SYSTEM AND METHOD FOR MACHINE DIAGNOSIS

A system (1A; 1D, 1E), comprises: a frame (F); a plurality of machines (10A-10E) mounted on the frame (F), each machine (10A-10E) having an actuator (101, 102, 14) and being operable in an defined condition; one or more controllers (11) to control the actuators (101, 102, 14) so as to exert an excit...

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Bibliographische Detailangaben
Hauptverfasser:	CICIRIELLO, Lucia, BAUER, Johannes Gabriel
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	AIRCRAFT AVIATION CONTROL OR REGULATING SYSTEMS IN GENERAL CONTROLLING COSMONAUTICS DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING ORREPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR FUNCTIONAL ELEMENTS OF SUCH SYSTEMS GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLYADAPTED FOR USE IN CONNECTION WITH AIRCRAFT HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFTCOMPONENTS, NOT OTHERWISE PROVIDED FOR MEASUREMENT OF MECHANICAL VIBRATIONS OR ULTRASONIC, SONIC ORINFRASONIC WAVES MEASURING MONITORING OR TESTING ARRANGEMENTS FOR SUCH SYSTEMS ORELEMENTS PERFORMING OPERATIONS PHYSICS REGULATING TESTING TRANSPORTING
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Beschreibung
Zusammenfassung:	A system (1A; 1D, 1E), comprises: a frame (F); a plurality of machines (10A-10E) mounted on the frame (F), each machine (10A-10E) having an actuator (101, 102, 14) and being operable in an defined condition; one or more controllers (11) to control the actuators (101, 102, 14) so as to exert an excitation of each of the machines (10A-10E); at least one sensor (12, 108) to measure at least one response indicator of a response of the system (1A; 1D, 1E) to the excitations of the machines (10A-10E); and a diagnosis system (13) adapted to receive the at least one measured response indicator.