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:
Oct. 02, 2018

Filed:

Mar. 06, 2014
Applicant:

Rolls-royce Plc, London, GB;

Inventor:
Assignee:

ROLLS-ROYCE plc, London, GB;

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F03B 11/00 (2006.01); F01D 25/08 (2006.01); F03D 11/00 (2006.01); F01D 25/12 (2006.01); F01D 9/06 (2006.01); F01D 5/08 (2006.01); F01D 25/24 (2006.01); F02C 6/08 (2006.01); F02C 7/18 (2006.01); F04D 29/54 (2006.01); F04D 29/32 (2006.01);
U.S. Cl.
CPC ...
F01D 25/12 (2013.01); F01D 5/082 (2013.01); F01D 5/085 (2013.01); F01D 9/065 (2013.01); F01D 25/246 (2013.01); F02C 6/08 (2013.01); F02C 7/185 (2013.01); F04D 29/321 (2013.01); F04D 29/542 (2013.01); F05D 2240/90 (2013.01); F05D 2260/213 (2013.01); Y02T 50/671 (2013.01); Y02T 50/673 (2013.01); Y02T 50/676 (2013.01);
Abstract

A gas turbine engine comprises a compressor, a combustion chamber, an outer casing, an inner casing and a cooling arrangement. The outer casing surrounds the compressor and the combustion chamber and the combustion chamber has turbine nozzle guide vanes. The compressor has load carrying outlet guide vanes connected to the outer casing and the inner casing. The turbine nozzle guide vanes connect the outer casing and the inner casing. The cooling arrangement comprises a cooling air duct located between the compressor and the combustion chamber. The compressor outlet guide vanes carry at least one aerodynamic fairing. A support structure supports the cooling air duct from the inner casing at two spaced positions and the support structure forms a chamber with the inner casing. The support structure comprises at least one hollow duct and each hollow duct locates behind a respective one of the aerodynamic fairings.


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