Nose cone assembly and gas turbine engine comprising such an assemby

A nose cone assembly 30 for a gas turbine engine 10 comprises a spinner 34 and a plurality of circumferentially spaced mounting members 36 for mounting the spinner 34 on a fan hub 6 of the gas turbine engine 10. Each of the mounting members 36 is rigid in a generally axial direction and flexible in...

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Bibliographische Detailangaben
1. Verfasser:	BAGNALL, ADAM MACGREGOR
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 ENGINE PLANTS IN GENERAL GAS-TURBINE PLANTS HEATING HELICOPTERS HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS JET-PROPULSION PLANTS LIGHTING MACHINES OR ENGINES IN GENERAL MECHANICAL ENGINEERING NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES PERFORMING OPERATIONS STEAM ENGINES TRANSPORTING WEAPONS
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Beschreibung
Zusammenfassung:	A nose cone assembly 30 for a gas turbine engine 10 comprises a spinner 34 and a plurality of circumferentially spaced mounting members 36 for mounting the spinner 34 on a fan hub 6 of the gas turbine engine 10. Each of the mounting members 36 is rigid in a generally axial direction and flexible in a generally radial direction.