Composite fan containment case

Patent metadata

Field	Value
Publication number	US-11499448-B2
Application number	US-201916424843-A
Country	US
Kind code	B2
Filing date	May 29, 2019
Priority date	May 29, 2019
Publication date	Nov 15, 2022
Grant date	Nov 15, 2022

Abstract

A composite fan casing for a gas turbine engine defining a central axis is generally provided. The composite fan casing includes a core having a plurality of core layers of reinforcing fibers bonded together with a thermosetting polymeric resin and having an outer surface. The composite fan casing further includes at least one stiffener integrally coupled to an aft portion of the outer surface of the core relative to the central axis. Additionally, the at least one stiffener comprises an elastic material.

First claim

What is claimed is:

1. A composite fan casing for a gas turbine engine comprising a plurality of fan blades, the gas turbine engine defining a central axis, the composite fan casing comprising:
a core having a plurality of core layers of reinforcing fibers bonded together with a thermosetting polymeric resin and having an outer surface; and
at least one stiffener that comprises an external structure that defines an internal cavity, wherein the external structure extends from a first axial location to a second axial location, the first axial location and the second axial location being aft of the plurality of fan blades of the gas turbine engine,
wherein the external structure is integrally coupled to an aft portion of the outer surface of the core relative to the central axis at the first axial location and at the second axial location, wherein the aft portion of the outer surface of the core is aft of the plurality of fan blades of the gas turbine engine, wherein the internal cavity of the at least one stiffener comprises an elastic material, wherein the elastic material comprises a first layer of a shape memory alloy and a second layer of an elastomer or a rubber.

2. The composite fan casing of claim 1 , wherein the elastic material comprises the shape memory alloy.

3. The composite fan casing of claim 2 , wherein the shape memory alloy comprises at least one of nickel-titanium, a nickel-titanium based alloy, a copper-aluminum-nickel alloy, or an alloy containing zinc, copper, gold, or iron.

4. The composite fan casing of claim 1 , wherein the elastic material comprises the elastomer or the rubber.

5. The composite fan casing of claim 1 , wherein the elastic material comprises the shape memory alloy and the elastomer or the rubber.

6. The composite fan casing of claim 5 , wherein the stiffener comprises one or more layers of the shape memory alloy arranged to alternate with one or more layers of the elastomer or the rubber.

7. The composite fan casing of claim 1 , wherein the stiffener comprises an external hat-shaped structure that defines the internal cavity, the external hat-shaped structure comprising the first layer of the shape memory alloy and the second layer of the elastomer or the rubber, wherein the internal cavity comprises a third layer of the shape memory alloy, the elastomer, or the rubber.

8. The composite fan casing of claim 7 , wherein the third layer comprises the shape memory alloy and the internal cavity further comprises a fourth layer of the elastomer or the rubber, wherein the first layer is adjacent to the second layer and the third layer is adjacent to the fourth layer.

9. The composite fan casing of claim 1 , wherein the thermosetting polymeric resin comprises at least one of a vinyl ester resin, a polyester resin, an acrylic resin, an epoxy resin, or a polyurethane resin.

10. The composite fan casing of claim 1 , wherein the reinforcing fibers comprise at least one of carbon fibers, graphite fibers, glass fibers, ceramic fibers, or aromatic polyamide fibers.

11. A composite fan casing for a gas turbine engine defining a central axis, the composite fan casing comprising:
a core having a plurality of core layers of reinforcing fibers bonded together with a thermosetting polymeric resin and having an outer surface; and
at least one stiffener integrally coupled to an aft portion of the outer surface of the core relative to the central axis, wherein the at least one stiffener comprises an elastic material, wherein the elastic material comprises a shape memory alloy,
wherein the stiffener comprises an external hat-shaped structure, wherein a mesh of the elastic material is housed within the external hat-shaped structure.

