MANIFOLD FOR GEARED TURBOFAN ENGINE

A geared architecture (48) for a gas turbine engine (20) includes a lubricant manifold (76) for directing lubricant flow to the geared architecture (48). The manifold (76) including annular channel (80, 84) and a bowl member (82, 86) received within the annular channel (80, 84) for defining a passag...

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Bibliographische Detailangaben
Hauptverfasser:	COFFIN, James B, HAUGH, Tony
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	AIR INTAKES FOR JET-PROPULSION PLANTS BLASTING COMBUSTION ENGINES CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS CRANKCASE VENTILATING ENGINE PLANTS IN GENERAL GAS-TURBINE PLANTS HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS JET-PROPULSION PLANTS LIGHTING LUBRICATING INTERNAL COMBUSTION ENGINES LUBRICATING OF MACHINES OR ENGINES IN GENERAL 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:	A geared architecture (48) for a gas turbine engine (20) includes a lubricant manifold (76) for directing lubricant flow to the geared architecture (48). The manifold (76) including annular channel (80, 84) and a bowl member (82, 86) received within the annular channel (80, 84) for defining a passage for directing lubricant.