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 | , , , , |
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Format | Patent |
Language | English French |
Published |
24.03.2020
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Subjects | |
Online Access | Get full text |
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Summary: | 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). |
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Bibliography: | Application Number: CA20122851556 |