OPERATING METHOD FOR A POSITIONING SYSTEM

The invention relates to an operating method for a positioning system 1, in particular for the structural assembly of aircraft, wherein the positioning system 1 comprises a plurality of positioners 2a, 2b, 2c, each of which has at least one manipulator M. The manipulators M grasp a component B and m...

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Main Authors HACKER, JENS, MEISSNER, ALEXANDER, BIYIKLIOGLU, NIHAT, MBAREK, TAOUFIK, POPPE, DIRK
Format Patent
LanguageEnglish
French
Published 24.03.2020
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Abstract The invention relates to an operating method for a positioning system 1, in particular for the structural assembly of aircraft, wherein the positioning system 1 comprises a plurality of positioners 2a, 2b, 2c, each of which has at least one manipulator M. The manipulators M grasp a component B and manipulate it in a synchronised manner, while it is jointly grasped by the manipulators M. La présente invention concerne un procédé pour faire fonctionner un système de positionnement (1), notamment pour le montage de structures d'aéronefs, le système de positionnement (1) comprenant plusieurs dispositifs de positionnement (2a, 2b, 2c) qui présentent respectivement au moins un manipulateur (M). Les manipulateurs (M) se saisissent d'une pièce de structure (B) et la manipulent de manière synchrone alors que ladite pièce est tenue communément par les manipulateurs (M).
AbstractList The invention relates to an operating method for a positioning system 1, in particular for the structural assembly of aircraft, wherein the positioning system 1 comprises a plurality of positioners 2a, 2b, 2c, each of which has at least one manipulator M. The manipulators M grasp a component B and manipulate it in a synchronised manner, while it is jointly grasped by the manipulators M. La présente invention concerne un procédé pour faire fonctionner un système de positionnement (1), notamment pour le montage de structures d'aéronefs, le système de positionnement (1) comprenant plusieurs dispositifs de positionnement (2a, 2b, 2c) qui présentent respectivement au moins un manipulateur (M). Les manipulateurs (M) se saisissent d'une pièce de structure (B) et la manipulent de manière synchrone alors que ladite pièce est tenue communément par les manipulateurs (M).
Author POPPE, DIRK
HACKER, JENS
MBAREK, TAOUFIK
BIYIKLIOGLU, NIHAT
MEISSNER, ALEXANDER
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DocumentTitleAlternate PROCEDE POUR FAIRE FONCTIONNER UN SYSTEME DE POSITIONNEMENT
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Snippet The invention relates to an operating method for a positioning system 1, in particular for the structural assembly of aircraft, wherein the positioning system...
SourceID epo
SourceType Open Access Repository
SubjectTerms AIRCRAFT
AVIATION
CHAMBERS PROVIDED WITH MANIPULATION DEVICES
COMBINED OPERATIONS
COSMONAUTICS
DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING ORREPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR
GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLYADAPTED FOR USE IN CONNECTION WITH AIRCRAFT
HAND TOOLS
HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFTCOMPONENTS, NOT OTHERWISE PROVIDED FOR
MACHINE TOOLS
MANIPULATORS
METAL-WORKING NOT OTHERWISE PROVIDED FOR
OTHER WORKING OF METAL
PERFORMING OPERATIONS
PORTABLE POWER-DRIVEN TOOLS
TRANSPORTING
UNIVERSAL MACHINE TOOLS
Title OPERATING METHOD FOR A POSITIONING SYSTEM
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