To provide systems and methods for assembling a section of a fuselage of an aircraft.SOLUTION: The method includes transferring a half barrel section 24 of a fuselage of an aircraft along a track 110-1, 110-2 in a process direction, utilizing an indexing feature associated with the half barrel section 24 to determine a desired contour 361 for a portion of the half barrel section 24, and enforcing the desired contour 361 on the half barrel section 24 using components that enforce an inner mold line 128 and components that enforce an outer mold line 126 when the contour of the half barrel section 24 is out of tolerance from the desired contour 361.SELECTED DRAWING: Figure 3
【課題】航空機の胴体の一区分を組み立てるためのシステム及び方法が提供される。【解決手段】航空機の胴体のハーフバレル区分24を軌道110-1、110-2に沿って処理方向に送ることと、ハーフバレル区分24の一部分の所望の輪郭361を決定するために、ハーフバレル区分24の関連付けられたインデキシング特徴を利用することと、ハーフバレル区分24の輪郭が、所望の輪郭361の許容誤差の範囲外にあるときには、インナモールドライン128を強化する構成要素、及びアウタモールドライン126を強化する構成要素を用いて、ハーフバレル区分24上で所望の輪郭361を強化することと、を含む。【選択図】図3
CONTOUR ENFORCEMENT FOR LINE-ASSEMBLED FUSELAGE SEGMENTS
ラインで組み立てられる胴体セグメントのための輪郭強化
2022-05-30
Patent
Electronic Resource
Japanese
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