holes in large-sized global shell
  • Method and system for machining multiple holes in large-sized global shell

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Embodiment Construction

[0037] The embodiment of the present application solves the technical problem of the lack of high-precision machining methods for large-scale spherical shells in the prior art by providing a method and system for processing large-scale spherical shells with holes; The technical effect of machining accuracy.

[0038] In order to solve the above technical problems, the general idea of ​​the technical solution provided by the embodiment of the present application is as follows:

[0039] Through the measurement based on the three-dimensional space coordinate system, the large spherical shell is converted into three-dimensional data; and the processing system is positioned in the three-dimensional space coordinate system; the machining accuracy is greatly improved; at the same time, by combining the theoretical model of the target processing with the large spherical The three-dimensional data information comparison of the shell screens out the processing coordinates expressed based...

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Abstract

The invention belongs to the technical field of shell machining, and discloses a method for machining multiple holes in a large-sized global shell. The method includes the steps that a three-dimensional space coordinate system of the large-sized global shell is established, and three-dimensional data of the large-sized global shell are measured; position coordinates of a machining system in the three-dimensional space coordinate system are determined; a machining theoretical model of the large-sized global shell is compared with the three-dimensional data of the large-sized global shell to obtain machining coordinates based on the three-dimensional space coordinate system; the machining system is moved, and the holes are formed in the large-sized global shell based on the machining coordinates; and the steps are repeatedly executed, and the next holes are machined. The method for machining the multiple holes in the large-sized global shell is specially used for large-diameter specifications and is high in precision requirement.

Description

technical field [0001] The invention relates to the technical field of shell processing, in particular to a method and system for processing holes in a large spherical shell. Background technique [0002] Affected by the processing stress and the change in self-weight after material removal, the perforation of the spherical shell will lead to large deformation of the spherical shell, offset of the center of the ball, and difficult processing. [0003] In the prior art, the hole machining of the spherical shell is generally realized by the existing large-scale five-axis machining center. The limitation of this method is too strong. There is a lack of effective processing methods for high-precision perforated spherical shell processing in the range of machine tools. Contents of the invention [0004] The invention provides a method and system for processing holes in a large-scale spherical shell, which solves the technical problem in the prior art that there is a lack of hi...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B23B41/00B23Q17/20B23Q17/24
CPCB23B41/00B23Q17/20B23Q17/2471
Inventor 严山罗加斌
Owner HUBEI SANJIANG AEROSPACE GRP HONGYANG ELECTROMECHANICAL
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