发明名称 Containment casing for an aero engine
摘要 A containment assembly for a turbo fan engine, comprises a casing (30) arranged in use around a rotatable fan, to form a duct for the fan, the containment assembly comprising at least one liner element (32) disposed on an interior surface between the casing and blades (42) of a rotatable fan, the liner element comprising a body portion (34) mounted in a recess in the casing and a wall portion arranged to form part of an inner wall of the duct, the wall portion and the body portion being attached and defining a containment cavity (30a) therebetween for containment of a detached fan blade fragment in use, wherein the wall portion comprises a moveable portion (36) which is movable between a first configuration in which it lies substantially flush with the inner wall of the duct, and a second configuration in which it provides an opening through which a fan blade fragment can enter the containment cavity.
申请公布号 EP2305985(A3) 申请公布日期 2014.03.12
申请号 EP20100173514 申请日期 2010.08.20
申请人 ROLLS-ROYCE PLC 发明人 BOTTOME, KRISTOFER
分类号 F02C7/05;B64D33/02;F01D21/04;F01D25/26 主分类号 F02C7/05
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