CA2894306C - Systeme fonde sur la metrologie destine au fonctionnement d'un mecanisme de fabrication souple - Google Patents

Systeme fonde sur la metrologie destine au fonctionnement d'un mecanisme de fabrication souple Download PDF

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Publication number
CA2894306C
CA2894306C CA2894306A CA2894306A CA2894306C CA 2894306 C CA2894306 C CA 2894306C CA 2894306 A CA2894306 A CA 2894306A CA 2894306 A CA2894306 A CA 2894306A CA 2894306 C CA2894306 C CA 2894306C
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Canada
Prior art keywords
end effector
fuselage
fuselage assembly
assembly
positioning
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
CA2894306A
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English (en)
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CA2894306A1 (fr
Inventor
Harinder Oberoi
Kevin Marion Barrick
Branko Sarh
Gregory Gudzinski
Yuanxin Charles Hu
Jeffrey Lawrence Miller
Melissa Ann Findlay
Jorge Alberto Arriaga
John Willard Dorsey-Palmateer
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
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Boeing Co
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Publication date
Priority claimed from US14/559,855 external-priority patent/US10046381B2/en
Application filed by Boeing Co filed Critical Boeing Co
Publication of CA2894306A1 publication Critical patent/CA2894306A1/fr
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Publication of CA2894306C publication Critical patent/CA2894306C/fr
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Abstract

Une méthode et un appareil servent à positionner un effecteur dextrémité par rapport à un assemblage de fuselage. Une configuration de lassemblage du fuselage peut être déterminée. Leffecteur dextrémité peut être positionné par rapport à lassemblage du fuselage en fonction de la configuration déterminée. Un ensemble demplacements de référence actuels peut être déterminé pour un ensemble de points de référence sur lassemblage du fuselage. Leffecteur dextrémité peut être positionné à un emplacement fonctionnel en fonction de lensemble des emplacements de référence actuels identifiés.
CA2894306A 2014-07-09 2015-06-15 Systeme fonde sur la metrologie destine au fonctionnement d'un mecanisme de fabrication souple Active CA2894306C (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
US14/559,855 US10046381B2 (en) 2014-07-09 2014-12-03 Metrology-based system for operating a flexible manufacturing system
US14/559,855 2014-12-03

Publications (2)

Publication Number Publication Date
CA2894306A1 CA2894306A1 (fr) 2016-01-09
CA2894306C true CA2894306C (fr) 2019-02-12

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ID=55027867

Family Applications (1)

Application Number Title Priority Date Filing Date
CA2894306A Active CA2894306C (fr) 2014-07-09 2015-06-15 Systeme fonde sur la metrologie destine au fonctionnement d'un mecanisme de fabrication souple

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CA (1) CA2894306C (fr)

Families Citing this family (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US10926407B2 (en) * 2016-08-24 2021-02-23 The Boeing Company Movement control for tracked robot assemblies that manufacture aircraft
US10344906B2 (en) * 2017-01-27 2019-07-09 The Boeing Company Isolated human work platform for stabilized positioning of collaborative robotics
US10795342B1 (en) 2019-04-01 2020-10-06 The Boeing Company Proximity detection in assembly environments having machinery
US10789824B1 (en) 2019-04-01 2020-09-29 The Boeing Company Proximity detection in fabrication environments having robots
US10796555B1 (en) 2019-04-01 2020-10-06 The Boeing Company Proximity detection in assembly environments having machinery
CN112660412B (zh) * 2021-01-07 2023-07-28 中国航空工业集团公司北京长城航空测控技术研究所 一种可调弱刚性大部件保形工装及飞机筒段的支撑方法
US12440991B2 (en) 2022-11-09 2025-10-14 The Boeing Company Ultra wideband location determination with predicative and power saving capabilities

Also Published As

Publication number Publication date
CA2894306A1 (fr) 2016-01-09

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