Invention Grant
- Patent Title: Gas turbine engine
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Application No.: US14608833Application Date: 2015-01-29
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Publication No.: US09835046B2Publication Date: 2017-12-05
- Inventor: Julian Mark Reed
- 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: GB1402577.9 20140214
- Main IPC: F01B25/16
- IPC: F01B25/16 ; F01D21/04 ; F01D25/24

Abstract:
A fan containment system for fitment around an array of radially extending fan blades mounted on a hub in an axial gas turbine engine, including: a fan case having an annular casing element for encircling an array of fan blades and an annular fan track liner lining a radially inner side of the casing element, including a first fan track liner panel positioned circumferentially adjacent a second fan track liner panel. An engagement arrangement engages the first fan track liner panel to the second, extending along at least a portion of adjacent sides of the liner panels, and is configured and the liner panels are shaped such that axial movement of the first fan track liner panel by a distance less than the length of the engagement arrangement, being measured in a direction parallel to the adjacent sides of the liner panels, disengages the first liner panel from the second.
Public/Granted literature
- US20150233262A1 GAS TURBINE ENGINE Public/Granted day:2015-08-20
Information query
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