Invention Application
- Patent Title: GAS TURBINE ENGINE
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Application No.: US15333624Application Date: 2016-10-25
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Publication No.: US20170145959A1Publication Date: 2017-05-25
- 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
- Priority: GB1520620.4 20151123
- Main IPC: F02K3/06
- IPC: F02K3/06
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
- US10451005B2 Gas turbine engine Public/Granted day:2019-10-22
Information query
