Invention Grant
- Patent Title: Gas turbine engine
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Application No.: US15333624Application Date: 2016-10-25
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Publication No.: US10451005B2Publication Date: 2019-10-22
- Inventor: Stephane M M Baralon
- 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: GB1520620.4 20151123
- Main IPC: F02K3/06
- IPC: F02K3/06 ; F01D9/04 ; F02C7/20 ; B64D27/26
Abstract:
A gas turbine engine comprising in flow series: a fan; a series of outlet guide vanes; and a bifurcation. The outlet guide vanes are more densely distributed in a region circumferentially aligned with the bifurcation than in a region circumferentially offset from the bifurcation.
Public/Granted literature
- US20170145959A1 GAS TURBINE ENGINE Public/Granted day:2017-05-25
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