公开(公告)号：US09835046B2

公开(公告)日：2017-12-05

申请号：US14608833

申请日：2015-01-29

Applicant: ROLLS-ROYCE PLC

Inventor： Julian Mark Reed

IPC: F01B25/16 ,  F01D21/04 ,  F01D25/24

CPC classification number: F01D21/045 ,  F01D25/246 ,  F05D2220/36 ,  F05D2250/294 ,  F05D2260/36 ,  Y02T50/671

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.

公开(公告)号：US09683490B2

公开(公告)日：2017-06-20

申请号：US14529810

申请日：2014-10-31

Applicant: ROLLS-ROYCE PLC

Inventor： Cedric Brett Harper ,  Ian Colin Deuchar Care ,  Julian Mark Reed

IPC: F02C7/05 ,  F01D11/12 ,  F01D21/04 ,  F02K3/06 ,  F01D21/10 ,  F01D25/24

CPC classification number: F02C7/05 ,  F01D11/122 ,  F01D21/04 ,  F01D21/045 ,  F01D21/10 ,  F01D25/246 ,  F02K3/06 ,  F05D2220/36

Abstract: A fan containment system includes an annular casing element and a hook projecting in a generally radially inward direction from the annular casing element. A fan track liner is connected to the hook via a fastener. The fan track liner has a forward end proximal to the hook and a rearward end distal to the hook. A pivot member protrudes radially inward from the annular casing element and is arranged and positioned between the forward and rearward end of the fan track liner such that a forward portion of the fan track liner is pivotable about the pivot member, so that upon release of a fan blade the forward portion of the fan track liner pivots about the pivot member into a voidal region provided between the annular casing element and the forward portion of the fan track liner to encourage engagement of the hook with a released fan blade.

公开(公告)号：US10294794B2

公开(公告)日：2019-05-21

申请号：US14835342

申请日：2015-08-25

Applicant: ROLLS-ROYCE PLC

Inventor： Julian Mark Reed

IPC: F01D5/06 ,  F01D21/04 ,  F04D29/52 ,  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. The fan containment system comprises a fan case having an annular casing element for encircling an array of fan blades and a hook projecting in a generally radially inward direction from the annular casing element. An annular fan track liner is provided comprising a first fan track liner panel positioned circumferentially adjacent a second fan track liner panel. A coupling connects the first fan track liner panel to the second fan track liner panel and the first fan track liner panel and the second fan track liner panel each comprise a groove along an axial face thereof and a portion of the coupling is received in each of said grooves.