High temperature composite seal

Patent metadata

Field	Value
Publication number	US-11065825-B2
Application number	US-201816210528-A
Country	US
Kind code	B2
Filing date	Dec 5, 2018
Priority date	Dec 5, 2018
Publication date	Jul 20, 2021
Grant date	Jul 20, 2021

Abstract

A method of sealing a first component to a second component comprising the steps of locating at least one fiber reinforced polyimide resin layer against a first sealing surface on a first component and against a second sealing surface on a second component. At least one fiber reinforced polyimide resin layer is compressed against the first sealing surface and the second sealing surface prior to curing at least one fiber reinforced polyimide resin layer. At least one fiber reinforced polyimide resin layer is heated to promote flow and conformation to the first sealing surface and the second sealing surface. At least one fiber reinforced polyimide resin layer is cured to provide a fluid tight seal between the first component and the second component.

First claim

What is claimed is:

1. A method of sealing a first component to a second component comprising the steps of:
locating at least one fiber reinforced polyimide resin layer against a first sealing surface on a first component and against a second sealing surface on a second component;
compressing the at least one fiber reinforced polyimide resin layer against the first sealing surface and the second sealing surface prior to curing the at least one fiber reinforced polyimide resin layer;
heating the at least one fiber reinforced polyimide resin layer to promote flow and conformation to the first sealing surface and the second sealing surface; and
curing the at least one fiber reinforced polyimide resin layer to provide a fluid tight seal between the first component and the second component.

2. The method of claim 1 , further comprising compressing the first component towards the second component to a predetermined force after the at least one fiber reinforced polyimide resin layer has cured.

3. The method of claim 2 , wherein heating the at least one fiber reinforced polyimide resin layer includes heating to between 600 degrees Fahrenheit and less than 750 degrees Fahrenheit.

4. The method of claim 1 , wherein the at least one fiber reinforced polyimide resin layer includes fibers forming at least one of a fabric or a braid.

5. The method of claim 4 , wherein the first component and the second component contribute to communicating at least one of bleed air, fuel, or lubricant in a gas turbine engine.

6. The method of claim 4 , further comprising disassembling the first component from the second component during service by separating the first component from the second component after the at least one fiber reinforced polyimide resin layer has cured and bonded to the first component and the second component while maintaining the first component and the second component in reusable condition.

7. The method of claim 6 , further comprising:
locating at least one second fiber reinforced polyimide resin layer against the first sealing surface of the first component and against the second sealing surface of the second component;
compressing at least one second fiber reinforced polyimide resin layer against the first sealing surface and the second sealing surface prior to curing the at least one second fiber reinforced polyimide resin layer;
heating the at least one second fiber reinforced polyimide resin layer to conform to the first sealing surface and the second sealing surface; and
curing the at least one fiber reinforced polyimide resin layer to provide a fluid tight seal between the first component and the second component.

8. The method of claim 1 , further comprising coating at least one of the first sealing surface and the second sealing with an adhesion reducing material at least one of a frangible oxide, a frangible primer, a non-adherent film, or a non-adherent coating.

9. The method of claim 8 , wherein the first sealing surface is located on an outer diameter of the first component with the first component being a first fluid tube and the second sealing surface is located on an inner diameter of the second component with the second component being a second fluid tube and the first and second sealing surfaces are in an axially overlapping relationship relative to a common longitudinal axis of first and second component.

10. The method of claim 1 , wherein an outer diameter of the first component is less than an inner diameter defined by the second sealing surface of the second component and the first and second components are each a fluid tube.

11. The method of claim 1 , wherein the first sealing surface is located on a first component flange with the first component being a first fluid tube and the second sealing surface is located on a second component flange with the second component being a second fluid tube and the first and second sealing surfaces are axially spaced from each other relative to a common longitudinal axis of first and second components, a clamp compressing the first component flange towards the second component flange, and the seal forms an annular ring.

12. The method of claim 1 , further comprising isolating the first component from the second component with the at least one fiber reinforced polyimide resin layer to prevent material reactions between the first component and the second component.

13. The method of claim 1 , further comprising bonding the at least one fiber reinforced polyimide to the first component and the second component, wherein at least one of the first sealing surface and the second sealing surface includes at least one of a surface irregularity and the at least one fiber reinforced polyimide resin layer conforms to the irregularity.

14. A gas turbine engine assembly comprising:
a first component including a first sealing surface;
a second component including a second sealing surface and the second component is in fluid communication with the first component; and
a seal engaging the first sealing surface and the second sealing surface forming a fluid tight connection between the first component and the second component, wherein the seal includes at least one fiber reinforced polyimide resin layer in a cured state that follows a profile of the first sealing surface and a profile of the second sealing surface, wherein the first surface and the second surface are each bonded to the seal to create a fluid tight seal and at least one of the first sealing surface and the second sealing surface includes at least one of a surface irregularity and the seal at least partially conforms to the surface irregularities.

15. The assembly of claim 14 , wherein at least one of the first sealing surface and the second sealing surface are coated with at least one of the following adhesion reducing materials: a frangible oxide, a frangible primer, a non-adherent film, or a non-adherent coating.

16. The assembly of claim 14 , wherein the at least one fiber reinforced polyimide resin layer prevents material reactions between the first component and the second component.

17. The assembly of claim 14 , wherein the first sealing surface is located on a first component flange with the first component being a first fluid tube and the second sealing surface is located on a second component flange with the second component being a second fluid tube, the first and second sealing surfaces are axially spaced from each other relative to a common longitudinal axis of first and second component, a clamp for compressing the first component flange towards the second component flange, and the seal forms an annular ring.

18. The assembly of claim 14 , wherein the first sealing surface is located on an outer diameter of the first component with the first component being a first fluid tube and the second sealing surface is located on an inner diameter of the second component with the second component being a second fluid tube and the first and second sealing surfaces are in an axially overlapping relationship relative to a common longitudinal axis of first and second component.

19. The assembly of claim 14 , wherein the first sealing surface is located on an outer diameter of the first component with the first component being a first fluid tube and the second sealing surface is located on an outer diameter of the second component with the second component being a second fluid tube and a first sleeve half and a second sleeve half surround distal ends of the first and second components.

20. The assembly of claim 14 ,

Assignees

• United Technologies Corp
• Raytheon Tech Corp

Inventors

• Davis Kerry Lynn
• Bogue William

Classifications

• F16J15/3284 Primary

  characterised by their structure; Selection of materials · CPC title

• F05D2300/434

  Polyimides, e.g. AURUM · CPC title

• B29C66/522

  Joining tubular articles (B29C66/53241 takes precedence) · CPC title

• F16J15/14

  by means of granular or plastic material, or fluid · CPC title

• F05D2240/55

  Seals · CPC title