Methods and systems for inspecting aircraft fuselage frames

G - Physics – 01 – M

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G01M 17/00 (2006.01) B64F 5/00 (2006.01) G01N 23/04 (2006.01)

Patent

CA 2490059

A method for inspecting an aircraft fuselage (10) using an inspection system (12) including a moveable detector (14), wherein the method includes coupling a collision avoidance system (20) to the inspection system detector, monitoring the collision avoidance system during operation of the inspection system, and controlling operation of the inspection system with the collision avoidance system.

Cette invention concerne un procédé d'inspection du fuselage (10) d'un aéronef faisant intervenir un système (12) d'inspection comprenant un détecteur (14) mobile, Ce procédé consiste à connecter un système anticollision (12) au détecteur du système d'inspection ; à surveiller le système anticollision pendant le fonctionnement du système d'inspection ; et à contrôler le fonctionnement du système d'inspection avec le système anticollision.

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