SYSTEM COMPRISING A HELICOPTER ROTOR AND BEARINGS WITH SENSORS AND METHOD OF MONITORING THE SYSTEM

A system comprises a plurality of identical helicopter pitch control bearings (22a - 22d) operating under identical conditions, wherein each of the bearings (22a - 22d) is equipped with at least one sensor (30a - 30d) for measuring the same operating parameter for each of the bearings (22a - 22d) at...

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Bibliographische Detailangaben
Hauptverfasser:	Colton, Michael, Bell, Andrew
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	BEARINGS BLASTING ELEMENTS OR CRANKSHAFT MECHANISMS ENGINEERING ELEMENTS AND UNITS FLEXIBLE SHAFTS GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVEFUNCTIONING OF MACHINES OR INSTALLATIONS HEATING LIGHTING MEASURING MECHANICAL ENGINEERING PHYSICS ROTARY BODIES OTHER THAN GEARING ELEMENTS SHAFTS TESTING TESTING STATIC OR DYNAMIC BALANCE OF MACHINES ORSTRUCTURES TESTING STRUCTURES OR APPARATUS NOT OTHERWISE PROVIDED FOR THERMAL INSULATION IN GENERAL WEAPONS
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