Invention Grant
- Patent Title: Bifurcation fairing
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Application No.: US14705550Application Date: 2015-05-06
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Publication No.: US09771873B2Publication Date: 2017-09-26
- Inventor: Peter Beecroft , Richard Geoffrey Stretton , Philip Geoffrey Woodrow , Stephane Michel Marcel Baralon , Angus Roy Smith
- Applicant: ROLLS-ROYCE PLC
- Applicant Address: GB London
- Assignee: ROLLS-ROYCE plc
- Current Assignee: ROLLS-ROYCE plc
- Current Assignee Address: GB London
- Agency: Oliff PLC
- Priority: GB1408415.6 20140513
- Main IPC: F02C9/18
- IPC: F02C9/18 ; F02K3/06 ; F02K3/115 ; F02C7/18 ; F02C7/14 ; F01D9/06 ; F01D9/02 ; F01D25/24 ; F02C6/08

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.
Public/Granted literature
- US20150330236A1 BIFURCATION FAIRING Public/Granted day:2015-11-19
Information query
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