The patent badge is an abbreviated version of the USPTO patent document. The patent badge does contain a link to the full patent document.

The patent badge is an abbreviated version of the USPTO patent document. The patent badge covers the following: Patent number, Date patent was issued, Date patent was filed, Title of the patent, Applicant, Inventor, Assignee, Attorney firm, Primary examiner, Assistant examiner, CPCs, and Abstract. The patent badge does contain a link to the full patent document (in Adobe Acrobat format, aka pdf). To download or print any patent click here.

Date of Patent:
Sep. 10, 2002

Filed:

Dec. 14, 1999
Applicant:
Inventors:

Adam M Bagnall, Derby, GB;

Kevin P Vyze, Burton on Trent, GB;

Assignee:

Rolls-Royce plc, London, GB;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F01D 2/500 ; B64C 1/114 ;
U.S. Cl.
CPC ...
F01D 2/500 ; B64C 1/114 ;
Abstract

A nose cone assembly ( ) for a gas turbine engine ( ) comprising a spinner ( ) having a generally conical forward portion ( ) and a base portion ( ). The base portion ( ) of the spinner ( ) is disposed radially inside an extended profile of the forward portion ( ). Upon the base ( ) there is a radially outwardly extending flange ( ) through which mounting fasteners ( ) are arranged to attach the spinner ( ) to a fan hub ( ) of the gas turbine engine ( ). A fairing ( ) is arranged to surround and cover the base portion ( ) of the spinner ( ) when the nose cone assembly ( ) is fitted to the fan hub ( ). The fairing ( ) having a generally circumferentially and axially smooth continuous outer surface, the profile of which continues that of the forward portion of the spinner . Fasteners ( ) preferably extend from the fairing ( ) in a substantially radially inwardly directed direction to attach the fairing ( ). At least three mounting brackets ( ) are disposed radially inside the fairing ( ) to attach the fairing ( ).


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