Pivoting fan track liner for blade retainment

Patent metadata

Field	Value
Publication number	US-9683490-B2
Application number	US-201414529810-A
Country	US
Kind code	B2
Filing date	Oct 31, 2014
Priority date	Nov 21, 2013
Publication date	Jun 20, 2017
Grant date	Jun 20, 2017

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.

First claim

The invention claimed is:

1. 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 comprising:
an annular casing element for encircling an array of fan blades;
a hook projecting in a generally radially inward direction from the annular casing element;
a fan track liner connected to the hook via a fastener configured so as to permit movement of the fan track liner relative to the hook, the fan track liner having a forward end proximal to the hook and a rearward end distal to the hook;
a voidal region provided between the annular casing element and a forward portion of the fan track liner; and
a pivot member protruding radially inward from the annular casing element and being 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 the 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.

2. The fan containment system according to claim 1 , wherein the pivot is located in a position such that, in use, when a fan blade is released from a hub a controlled buckling of the released blade tip is made before the released blade's centre of gravity passes the pivot point.

3. The fan containment system according to claim 1 , wherein the pivot member is positioned to be, in use, substantially axially aligned with a position between a leading edge and a trailing edge of a fan blade.

4. The fan containment system according to claim 1 , comprising a circumferential rib positioned around a radially outer surface of the annular casing element, and wherein the pivot member is substantially axially aligned with the circumferential rib.

5. The fan containment system according to claim 1 , wherein the pivot member has a substantially L-shaped cross section.

6. The fan containment system according to claim 5 , wherein the pivot member is angled towards a forward position of the fan containment system.

7. The fan containment system according to claim 1 , wherein the fan track liner is connected to the pivot member.

8. The fan containment system according to claim 7 , wherein the fan track liner is connected to the pivot member using one or more fasteners.

9. The fan containment system according to claim 1 , wherein the fan track liner comprises a tray to which a filler layer and/or an abradable layer are attached, and wherein the pivot member extends to a position proximal to the tray and distal to the abradable layer.

10. The fan containment system according to claim 1 , wherein the fan track liner comprises a series of arcuate panels arranged so that a longitudinal axis of each arcuate panel is coaxial such that the series of panels form an annulus.

11. The fan containment system according to claim 1 , wherein the fan track liner comprises an attrition layer positioned, in use, proximal to the fan blades, and wherein the attrition layer comprises a first portion and a second portion, the first portion having different properties to the second portion, so as to vary the properties of the attrition layer in an axial direction.

12. The fan containment system according to claim 11 , wherein the fan track liner comprises a filler layer connected to the attrition layer on a side of the attrition layer distal to, in use, the fan blades, wherein the filler layer is configured to be deformable at a pre-determined load, and wherein the filler layer comprises a first portion and a second portion, the first portion having different properties to the second portion, so as to vary the properties of the filler layer in an axial direction.

13. The fan containment system according to claim 1 , wherein a region of the fan track liner forward of the pivot member is shaped so as to have in an axially forward direction a gradually decreasing radial thickness.

14. 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 comprising:
an annular casing element for encircling an array of fan blades;
a hook projecting in a generally radially inward direction from the annular casing element and positioned axially forward of an array of fan blades when the fan containment system is fitted around said fan blades;
a fan track liner connected to the hook via a fastener configured so as to permit movement of the fan track liner relative to the hook, the fan track liner having a forward end proximal to the hook and a rearward end distal to the hook;
a standoff protruding radially inward from the annular casing element; and
one or more connectors securing the fan track liner to the standoff.

15. The fan containment system according to claim 14 , wherein the fan track liner is formed of an axially forward part and an axially rearward part, and wherein the axially forward and/or the axially rearward part is secured to the annular casing element via one or more standoffs.

16. The fan containment system according to claim 14 , wherein the fan track liner comprises a plurality of adjacent fan track liner panels and each fan track liner panel is connected to the standoff via one or more fasteners, and wherein the fasteners are spaced so as to break up the natural resonance of the fan track liner panels.

17. The fan containment system according to claim 14 , wherein the fan track liner comprises a plurality of adjacent fan track liner panels and each fan track liner panel is connected to the standoff via one or more fasteners, and wherein the one or more fasteners are spaced to be circumferentially out of phase with the fasteners connecting to the hook or fasteners connecting a rearward end of the fan track liner panel to the annular casing element.

18. 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 comprising:
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 and positioned axially forward of an array of fan blades when the fan containment system is fitted around said fan blades; and
a fan track liner wherein the fan track liner is connected to the fan case at the hook via a first connector and at a position axially rearward of the hook via a second connector, wherein the first connector is configured so as to deform or fail to permit movement of the fan track liner relative to the hook such that a forward region of the fan track liner can pivot towards the annular casing element when a pre-determined load is applied to the forward region of the fan track liner; and
wherein the forward region of the fan track liner is shaped so as to have in an axially rearward direction a gradually increasing radial thickness and then a decreasing radial thickness so as to form an apex adjacent the annular casing element, the gradually decreasing thickness is directly adjacent the gradually increasing thickness.

19. The fan containment system according to claim 18 , wherein the second connector connects the fan track liner to the fan case at a position adjacent the forward region of the fan track liner, and wherein the radial thick

Assignees

• Rolls Royce Plc

Inventors

• Harper Cedric Brett
• Care Ian Colin Deuchar
• Reed Julian Mark

Classifications

• F05D2220/36

  specially adapted for the fan of turbofan engines · CPC title

• F02C7/05 Primary

  having provisions for obviating the penetration of damaging objects or particles · CPC title

• F01D11/122 Primary

  with erodable or abradable material (blades having cutting or grinding tips F01D5/20) · CPC title

• F01D21/04

  responsive to undesired position of rotor relative to stator {or to breaking-off of a part of the rotor}, e.g. indicating such position · CPC title

• F02K3/06

  with front fan · CPC title