SPINNER AFT-EXTENDED FORWARD RETURN FLANGE

A spinner (15) for a fan assembly (11) of a gas turbine engine (10), a method of fabricating a spinner for a fan assembly (11) of a gas turbine engine (10), and a gas turbine engine (10) are disclosed. The fan section (11) may include a nosecap (25). The spinner (15) may include a forward end (17),...

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Bibliographische Detailangaben
Hauptverfasser:	KLING, Colin J, LUSSIER, Darin X
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	AEROPLANES AIR INTAKES FOR JET-PROPULSION PLANTS AIRCRAFT AVIATION BLASTING COMBUSTION ENGINES CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS COSMONAUTICS GAS-TURBINE PLANTS HEATING HELICOPTERS HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS LIGHTING MECHANICAL ENGINEERING PERFORMING OPERATIONS TRANSPORTING WEAPONS
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Beschreibung
Zusammenfassung:	A spinner (15) for a fan assembly (11) of a gas turbine engine (10), a method of fabricating a spinner for a fan assembly (11) of a gas turbine engine (10), and a gas turbine engine (10) are disclosed. The fan section (11) may include a nosecap (25). The spinner (15) may include a forward end (17), an aft end (18), and a return flange (30) associated with the forward end (17). The return flange (30) may include a forward flange (34) extending forward towards the nosecap (25) and an aft flange (32) extending aft towards the aft end (18).