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. 26, 2017

Filed:

May. 06, 2015
Applicant:

Rolls-royce Plc, London, GB;

Inventors:

Peter Beecroft, Derby, GB;

Richard Geoffrey Stretton, Ashby-de-la-Zouch, GB;

Philip Geoffrey Woodrow, Derby, GB;

Stephane Michel Marcel Baralon, Derby, GB;

Angus Roy Smith, Derby, GB;

Assignee:

ROLLS-ROYCE plc, London, GB;

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F02C 9/18 (2006.01); F02K 3/06 (2006.01); F02K 3/115 (2006.01); F02C 7/18 (2006.01); F02C 7/14 (2006.01); F01D 9/06 (2006.01); F01D 9/02 (2006.01); F01D 25/24 (2006.01); F02C 6/08 (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 including an outlet guide vane and a bifurcation fairing is disclosed. The outlet guide vane is located in a bypass duct of the gas turbine engine downstream of a fan and is of aerofoil form. The bifurcation fairing traverses the radial extent of the bypass duct and has an upstream end that blends into a trailing edge of the outlet guide vane. The bifurcation fairing includes a scoop protruding outwards from its side corresponding to a pressure side of the upstream outlet guide vane. The scoop includes a forward facing inlet leading to a delivery conduit extending inside the bifurcation fairing for delivery in use of bypass air to one or more components of the gas turbine engine.


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