POWER TAKE-OFF SYSTEM AND GAS TURBINE ENGINE ASSEMBLY INCLUDING SAME

A power take-off system (100,400,500) for a gas turbine engine assembly (10) is provided. The gas turbine engine includes a first spool (40) and a second spool (42), the power take-off system including a starter (102) coupled to the second spool, and a clutch assembly (200) coupled between the start...

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Bibliographische Detailangaben
Hauptverfasser:	ORLANDO, ROBERT JOSEPH, SCHILLING, JAN CHRISTOPHER, MONIZ, THOMAS ORY, PATT, RAYMOND FELIX
Format:	Patent
Sprache:	eng ; fre
Schlagworte:	AIR INTAKES FOR JET-PROPULSION PLANTS BLASTING CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TOTRANSPORTATION COMBUSTION ENGINES CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS GAS-TURBINE PLANTS GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS LIGHTING MECHANICAL ENGINEERING TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION TECHNICAL SUBJECTS COVERED BY FORMER USPC TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINSTCLIMATE CHANGE WEAPONS
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Beschreibung
Zusammenfassung:	A power take-off system (100,400,500) for a gas turbine engine assembly (10) is provided. The gas turbine engine includes a first spool (40) and a second spool (42), the power take-off system including a starter (102) coupled to the second spool, and a clutch assembly (200) coupled between the starter and the first spool, the clutch assembly configured to couple the first spool to the starter when starting the gas turbine engine assembly.