12. The composite fan casing of claim 11 , wherein the shape memory alloy comprises at least one of nickel-titanium, a nickel-titanium based alloy, a copper-aluminum-nickel alloy, or an alloy containing zinc, copper, gold, or iron, wherein the thermosetting polymeric resin comprises at least one of a vinyl ester resin, a polyester resin, an acrylic resin, an epoxy resin, or a polyurethane resin.

13. The composite fan casing of claim 11 , wherein the reinforcing fibers comprise at least one of carbon fibers, graphite fibers, glass fibers, ceramic fibers, or aromatic polyamide fibers.

14. A composite fan casing for a gas turbine engine defining a central axis, the composite fan casing comprising:
a core having a plurality of core layers of reinforcing fibers bonded together with a thermosetting polymeric resin and having an outer surface; and
at least one stiffener integrally coupled to an aft portion of the outer surface of the core relative to the central axis, wherein the at least one stiffener comprises an elastic material, wherein the elastic material comprises a shape memory alloy, an elastomer, or a rubber,
wherein the elastic material comprises the shape memory alloy and the elastomer or the rubber,
wherein the stiffener comprises one or more layers of the shape memory alloy and one or more layers of the elastomer or the rubber, which define a lattice structure.

15. The composite fan casing of claim 14 , wherein the shape memory alloy comprises at least one of nickel-titanium, a nickel-titanium based alloy, a copper-aluminum-nickel alloy, or an alloy containing zinc, copper, gold, or iron, wherein the thermosetting polymeric resin comprises at least one of a vinyl ester resin, a polyester resin, an acrylic resin, an epoxy resin, or a polyurethane resin.

16. The composite fan casing of claim 14 , wherein the reinforcing fibers comprise at least one of carbon fibers, graphite fibers, glass fibers, ceramic fibers, or aromatic polyamide fibers.

17. A composite fan casing for a gas turbine engine defining a central axis, the composite fan casing comprising:
a core having a plurality of core layers of reinforcing fibers bonded together with a thermosetting polymeric resin and having an outer surface; and
at least one stiffener integrally coupled to an aft portion of the outer surface of the core relative to the central axis, wherein the at least one stiffener comprises an elastic material, wherein the elastic material comprises a shape memory alloy, an elastomer, or a rubber,
wherein the stiffener comprises an external hat-shaped structure that defines an internal cavity, the external hat-shaped structure comprising a first layer of the shape memory alloy and a second layer of the elastomer or the rubber,
wherein the internal cavity comprises a third layer of the shape memory alloy, the elastomer, or the rubber.

18. The composite fan casing of claim 17 , wherein the shape memory alloy comprises at least one of nickel-titanium, a nickel-titanium based alloy, a copper-aluminum-nickel alloy, or an alloy containing zinc, copper, gold, or iron.

19. The composite fan casing of claim 17 , wherein the thermosetting polymeric resin comprises at least one of a vinyl ester resin, a polyester resin, an acrylic resin, an epoxy resin, or a polyurethane resin.

20. The composite fan casing of claim 17 , wherein the reinforcing fibers comprise at least one of carbon fibers, graphite fibers, glass fibers, ceramic fibers, or aromatic polyamide fibers.

Assignees

• Gen Electric

Inventors

• Yadav Abhijeet Jayshingrao
• Prabhakar Nagamohan Govinahalli
• Kray Nicholas Joseph
• Mittal Shivam
• Sharma Praveen
• Mahadeo Bhujabal Prashant
• Ganiger Ravindra Shankar

Classifications

• F05D2300/1723

  Nickel-Copper alloy, e.g. Monel · CPC title

• F01D25/24 Primary

  Casings (modified for heating or cooling F01D25/14); Casing parts, e.g. diaphragms, casing fastenings (casings for rotary machines or engines in general F16M {; special arrangements in stators dealing with breaking-off of part of rotor F01D21/045}) · CPC title

• F01D25/005

  Selecting particular materials · CPC title

• F04D29/023

  especially adapted for elastic fluid pumps · CPC title

• F05D2300/501

  Elasticity · CPC title