METHOD FOR MONITORING AN AIRCRAFT LANDING GEAR EMPLOYING AT LEAST ONE ACCELEROMETER SUPPORTED BY A WHEEL OF THE LANDING GEAR, AND AIRCRAFT IMPLEMENTING THIS METHOD

A method for monitoring an aircraft landing gear. The method includes using information from at least one accelerometer firmly secured to a landing gear wheel mounted to rotate on a landing gear axle to estimate an angle of deflection α of the axle at least when the wheel is in contact with the grou...

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Bibliographische Detailangaben
Hauptverfasser:	ZABULON, Joël, FANTON, Nicolas, BRUNSTEIN, Etienne, MICHAUD, Benjamin, LEKARSKI, Kyril
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	AEROPLANES AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION COSMONAUTICS DEVICES OR ARRANGEMENTS RELATED TO TYRES EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS HELICOPTERS MEASURING MEASURING ANGLES MEASURING AREAS MEASURING IRREGULARITIES OF SURFACES OR CONTOURS MEASURING LENGTH, THICKNESS OR SIMILAR LINEARDIMENSIONS PARACHUTES PERFORMING OPERATIONS PHYSICS REPAIRING, OR CONNECTING VALVES TO, INFLATABLE ELASTIC BODIESIN GENERAL TESTING TRANSPORTING TYRE CHANGING OR REPAIRING TYRE INFLATION VEHICLE TYRES VEHICLES IN GENERAL
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