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:
Mar. 26, 2019

Filed:

Apr. 24, 2015
Applicant:

Rolls-royce Plc, London, GB;

Inventors:
Assignee:

ROLLS-ROYCE plc, London, GB;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02C 9/18 (2006.01); F02C 7/18 (2006.01); F02C 6/08 (2006.01); F01D 9/02 (2006.01); F01D 25/24 (2006.01); F02K 3/06 (2006.01); F01D 9/06 (2006.01); F02C 7/14 (2006.01); F02K 3/115 (2006.01);
U.S. Cl.
CPC ...
F02C 9/18 (2013.01); F01D 9/02 (2013.01); F01D 9/065 (2013.01); F01D 25/24 (2013.01); F02C 6/08 (2013.01); F02C 7/14 (2013.01); F02C 7/18 (2013.01); F02C 7/185 (2013.01); F02K 3/06 (2013.01); F02K 3/115 (2013.01); Y02T 50/675 (2013.01);
Abstract

A gas turbine engine is disclosed including a bifurcation fairing located in a bypass duct of the gas turbine engine and traversing the radial extent of the bypass duct. The bifurcation fairing has a delivery conduit inlet leading to a delivery conduit extending inside the bifurcation fairing, the delivery conduit being arranged in use for delivery of bypass air to one or more components of the gas turbine engine. A diverter conduit has a diverter conduit inlet from the delivery conduit upstream of the delivery conduit reaching the one or more components of the gas turbine engine. The diverter conduit has an outlet to a location other than the one or more components of the gas turbine engine.


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