IMAGING SYSTEM FOR FUEL TANK ANALYSIS

A method can include generating image data of an interior of a fuel tank disposed within a wing of an aircraft, and deteimining, by a processing device, an amount of wing bending of the wing of the aircraft based on the generated image data of the interior of the fuel tank. The method can further in...

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Bibliographische Detailangaben
Hauptverfasser:	LYNCH, MICHAEL A, ZAKRZEWSKI, RADOSLAW, MILLER, MARK SHERWOOD
Format:	Patent
Sprache:	eng ; fre
Schlagworte:	AEROPLANES AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION COSMONAUTICS EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS HELICOPTERS INVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIRCHEMICAL OR PHYSICAL PROPERTIES MEASURING MEASURING ANGLES MEASURING AREAS MEASURING IRREGULARITIES OF SURFACES OR CONTOURS MEASURING LENGTH, THICKNESS OR SIMILAR LINEARDIMENSIONS MEASURING VOLUME, VOLUME FLOW, MASS FLOW OR LIQUIDLEVEL METERING BY VOLUME PARACHUTES PERFORMING OPERATIONS PHYSICS TESTING TRANSPORTING
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Beschreibung
Zusammenfassung:	A method can include generating image data of an interior of a fuel tank disposed within a wing of an aircraft, and deteimining, by a processing device, an amount of wing bending of the wing of the aircraft based on the generated image data of the interior of the fuel tank. The method can further include producing, by the processing device, a fuel measurement value representing an amount of fuel contained in the fuel tank based on the amount of wing bending of the wing of the aircraft, and outputting, by the processing device, an indication of the fuel measurement value. Une méthode peut comprendre la génération de données d'image de lintérieur dun réservoir dans laile dun avion, et la détermination, au moyen dun appareil de traitement, la flexion de laile de lavion en fonction des données dimage générées à partir de lintérieur du réservoir. Le procédé peut également comprendre la détermination, par lappareil de traitement, dune valeur de mesure de carburant représentant la quantité de carburant contenue dans le réservoir de carburant daprès la flexion de laile de lavion, et la génération, par lappareil de traitement, dune indication de la valeur de mesure de carburant.