Apparatus for balancing gas turbine engines

A system for balancing a rotating assembly including a gas turbine engine is provided whicch includes a plurality of couplers(100) configured to couple the engine to a rotating load such that torque from the engine is transmitted to the rotating load through the plurality of couplers. Each coupler i...

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Bibliographische Detailangaben
Hauptverfasser:	LEE, MICHAEL, ADELMANN, WILLIAM JOSEPH, DIX, BRIAN EDWARD, FREEDMAN, MAX
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	BLASTING ENGINE PLANTS IN GENERAL ENGINEERING ELEMENTS AND UNITS GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVEFUNCTIONING OF MACHINES OR INSTALLATIONS HEATING LIGHTING MACHINES OR ENGINES IN GENERAL MEANS FOR DAMPING VIBRATION MECHANICAL ENGINEERING NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES NON-POSITIVE DISPLACEMENT PUMPS POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS PUMPS FOR LIQUIDS OR ELASTIC FLUIDS SHOCK-ABSORBERS SPRINGS STEAM ENGINES THERMAL INSULATION IN GENERAL WEAPONS
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Beschreibung
Zusammenfassung:	A system for balancing a rotating assembly including a gas turbine engine is provided whicch includes a plurality of couplers(100) configured to couple the engine to a rotating load such that torque from the engine is transmitted to the rotating load through the plurality of couplers. Each coupler includes a head portion (106), an elongated shank portion (110) extending from the head portion along a longitudinal axis (112) of the coupler, and a threaded stud (120) extending from the head portion along the longitudinal axis and opposite the shank portion. A balance weight is configured to be coupled to each of the plurality of couplers.