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Precision self-correction method and system for aircraft panel manufacturing

An aircraft siding, self-correcting technology, applied in the direction of comprehensive factory control, the use of optical devices, instruments, etc., to achieve the effects of correcting manufacturing accuracy, reducing machining vibration, and fast measurement response

Active Publication Date: 2022-07-12
杨海成
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  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] This application aims at the deformation problem of the aircraft panel during the manufacturing process, and combines the visual measurement technology with the flexible tooling, aiming to provide a precision self-correction method for the manufacture of the aircraft panel

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  • Precision self-correction method and system for aircraft panel manufacturing
  • Precision self-correction method and system for aircraft panel manufacturing
  • Precision self-correction method and system for aircraft panel manufacturing

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Embodiment Construction

[0037] Example embodiments are described more fully below with reference to the accompanying drawings. Example embodiments, however, can be embodied in various forms and should not be construed as limited to the embodiments set forth herein. These embodiments are provided so that this application will be thorough and complete, and will fully convey the concept of example embodiments to those skilled in the art. The same reference numerals in the drawings denote the same or similar parts, and thus their repeated descriptions will be omitted.

[0038] Furthermore, the described features, structures, or characteristics may be combined in any suitable manner in one or more embodiments. In the following description, numerous specific details are provided in order to give a thorough understanding of the embodiments of the present application. However, those skilled in the art will appreciate that the technical solutions of the present application may be practiced without one or mo...

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Abstract

The present application provides a precision self-correction method and system for aircraft panel manufacturing. The precision self-correction method includes: arranging a visual measurement system according to the process information of the aircraft panel; during the workpiece manufacturing process, using the visual measurement system for real-time monitoring to acquire measurement data; and combining the acquired measurement data with the workpiece The theoretical data is compared to obtain the real-time error; according to the real-time error, the process parameters of the flexible tooling or manufacturing equipment are adjusted. The precision self-correction method uses the method of visual measurement of the depth of field data to monitor the deformation, the measurement range is large, and the measurement response is fast; the deformation data is fed back to the flexible tooling, and the flexibility of the flexible tooling is fully utilized to improve the rigidity of thin-walled parts and reduce machining vibration. , thereby correcting the manufacturing accuracy.

Description

technical field [0001] The present application relates to the field of aviation manufacturing, in particular to a precision self-correction method and system for aircraft panel manufacturing. Background technique [0002] Aircraft wall panels have the characteristics of large size (eg 2500mm×30000mm) and thin thickness (eg 60mm), and are typical large thin-walled parts. In the process of aircraft panel processing or assembly, in order to ensure the accuracy of the final panel, the deformation of the workpiece during processing or assembly must be controlled within a certain range. At present, the deformation problem in the manufacturing process of the aircraft panel is usually solved by manual correction after the manufacturing is completed. Under current process conditions, the accuracy of the shape of aircraft panels is ensured by tooling, for example, by the assembly frame during the assembly process. A jig is a rigid positioning technique that has no variability in the...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): G01B11/16G01B11/00
CPCG01B11/16G01B11/002Y02P90/02
Inventor 杨海成
Owner 杨海成
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