Engine exhaust skin connection system

Patent metadata

Field	Value
Publication number	US-11300075-B2
Application number	US-201916299961-A
Country	US
Kind code	B2
Filing date	Mar 12, 2019
Priority date	Mar 12, 2019
Publication date	Apr 12, 2022
Grant date	Apr 12, 2022

Abstract

A mechanical connection system is provided that includes a ceramic skin panel, at least one bushing, and at least one bolt. The ceramic skin panel includes a first surface, a second surface, and at least one aperture extending between the first surface and the second surface. The aperture has an axial centerline, a chamfered portion contiguous with the first surface, and an axial portion contiguous with the second surface. The chamfered portion includes a tapered surface disposed at a first angle such that a line extending along the tapered surface intersects the axial centerline at a plane of the second surface. The bushing has a housing and a collar. The housing is configured to mate with the chamfered portion of the aperture disposed within the ceramic skin panel. The collar is configured for engagement with the housing.

First claim

What is claimed is:

1. A mechanical connection system, comprising:
a ceramic skin panel having a first surface, a second surface, and at least one aperture extending between the first surface and the second surface, the aperture having an axial centerline, a chamfered portion contiguous with the first surface, and an axial portion contiguous with the second surface, wherein the chamfered portion includes a tapered surface disposed at a first angle such that a line extending along the tapered surface intersects the axial centerline at a plane of the second surface;
at least one bushing having a housing and a collar, the housing having a head configured to mate with the chamfered portion of the at least one aperture disposed within the ceramic skin panel, and a body configured to extend within the at least one aperture, and the collar is configured for engagement with the housing from the second surface of the ceramic skin panel; and
at least one bolt configured for engagement with the bushing and a support structure.

2. The connection system of claim 1 , further comprising a nut plate affixed to the support structure, wherein the bolt is configured for engagement with the support structure via the nut plate.

3. The system of claim 1 , wherein the ceramic skin panel is a ceramic matrix composite.

4. The system of claim 1 , wherein the ceramic skin panel has a first coefficient of thermal expansion (CTE) value, and the support structure has a second CTE value, and the first CTE value is less than the second CTE value.

5. The system of claim 4 , wherein the support structure comprises a metallic material.

6. The system of claim 4 , wherein the support structure comprises a nickel alloy.

7. The system of claim 1 , wherein the collar includes a head, a body, and a center bore extending through the body; and
wherein the ceramic skin panel is arcuately shaped to form a part of an annular structure; and
wherein the system further comprises a washer having a first contact surface and a second contact surface, the second contact surface is opposite the first contact surface, wherein the first contact surface is configured to mate with the head of the collar and the second contact surface is configured to mate with the arcuate shape of the ceramic skin panel; and
wherein the washer is disposed between the collar and the ceramic skin panel.

8. The system of claim 1 , wherein the housing, the collar, and the washer are configured to permit sufficient compressive attachment of the bushing to the ceramic skin panel in an amount that prevents rotation of the bushing relative to the ceramic skin panel without deformation of the ceramic skin panel in an amount that produces detrimental mechanical properties within the ceramic skin panel.

9. A gas turbine engine nacelle, comprising:
an annular support structure;
a plurality of ceramic skin panels attached to the annular support structure, the plurality of ceramic skin panels collectively forming at least a portion of a first annular duct;
wherein each ceramic skin panel has a first surface, a second surface, and a plurality of apertures extending between the first surface and the second surface, the apertures each having an axial centerline, a chamfered portion contiguous with the first surface, and an axial portion contiguous with the second surface, wherein the chamfered portion includes a tapered surface disposed at a first angle such that a line extending along the tapered surface intersects the axial centerline at a plane of the second surface; and
a plurality of connection systems, each connecting a respective one of the ceramic skin panels to the support structure, the connection system including a bushing for connecting the ceramic skin panel to the annular support structure, each bushing having a housing and a collar, the housing having a head configured to mate with the chamfered portion of one of the apertures disposed within the ceramic skin panel, and a body configured to extend within the aperture, and the collar is configured for engagement with the housing from the second surface of the ceramic skin panel, and a bolt configured for engagement with the bushing and the support structure.

10. The nacelle of claim 9 , wherein each connection system further comprises a nut plate affixed to the support structure, wherein the bolt is configured for engagement with the support structure via the nut plate.

11. The nacelle of claim 9 , wherein the ceramic skin panels are each a ceramic matrix composite.

12. The nacelle of claim 9 , wherein the ceramic skin panels each have a first coefficient of thermal expansion (CTE) value, and the support structure has a second CTE value, and the first CTE value is less than the second CTE value.

13. The nacelle of claim 12 , wherein the support structure comprises a metallic material.

14. The nacelle of claim 12 , wherein the support structure comprises a nickel alloy.

15. The nacelle of claim 9 , wherein the collar of each connection system includes a head, a body, and a center bore extending through the body; and
wherein the ceramic skin panels are each arcuately shaped; and
wherein each connection system further comprises a washer having a first contact surface and a second contact surface, the second contact surface is opposite the first contact surface, wherein the first contact surface is configured to mate with the head of the collar and the second contact surface is configured to mate with the arcuate shape of the ceramic skin panel; and
wherein the washer is disposed between the collar and the ceramic skin panel.

16. The nacelle of claim 15 , wherein the housing, the collar, and the washer of each connection system are configured to permit sufficient compressive attachment of the bushing to the ceramic skin panel in an amount that prevents rotation of the bushing relative to the ceramic skin panel without deformation of the ceramic skin panel in an amount that produces detrimental mechanical properties within the ceramic skin panel.

17. The nacelle of claim 9 , wherein the plurality of ceramic skin panels attached to the annular support structure, include a plurality of inner skin panels that collectively form the at least a portion of the first annular duct, and a plurality of outer skin panels that collectively form at least a portion of a second annular duct disposed radially outside of the first annular duct.

18. The nacelle of claim 17 , wherein a first number of the plurality of connection systems connect the inner skin panels to the support structure and a second number of the plurality of connection systems connect the outer skin panels to the support structure.

19. The nacelle of claim 17 , further comprising a seal disposed between an aft portion of at least one of the inner skin panels and an aft portion of a respective one of the outer skin panels, the seal attached to the aft portion of the at least one of the inner skin panels, or the aft portion of the respective one of the outer skin panels, or both.

20. The nacelle of claim 19 , wherein the seal extends circumferentially between the aft portions of all of the plurality of inner skin panels and the aft portion of all of the plurality of the outer skin panels.

Assignees

• Rohr Inc

Inventors

• Alloway Richard S
• Pujar Vijay V
• Lu Jinqiu
• Saunders Adam
• Bowman Gary E

Classifications

• Y02T50/60

  Efficient propulsion technologies, e.g. for aircraft · CPC title

• F05D2260/31

  Retaining bolts or nuts · CPC title

• F05D2300/6033

  Ceramic matrix composites [CMC] · CPC title

• F01D25/28

  Supporting or mounting arrangements, e.g. for turbine casing · CPC title

• F02C7/32 Primary

  Arrangement, mounting, or driving, of auxiliaries · CPC title