Conformal and flexible woven heat shields for gas turbine engine components

Patent metadata

Field	Value
Publication number	US-11635210-B2
Application number	US-202017125028-A
Country	US
Kind code	B2
Filing date	Dec 17, 2020
Priority date	Dec 17, 2020
Publication date	Apr 25, 2023
Grant date	Apr 25, 2023

Abstract

A heat shielded assembly includes a fuel structure of a combustor of a gas turbine engine and a woven heat shield at least partially conformally surrounding the fuel structure and spaced from an exterior of the fuel structure by a distance where it surrounds the fuel structure. The fuel structure is configured to deliver fuel to the combustor. The woven heat shield comprises a first set of strands, a second set of strands interwoven with the first set of strands, and a weave pattern comprising the first set of strands and the second set of strands. Each strand of the first set of strands extends in a first direction, each strand of the second set of strands extends in a second direction transverse to the first direction, and the first set of strands and the second set of strands are not attached where they intersect in the weave pattern.

First claim

The invention claimed is:

1. A heat shielded assembly comprising:
a fuel structure of a combustor of a gas turbine engine, wherein the fuel structure is configured to deliver fuel to the combustor; and
a woven heat shield at least partially conformally surrounding the fuel structure and spaced from an exterior of the fuel structure by a distance where the woven heat shield conformally surrounds the fuel structure, the woven heat shield comprising:
a first set of strands, wherein each strand of the first set of strands extends in a first direction;
a second set of strands interwoven with the first set of strands, wherein each strand of the second set of strands extends in a second direction transverse to the first direction;
a weave pattern comprising the first set of strands and the second set of strands, wherein the first set of strands and the second set of strands are not attached where they intersect in the weave pattern, such that the first set of strands are able to move relative to the second set of strands when undergoing thermal expansion;
wherein:
each strand of the first set of strands and the second set of strands does not contact any other strand of the first set of strands and the second set of strands at an ambient temperature;
the woven heat shield defines an air gap that extends between an inner surface of the woven heat shield and an outer surface of the fuel structure; and
the woven heat shield is configured to trap an insulating layer of stagnant air against the outer surface of the fuel structure.

2. The heat shielded assembly of claim 1 , wherein the fuel structure is centered on an axis, and each strand of at least one of the first set of strands or the second set of strands extends helically about the axis.

3. The heat shielded assembly of claim 2 , wherein the first set of strands and the second set of strands are able to compress when undergoing thermal expansion.

4. The heat shielded assembly of claim 1 , wherein the fuel structure, the first set of strands, and the second set of strands are additively manufactured.

5. The heat shielded assembly of claim 1 , wherein the woven heat shield is attached to a grommet that surrounds a portion of the fuel structure.

6. The heat shielded assembly of claim 1 , wherein the fuel structure is a fuel injector or a fuel manifold.

7. The heat shielded assembly of claim 1 , wherein the fuel structure extends non-linearly along an axis and adopts a curved or zig-zag shape.

8. The heat shielded assembly of claim 1 , wherein the first set of strands and second set of strands are not attached at an operating temperature of the gas turbine engine.

9. The heat shielded assembly of claim 1 , further comprising gaps formed in the weave pattern and disposed between the first set of strands and the second set of strands, wherein the gaps separate the first set of strands and the second set of strands and are permeable to fluids.

10. The heat shielded assembly of claim 1 , wherein at least one of the first set of strands, the second set of strands, or the first set of strands and the second set of strands comprises a metal material.

11. A method of forming a heat shield for a rigid component of a combustor section of a gas turbine engine comprising
the rigid component is a fuel structure of a combustor of the combustor section of the gas turbine engine, wherein the fuel structure is configured to deliver fuel to the combustor; and
the method further comprising:
additively manufacturing the fuel structure; and
additively manufacturing a woven heat shield around the fuel structure, wherein the woven heat shield at least partially conformally surrounds the fuel structure and is spaced from an exterior of the fuel structure by a distance where the woven heat shield conformally surrounds the fuel structure, the woven heat shield comprising:
a first set of strands, wherein each strand of the first set of strands extends in a first direction;
a second set of strands interwoven with the first set of strands, wherein each strand of the second set of strands extends in a second direction transverse to the first direction; and
a weave pattern comprising the first set of strands and the second set of strands, wherein the first set of strands and the second set of strands are not attached where they intersect in the weave pattern, such that the first set of strands are able to move relative to the second set of strands when undergoing thermal expansion;
wherein:
each strand of the first set of strands and the second set of strands does not contact any other strand of the first set of strands and the second set of strands at an ambient temperature;
the woven heat shield defines an air gap that extends between an inner surface of the woven heat shield and an outer surface of the fuel structure; and
the woven heat shield is configured to trap an insulating layer of stagnant air against the outer surface of the fuel structure.

12. The method of claim 11 , wherein the woven heat shield includes gaps formed between the first set of strands and the second set of strands, and the gaps are permeable to air.

13. The method of claim 11 , wherein the woven heat shield is additively manufactured at the same time as the fuel structure.

14. The method of claim 11 , wherein the fuel structure is additively manufactured before the woven heat shield is additively manufactured.

15. A method of forming a heat shield for a rigid component of a combustor section of a gas turbine engine comprising
the rigid component is a fuel structure of a combustor of the combustor section of the gas turbine engine, wherein the fuel structure is configured to deliver fuel to the combustor; and
the method further comprising:
additively manufacturing a woven heat shield, wherein the woven heat shield is at least partially annular and the annular portion has a larger diameter than a dimension of the fuel structure; the woven heat shield comprising:
a first set of strands, wherein each strand of the first set of strands extends in a first direction;
a second set of strands interwoven with the first set of strands, wherein each strand of the second set of strands extends in a second direction transverse to the first direction; and
a weave pattern comprising the first set of strands and the second set of strands;

placing the fuel structure within the annular portion of the woven heat shield;

and
mechanically tightening the weave pattern of the woven heat shield after placing the fuel structure within the annular portion to create a conformal fit of the woven heat shield about the fuel structure, wherein the woven heat shield at least partially conformally surrounds the fuel structure and is spaced from an exterior of the fuel structure by a distance where the woven heat shield conformally surrounds the fuel structure, wherein the first set of strands and the second set of strands are not attached where they intersect in the weave pattern, such that the first set of strands are able to move relative to the second set of strands when undergoing thermal expansion;
wherein:
each strand of the first set of strands and the second set of strands does not contact any other strand of the first set of strands and the second set of strands at an ambient temperature;
the woven heat shield defines an air gap that extends between an inner surface of the woven heat shield and an outer surface of the fuel structure; and
the woven heat shield weave pattern is configured to trap an insulating layer of stagnant air against the outer surface of the fuel structure.

16. The

Assignees

• Delavan Inc
• Collins Engine Nozzles Inc

Inventors

• Ryon Jason
• Zink Gregory
• Prociw Lev Alexander

Classifications

• F02C7/222

  Fuel flow conduits, e.g. manifolds · CPC title

• F05D2260/231

  Preventing heat transfer · CPC title

• F23R3/283 Primary

  Attaching or cooling of fuel injecting means including supports for fuel injectors, stems, or lances · CPC title

• F02C7/24

  Heat or noise insulation (air intakes having provisions for noise suppression F02C7/045; turbine exhaust heads, chambers, or the like F01D25/30; silencing nozzles of jet-propulsion plants F02K1/00) · CPC title

• F23R2900/00005

  Preventing fatigue failures or reducing mechanical stress in gas turbine components · CPC title