CA2895820C - Procede de fabrication souple autonome destine a la construction d'un fuselage - Google Patents

Procede de fabrication souple autonome destine a la construction d'un fuselage Download PDF

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Publication number
CA2895820C
CA2895820C CA2895820A CA2895820A CA2895820C CA 2895820 C CA2895820 C CA 2895820C CA 2895820 A CA2895820 A CA 2895820A CA 2895820 A CA2895820 A CA 2895820A CA 2895820 C CA2895820 C CA 2895820C
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CA
Canada
Prior art keywords
fixture
assembly
tower
utility
fuselage
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Active
Application number
CA2895820A
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English (en)
Other versions
CA2895820A1 (fr
Inventor
Harinder Oberoi
Richard Driffith Reese Iv
Kevin Marion Barrick
Quang T. Do
Alan S. Draper
Alfredo Jose Gerosa
Branko Sarh
Gregory Gudzinski
Yuanxin Charles Hu
Jeffrey Lawrence Miller
Vanco Stojanoski
Michael J. Kozak
Melissa Ann Findlay
Jorge Alberto Arriaga
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Boeing Co
Original Assignee
Boeing Co
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Priority claimed from US14/559,518 external-priority patent/US10213823B2/en
Application filed by Boeing Co filed Critical Boeing Co
Publication of CA2895820A1 publication Critical patent/CA2895820A1/fr
Application granted granted Critical
Publication of CA2895820C publication Critical patent/CA2895820C/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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Abstract

Une méthode et un appareil servent à bâtir un assemblage de fuselage daéronef. Un nombre daccessoires fixes peuvent être transportés sur un plancher vers une zone dassemblage pour former un accessoire fixe dassemblage. Lassemblage de fuselage peut être bâti sur laccessoire fixe dassemblage.
CA2895820A 2014-07-09 2015-06-26 Procede de fabrication souple autonome destine a la construction d'un fuselage Active CA2895820C (fr)

Applications Claiming Priority (4)

Application Number Priority Date Filing Date Title
US201462022641P 2014-07-09 2014-07-09
US62/022,641 2014-07-09
US14/559,518 US10213823B2 (en) 2014-07-09 2014-12-03 Autonomous flexible manufacturing system for building a fuselage
US14/559,518 2014-12-03

Publications (2)

Publication Number Publication Date
CA2895820A1 CA2895820A1 (fr) 2016-01-09
CA2895820C true CA2895820C (fr) 2017-12-19

Family

ID=55027876

Family Applications (1)

Application Number Title Priority Date Filing Date
CA2895820A Active CA2895820C (fr) 2014-07-09 2015-06-26 Procede de fabrication souple autonome destine a la construction d'un fuselage

Country Status (1)

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CA (1) CA2895820C (fr)

Also Published As

Publication number Publication date
CA2895820A1 (fr) 2016-01-09

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