Method for optimizing track of complex revolved body and system

A trajectory optimization and rotary body technology, applied in the field of material manufacturing, can solve problems such as unsatisfactory comprehensive mechanical properties of components and difficult structure to meet design requirements, and achieve the effect of improving comprehensive mechanical properties and high efficiency

Pending Publication Date: 2021-02-09
CHENGDU AIRCRAFT INDUSTRY GROUP +1
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Problems solved by technology

However, based on the existing technology, it is difficult to meet the design requirements for the structure of the complicated r

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  • Method for optimizing track of complex revolved body and system
  • Method for optimizing track of complex revolved body and system
  • Method for optimizing track of complex revolved body and system

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[0023]The technical solutions provided by the present invention will be described in detail below in conjunction with specific examples. It should be understood that the following specific embodiments are only used to illustrate the present invention and not to limit the scope of the present invention.

[0024]The present invention generates an initial trajectory according to the requirements of component placement angle and material curvature, and then uses an equidistant offset to generate an offset trajectory. Since it is difficult to ensure the curvature requirements and angular deviation of the offset trajectory, the present invention adopts an automatic wire laying path optimization method that adopts local adjustment and global optimization. The method of the present invention makes full use of the variable curvature algorithm to generate the initial trajectory, and on the basis of taking into account the structural design requirements and the silk laying process requirements, i...

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Abstract

The invention discloses a method for optimizing a track of a complex revolved body and a system capable of realizing the method. According to the method, an initial track is generated according to a component laying angle and a material curvature requirement, then an offset track is generated by adopting equidistant offset, and the track is optimized by adopting an automatic fiber laying path optimization method adopting local adjustment and global optimization. According to the method, the variable curvature algorithm is fully utilized to generate the initial trajectory, the advantage of highefficiency of the equidistant bias algorithm is fully utilized on the basis of considering the structural design requirement and the fiber placement manufacturability requirement, the bottleneck thatthe manufacturability of the complex revolving body fiber placement trajectory is difficult to meet the design requirement is broken through, therefore, high-performance, high-efficiency and high-precision laying forming of the complex revolved body continuous fiber reinforced composite material can be achieved. Based on the optimized track, the manufacturability requirement and the structural requirement are met, and the comprehensive mechanical property of the component can be remarkably improved.

Description

technical field [0001] The invention belongs to the technical field of material manufacturing, and relates to the technology of automatic laying and forming of carbon fiber composite materials, in particular to a trajectory optimization method for manufacturing complex revolving bodies using automatic laying technology and a system capable of realizing the method. Background technique [0002] Because of the light weight and high strength properties of carbon fiber reinforced resin matrix composites, its composite components are more and more widely used in aerospace, civil and other fields. With the improvement of manufacturing technology, the shape of composite components changes from traditional open curved surface to closed curved surface, from simple shape to complex contour, and the requirements for forming track design are getting higher and higher in the process of development. [0003] For complex rotary components, a reasonable wire laying path is crucial to ensure...

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Application Information

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IPC IPC(8): G06Q10/04G06F30/20G06F17/10B29C70/54B29C70/38G06F113/26
CPCG06Q10/04G06F30/20B29C70/382B29C70/54G06F17/10G06F2113/26
Inventor 聂海平王东立谢林杉陈浩然罗辑王显峰
Owner CHENGDU AIRCRAFT INDUSTRY GROUP
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