PROCEDE DE DETECTION D'UN DEFAUT MECANIQUE D'UN GENERATEUR DE GAZ D'UNE TURBOMACHINE D'UN AERONEF ET DISPOSITIF DE MISE EN ŒUVRE CORRESPONDANT

The invention relates to a method for detecting a mechanical defect in an aircraft gas generator or in an apparatus mounted onto theon an accessory gearbox connected to said generator. Said method is characterized in that it includes: a step (E1) for of creating, before commissioning of the aircraft...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	MERCIER-CALVAIRAC, FABIEN, VALLART, PHILIPPE
Format:	Patent
Sprache:	fre
Schlagworte:	MEASURING MEASURING FORCE, STRESS, TORQUE, WORK, MECHANICAL POWER,MECHANICAL EFFICIENCY, OR FLUID PRESSURE PHYSICS TESTING TESTING STATIC OR DYNAMIC BALANCE OF MACHINES ORSTRUCTURES TESTING STRUCTURES OR APPARATUS NOT OTHERWISE PROVIDED FOR
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