METHOD AND DEVICE FOR BALANCING GAS TURBINE ENGINE

PROBLEM TO BE SOLVED: To provide a system for balancing a rotating assembly 50 including a gas turbine engine 10. SOLUTION: The system comprises a plurality of couplers 100 for coupling the engine to a rotating load 12 to transmit torque from the engine to the rotating load via the couplers. Each of...

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Bibliographische Detailangaben
Hauptverfasser:	FREEDMAN MAX, LEE MICHAEL J, DIX BRIAN EDWARD, ADELMANN WILLIAM JOSEPH
Format:	Patent
Sprache:	eng
Schlagworte:	AIR INTAKES FOR JET-PROPULSION PLANTS BLASTING COMBUSTION ENGINES CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS ENGINE PLANTS IN GENERAL GAS-TURBINE PLANTS HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS LIGHTING MACHINES OR ENGINES IN GENERAL MECHANICAL ENGINEERING NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES STEAM ENGINES WEAPONS
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Beschreibung
Zusammenfassung:	PROBLEM TO BE SOLVED: To provide a system for balancing a rotating assembly 50 including a gas turbine engine 10. SOLUTION: The system comprises a plurality of couplers 100 for coupling the engine to a rotating load 12 to transmit torque from the engine to the rotating load via the couplers. Each of the couplers has a head portion 106, a slender shank portion 110 extending from the head portion to the longitudinal axis 112 of the coupler, and a stud 120 with a screw extending from the head portion along the longitudinal axis of the coupler to the opposite side to the shank portion. A balance weight 122 is coupled to each of the plurality of couplers. COPYRIGHT: (C)2006,JPO&NCIPI