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:
Jan. 01, 2002

Filed:

Jul. 24, 2000
Applicant:
Inventors:

Geoffrey M Dailey, Derby, GB;

Anthony Pidcock, Derby, GB;

Desmond Close, Derby, GB;

Assignee:

Rolls-Royce plc, London, GB;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02C 7/18 ; F02C 6/08 ;
U.S. Cl.
CPC ...
F02C 7/18 ; F02C 6/08 ;
Abstract

A combustor arrangement ( ) for a gas turbine engine ( ) comprising a combustion chamber, fuel nozzles( ), and a bled diffuser ( ) located upstream of said combustion chamber to, in use, direct an airflow from an upstream compressor ( ) into the combustor ( ). The fuel nozzles ( ) arranged in use to supply fuel into the combustion chamber where it is mixed and combusted with the airflow from the compressor ( ). The bled diffuser ( ) adapted to bleed off a portion of said airflow from a main airflow into the combustion chamber. At least one bleed duct ( ) is connected to the bled diffuser ( ) to return and direct the air bled from the diffuser ( ) to a main gas flow through the engine ( ) at a location downstream of the fuel supply means ( ). The bled air from the diffuser ( ) preferably providing cooling of a part of the gas turbine engine ( ), for example part of the turbine ( ) or combustor outlet vane ( ), downstream of the combustor ( ).


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