Method and system for health monitoring of aircraft landing...

G - Physics – 01 – M

Patent

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Details

G01M 17/00 (2006.01) G01M 99/00 (2011.01) B64C 25/28 (2006.01) B64F 5/00 (2006.01)

Patent

CA 2587750

The invention relates to a new method and system for health monitoring of aircraft landing gear. The system includes sensors that are attached to the landing gear structure and equipment (e.g., one or more of brakes, tires, hydraulics, electrical systems and switches) and analyzed to report and alert personnel such as pilots, maintenance personnel, airline operators, ground crew and regulatory authorities of the health of the landing gear and the potential need for service, maintenance or replacement. The system monitors and reports critical health issues as real-time information which can be analyzed in conjunction with an extensive database of information and used to alert pilots or other relevant personnel to the condition of the landing gear and actions that may be required as a result.

L~invention concerne un nouveau procédé et un nouveau système de contrôle de l~état d~un train d~atterrissage d~un aéronef. Le système comprend des capteurs fixés à la structure et à l~équipement (notamment un ou plusieurs freins, pneumatiques, systèmes hydrauliques, systèmes électriques et commutateurs) du train d~atterrissage et analysés afin de rendre compte de son état aux pilotes, au personnel de maintenance, aux exploitants de compagnies aériennes, au personnel au sol et aux organismes réglementaires et de les avertir éventuellement de la nécessité d~effectuer une intervention, une opération de maintenance ou un remplacement. Le système contrôle et rend compte d~aspects critiques relatifs à l~état du train d~atterrissage sous la forme d~informations en temps réel susceptibles d~être analysées conjointement avec une base de données exhaustive et d~être utilisées pour avertir les pilotes ou le personnel concerné de l~état du train d~atterrissage et les informer des mesures qui peuvent s~avérer nécessaires.

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