Large Subassembly Relocation for Finish Machining of Wing-Fuselage Joints in Digital Final Assembly of Aircraft

Chu Hui Liu

doi:10.4028/www.scientific.net/AMR.712-715.2474

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HomeAdvanced Materials ResearchAdvanced Materials Research Vols. 712-715Large Subassembly Relocation for Finish Machining...

Large Subassembly Relocation for Finish Machining of Wing-Fuselage Joints in Digital Final Assembly of Aircraft

Abstract:

During digital final assembly of some types of aircraft, the posture of fuselage or wing must be revised in the case that real cutting allowances of some wing-fuselage joint holes are insufficient for finish machining. A constrained optimization modal is proposed to gain the optimum objective posture, which will ensure that each wing-fuselage joint has enough cutting allowance and meet all other technological requirements on the posture of fuselage or wing too.

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Periodical:

Advanced Materials Research (Volumes 712-715)

Pages:

2474-2477

DOI:

https://doi.org/10.4028/www.scientific.net/AMR.712-715.2474

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Online since:

June 2013

Authors:

Chu Hui Liu

Keywords:

Aircraft Assembly, Finish Machining, Posture Optimization, Relocation

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References

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