Composite fan case containment hook and improved forward debris capture

Patent metadata

Field	Value
Publication number	US-12209506-B2
Application number	US-202217591210-A
Country	US
Kind code	B2
Filing date	Feb 2, 2022
Priority date	Feb 2, 2022
Publication date	Jan 28, 2025
Grant date	Jan 28, 2025

Abstract

A fan case assembly extend along and around a center axis. The fan case assembly may comprise a barrel extending along and around the center axis, the barrel configured to fasten to a flange of an engine case. The fan case assembly may comprise a fan track liner disposed radially inward of the barrel and a containment hook, wherein the containment hook is a discrete component separate from the barrel. The containment hook may include a front segment configured to fasten to the flange, and an axial segment disposed radially inward of the barrel. The axial segment may extend between the flange and the fan track liner and the front segment may extend radially outward from an end of the axial segment. The containment hook may also include a protruding segment extending radially inward from the axial segment.

First claim

What is claimed is:

1. A fan case assembly comprising:
a center axis, the fan case assembly extending along and around the center axis;
a barrel extending along and around the center axis, the barrel configured to fasten to a flange of an engine casing;
a fan track liner disposed radially inward of the barrel, a forward edge of the fan track liner disposed aft of the flange; and
a containment hook, wherein the containment hook is a discrete component separate from the barrel, the containment hook including
a front segment configured to fasten to the flange,
an axial segment disposed radially inward of the barrel, wherein the axial segment extends along the barrel from the flange to the fan track liner, wherein the front segment extends radially outward from an end of the axial segment, and
a protruding segment extending axially and radially inward from the axial segment to the fan track liner,

wherein the forward edge of the fan track liner is located aft of a terminal end of the protruding segment and the forward edge is configured to deform radially outwardly toward the barrel to form an opening between the forward edge of the fan track liner and the terminal end of the protruding segment in response to a projectile moving radially outwardly toward the barrel so that the projectile moves into the opening and is trapped within the opening,
wherein a terminal end of the axial segment of the containment hook extends axially aft beyond the terminal end of the protruding segment of the containment hook.

2. The fan case assembly of claim 1 wherein the barrel comprises a composite material.

3. The fan case assembly of claim 1 wherein the protruding segment of the containment hook includes a first portion that extends radially inward and axially aft from the axial segment of the containment hook and a second portion that extends axially aft from the first portion toward the fan track liner, and wherein the terminal end of the protruding segment is formed on the second portion.

4. The fan case assembly of claim 1 further comprising a forward acoustic panel disposed radially inward of the axial segment of the containment hook, wherein the protruding segment of the containment hook is disposed axially between the forward acoustic panel and the fan track liner.

5. The fan case assembly of claim 1 wherein at least a portion of the axial segment of the containment hook is a frame structure comprising openings.

6. The fan case assembly of claim 1 wherein the fan track liner comprises a first honeycomb section and a second honeycomb section, wherein the first honeycomb section is disposed axially between the protruding segment of the containment hook and the second honeycomb section.

7. The fan case assembly of claim 6 wherein the first honeycomb section is lower in density than the second honeycomb section.

8. The fan case assembly of claim 7 further comprising a first abradable layer section disposed radially inward of the first honeycomb section and a second abradable layer section disposed radially inward of the second honeycomb section, wherein the first abradable layer section is lower in strength than the second abradable layer section.

9. The fan case assembly of claim 7 wherein the first honeycomb section increases in width as the first honeycomb section extends radially inward from the barrel.

10. The fan case assembly of claim 7 wherein the first honeycomb section is a constant width as the first honeycomb section extends radially inward from the barrel.

11. The fan case assembly of claim 7 wherein a shielding piece is disposed between the first honeycomb section and the barrel.

12. The fan case assembly of claim 11 wherein there is a gap between the containment hook and the shielding piece.

13. The fan case assembly of claim 1 wherein the fan track liner comprises a radially inner honeycomb layer and a radially outer honeycomb layer.

14. The fan case assembly of claim 13 wherein the radially inner honeycomb layer is lower in density than the radially outer honeycomb layer.

15. The fan case assembly of claim 13 wherein the fan track liner comprises a forward honeycomb portion disposed between the containment hook and the radially inner honeycomb layer.

16. The fan case assembly of claim 15 wherein the forward honeycomb portion is lower in density than the radially inner honeycomb layer.

17. The fan case assembly of claim 1 wherein the forward edge of the fan track liner extends axially forward and radially inwardly from the barrel to form an acute angle with the barrel such that a radial gap is formed between the forward edge of the fan track liner and the barrel thereby allowing the forward edge to deform radially outwardly.

18. A fan case assembly comprising:
a center axis, the fan case assembly extending along and around the center axis;
a barrel extending along and around the center axis, the barrel comprising a composite material and configured to fasten to a flange of an engine casing;
a fan track liner disposed radially inward of the barrel, a forward edge of the fan track liner disposed aft of the flange;
a forward acoustic panel; and
a containment hook, wherein the containment hook is a discrete component separate from the barrel, the containment hook including
a front segment configured to fasten to the flange,
an axial segment disposed radially inward of the barrel, wherein the axial segment extends along the barrel from the flange to the fan track liner, wherein the front segment extends radially outward from a front end of the axial segment, and
a protruding segment extending radially and axially inward from the axial segment to the fan track liner, wherein the forward acoustic panel is disposed radially inward of the axial segment of the containment hook, and the protruding segment of the containment hook is disposed axially between the forward acoustic panel and the fan track liner,

wherein the forward edge of the fan track liner is located aft of a terminal end of the protruding segment and the forward edge is configured to deform radially outwardly toward the barrel to form an opening between the forward edge of the fan track liner and the terminal end of the protruding segment in response to a projectile moving radially outwardly toward the barrel so that the projectile moves into the opening and is trapped within the opening,
wherein the forward edge of the fan track liner extends axially forward and radially inwardly from the barrel to form an acute angle with the barrel such that a radial gap is formed between the forward edge of the fan track liner and the barrel thereby allowing the forward edge to deform radially outwardly.

19. The fan case assembly of claim 18 wherein a terminal end of the axial segment of the containment hook extends axially aft beyond the terminal end of the protruding segment of the containment hook.

20. A fan case assembly comprising:
a center axis, the fan case assembly extending along and around the center axis;
a barrel extending along and around the center axis, the barrel configured to fasten to a flange of an engine casing;
a fan track liner disposed radially inward of the barrel, a forward edge of the fan track liner disposed aft of the flange; and
a containment hook, wherein the containment hook is a discrete component separate from the barrel, the containment hook including
a front segment configured to fasten to the flange,
an axial segment disposed radially inward of the barrel, wherein the axial segment extends along the ba

Assignees

• Rolls Royce Nam Tech Inc

Inventors

• Heeter Robert W

Classifications

• F01D11/125

  with a reinforcing structure · CPC title

• F05D2250/283

  honeycomb · CPC title

• F05D2300/603

  Composites; e.g. fibre-reinforced · CPC title

• F05D2220/36

  specially adapted for the fan of turbofan engines · CPC title

• F05D2260/96

  Preventing, counteracting or reducing vibration or noise · CPC title