BEARING HOUSING OF A GAS TURBINE ENGINE

A bearing housing (30) for supporting a bearing (32) of a gas turbine engine (10). The bearing housing (30) comprises an annular body extending around an axis (11) and having an oil inlet (42) and an oil outlet (44). The bearing housing (30) further comprises an oil manifold (34) integrated into the...

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Bibliographische Detailangaben
1. Verfasser:	MORENKO, Oleg
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 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:	A bearing housing (30) for supporting a bearing (32) of a gas turbine engine (10). The bearing housing (30) comprises an annular body extending around an axis (11) and having an oil inlet (42) and an oil outlet (44). The bearing housing (30) further comprises an oil manifold (34) integrated into the annular body, the oil manifold (34) having an inner oil channel (60) defined in the annular body and extending circumferentially around the axis (11), the inner oil channel (60) in fluid communication with the oil inlet (42) and at least one oil jet (62) directed towards the bearing (32).