Invention Grant
- Patent Title: Gas turbine engine
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Application No.: US14593623Application Date: 2015-01-09
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Publication No.: US09677417B2Publication Date: 2017-06-13
- Inventor: Mickael Drozdz
- 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: GB1401767.7 20140203
- Main IPC: F01D21/04
- IPC: F01D21/04 ; F04D29/52

Abstract:
A fan containment system has a fan case having an annular casing element for encircling an array of fan blades and a hook projecting generally radially inwardly from the annular casing element. An annular fan track liner is positioned substantially coaxial to the annular casing element, and positioned such that a forward end of the fan track liner is axially spaced from the hook so that there is a gap between the hook and the fan track liner. A bridge member spans the gap between the hook and the fan track liner, wherein the bridge member is connected to the hook and contacts a radially inner surface of the forward end of the fan track liner. The bridge member fails when impacted by a fan blade released from a hub so that the released fan blade can impact the hook and be contained by the fan containment system.
Public/Granted literature
- US20160208640A1 GAS TURBINE ENGINE Public/Granted day:2016-07-21
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