Functionally graded composite fan containment case

• US 10,443,617 B2
• Filed: 03/21/2016
• Issued: 10/15/2019
• Est. Priority Date: 07/02/2012
• Status: Active Grant

• Current Assignee: Rtx Corporation
• Original Assignee: United Technologies Corporation (Raytheon Technologies Corporation d/b/a RTX)
• Inventors: Finnigan, Peter, Voleti, Sreenivasa R., Foster, Larry, Lussier, Darin S., Aksel, Gulperi
• Primary Examiner(s): Piziali, Andrew T
• Application Number:
  US15/075,245
• Publication Number:
  US 20160281738A1
• Time in Patent Office: 1,303 Days
• CPC Class Codes: B29C 70/24 oriented in at least three directions forming a three dimensional structure
• CPC Class Codes: F01D 21/045 special arrangements in stators or in rotors dealing with breaking-off of part of rotor
• CPC Class Codes: F04D 29/526 Details of the casing section radially opposing blade tips ducts F04D29/545
• CPC Class Codes: F05D 2220/32 in gas turbines
• CPC Class Codes: F05D 2300/224 Carbon, e.g. graphite
• CPC Class Codes: F05D 2300/6012 Woven fabrics
• CPC Class Codes: F05D 2300/6031 Functionally graded composites
• CPC Class Codes: F05D 2300/6034 Orientation of fibres, weaving, ply angle
• CPC Class Codes: F05D 2300/614 Fibres or filaments
• CPC Class Codes: Y02T 50/60 Efficient propulsion technologies, e.g. for aircraft

Abstract

A fan containment case for a gas turbine engine includes a first inner layer and a second layer outside the first inner layer, where the second layer is made of a first material having a first fabric architecture. The fan containment case also includes a third layer outside of the second layer, where the third layer is made of a second material having a second fabric architecture, and at least one of the first material and the first fabric architecture of the second layer is different from the second material and the second architecture, respectively, of the third layer. A fourth outer layer is located outside of the third layer.

Claims

1. A fan containment case for a gas turbine engine comprising:

a first inner layer comprising an aramid fiber layer;

a second layer outside the first inner layer, wherein the second layer comprises a first material having a first fabric architecture;

a third layer outside of the second layer, wherein the third layer comprises a second material having a second fabric architecture, wherein at least one of the first material and the first fabric architecture of the second layer is different from the second material and the second fabric architecture, respectively, of the third layer; and

a fourth outer layer outside of the third layer, wherein the fourth outer layer comprises a third fabric architecture that is different from the first and second fabric architectures;

wherein the first architecture of the second layer comprises a triaxial braid utilizing a first set of weave angles, and the second architecture of the third layer comprises a triaxial braid utilizing a second set of weave angles that is different than the first set of weave angles.

2. The fan containment case as recited in claim 1, wherein the first inner layer comprises a fabric architecture of a three dimensional weave.

3. The fan containment case as recited in claim 1, wherein the first material of the second layer comprises a hybrid carbon-fiberglass.

4. The fan containment case as recited in claim 1, wherein the triaxial braid of the second layer includes first fibers, second fibers and third fibers, and the second fibers and third fibers extend at weave angles of about +/−

60°

relative to the first fibers.

5. The fan containment case as recited in claim 4, wherein the first fibers are carbon fibers, and the second fibers and the third fibers are fiberglass fibers.

6. The fan containment case as recited in claim 1, wherein the second material of the third layer is carbon.

7. The fan containment case as recited in claim 1, wherein the triaxial braid of the third layer includes first fibers, second fibers and third fibers, and the second fibers and third fibers extend at weave angles of about +/−

45°

relative to the first fibers.

8. The fan containment case as recited in claim 7, wherein the first fibers, the second fibers and the third fibers are carbon fibers.

9. The fan containment case as recited in claim 1, wherein the fourth outer layer comprises a fabric architecture of a non-crimp fabric.

10. The fan containment case as recited in claim 1, wherein a magnitude of non-zero weave angles of the second weave angle set is less than a magnitude of non-zero weave angles of the first weave angle set.

11. A fan containment case for a gas turbine engine comprising:

a first inner layer comprising an aramid fiber;

a second layer outside the first inner layer, wherein the second layer comprises a hybrid carbon-fiberglass having a first fabric architecture;

a third layer outside of the second layer, wherein the third layer comprises carbon and has a second fabric architecture, and the first fabric architecture is different from the second fabric architecture; and

a fourth outer layer outside of the third layer, wherein the fourth outer layer comprises a third fabric architecture that is different from the first and second fabric architectures;

wherein the first architecture of the second layer comprises a triaxial braid utilizing a first set of weave angles, and the second architecture of the third layer comprises a triaxial braid utilizing a second set of weave angles that is different than the first set of weave angles.

12. The fan containment case as recited in claim 11, wherein the triaxial braid of the second layer includes first fibers, second fibers and third fibers, and the second fibers and third fibers extend at weave angles of about +/−

60°

relative to the first fibers.

13. The fan containment case as recited in claim 12, wherein the first fibers are carbon fibers, and the second fibers and the third fibers are fiberglass fibers.

14. The fan containment case as recited in claim 11, wherein the triaxial braid of the third layer includes first fibers, second fibers and third fibers, and the second fibers and third fibers extend at weave angles of about +/−

45°

relative to the first fibers.

15. The fan containment case as recited in claim 14, wherein the first fibers, the second fibers and the third fibers are carbon fibers.

16. The fan containment case as recited in claim 11, wherein the first inner layer comprises a fabric architecture of a three dimensional weave.

17. The fan containment case as recited in claim 11, wherein the fourth outer layer comprises a fabric architecture of a non-crimp fabric.

18. The fan containment case as recited in claim 11, wherein a magnitude of non-zero weave angles of the second fabric architecture is less than a magnitude of non-zero weave angles of the first fabric architecture.

19. A fan containment case for a gas turbine engine comprising:

a first inner layer comprising an aramid fiber and having a triaxial braid, two-dimensional weave, or three-dimensional weave fabric architecture;

a second layer outside the first inner layer, wherein the second layer comprises a triaxial braid that includes first, second, and third fibers, the second and third fibers utilizing weave angles of about +/−

x relative to the first fibers;

a third layer outside of the second layer, wherein the third layer comprises a triaxial braid that includes first, second, and third fibers, the second and third fibers utilizing weave angles of about +/−

y relative to the first fibers, wherein y<

x; and

a fourth outer layer outside of the third layer and comprising a non-crimp fabric or a triaxial braid.