ATTACHMENT APPARATUS FOR CERAMIC MATRIX COMPOSITE MATERIALS

• US 20140314547A1
• Filed: 08/31/2012
• Published: 10/23/2014
• Est. Priority Date: 08/31/2012
• Status: Abandoned Application

• Current Assignee: United Technologies Corporation (Rtx Corporation)
• Original Assignee: United Technologies Corporation (Rtx Corporation)
• Inventors: Sander, David J., Duelm, Shelton O.
• Application Number:
  US13/600,781
• Publication Number:
  US 20140314547A1
• Time in Patent Office: Days
• US Class Current: 415/135
• CPC Class Codes: F01D 25/162 Bearing supports
• CPC Class Codes: F02C 7/20 Mounting or supporting of plant; Accommodating heat expansion or creep
• CPC Class Codes: F05D 2300/6033 Ceramic matrix composites [CMC]
• CPC Class Codes: Y02T 50/60 Efficient propulsion technologies, e.g. for aircraft
• CPC Class Codes: Y10T 29/49947 by applying separate fastener
• CPC Class Codes: Y10T 29/49948 Multipart cooperating fastener [e.g., bolt and nut]

Abstract

A first ceramic matrix composite structure having a first flange with a first aperture, and a second structure having a second flange with a second aperture are clamped together by a fastener and spring assembly. The second flange is in contact with the first flange and the apertures of the first and second flanges align with each other. A threaded fastener having a thermal expansion rate that is different than the thermal expansion rate of at least one of the first ceramic matrix composite structure and second structure extends through the aligned apertures. The fastener includes a bolt, a nut, and a spring assembly that maintains a constant clamping pressure irrespective of the thermal expansion differences between the bolt and the first ceramic matrix composite structure and second structure.

Claims

1. An apparatus comprising:

a first ceramic matrix composite structure, having a first flange with a first aperture;

a second structure, having a second flange with a second aperture, the second flange being in contact with the first flange with the second aperture aligned with the first aperture; and

a fastener having a portion extending through the first aperture of the first flange and the second aperture of the second flange, the fastener having a thermal expansion rate different than a thermal expansion rate of at least one of the first ceramic matrix composite structure and the second structure;

the fastener including a spring assembly that maintains a clamping pressure irrespective of thermal expansion differences between the fastener and at least one of the first ceramic matrix composite structure and the second structure.

2. The apparatus of claim 1, wherein the fastener further includes a bolt and a nut.

3. The apparatus of claim 2, wherein the bolt comprises a bolt head at a first end of the bolt and a threaded shank at a second end opposite the bolt head.

4. The apparatus of claim 2, wherein the nut comprises a nut body and a flange at one end of the nut body with the flange extending outward from an outer surface of the nut.

5. The apparatus of claim 1, wherein the spring assembly is located on the bolt between at least one of the bolt head and the nut and the first flange of the first ceramic matrix composite structure and the second flange of the second structure.

6. The apparatus of claim 1, wherein the spring assembly comprises at least one Belleville washer.

7. The apparatus of claim 6, wherein the spring assembly comprises a plurality of Belleville washers.

8. The apparatus of claim 7, wherein at least one of the plurality of Belleville washers faces concave away from and adjacent to the bolt head.

9. The apparatus of claim 7, wherein the plurality of Belleville washers include Belleville washers facing in opposite directions.

10. The apparatus of claim 1, wherein the second structure comprises a ceramic matrix composite material.

11. A mid-turbine frame located in a gas turbine engine, the mid-turbine frame comprising:

a first ceramic matrix composite component of the mid-turbine frame, the first component having a first flange with a first aperture;

a second component of the mid-turbine frame, the second component having a second flange with a second aperture, the second flange being in contact with the first flange with the second aperture aligned with the first aperture;

a bolt extending through the first aperture and the second aperture, the bolt having a thermal expansion rate different than a thermal expansion rate of at least one of the first ceramic matrix composite component of the mid-turbine frame and the second component of the mid-turbine frame, the bolt having a head and a bolt shank having a threaded portion;

a nut threadingly engaged onto the threaded portion of the bolt shank; and

a spring assembly disposed on the bolt shank between at least one of the bolt head and the nut and the first flange and the second flange that maintains a clamping pressure irrespective of thermal expansion differences between the fastener and at least one of the first ceramic matrix composite component of the mid-turbine frame and the second component of the mid-turbine frame.

12. The mid-turbine frame of claim 11, wherein the spring assembly comprises at least one Belleville washer.

13. The mid-turbine frame of claim 12, wherein the spring assembly comprises a plurality of Belleville washers.

14. The mid-turbine frame of claim 13, wherein at least one of the plurality of Belleville washers faces concave away from and adjacent to the bolt head.

15. The mid-turbine frame of claim 14, wherein the plurality of Belleville washers include Belleville washers facing in opposite directions.

16. The mid-turbine frame of claim 11, wherein the second component comprises a ceramic matrix composite material.

17. A method of assembling a mid-turbine frame for use in a gas turbine engine, the method comprising:

positioning a first flange of a first ceramic matrix composite component of the mid-turbine frame abutting a second flange of a second component of the mid-turbine frame;

attaching the first flange of the first ceramic matrix composite component of the mid-turbine frame to the second flange of the second component of the mid-turbine frame via a fastener having a spring assembly thereon; and

tightening the fastener to cause the spring assembly to apply a force that clamps the first and second flanges together.

18. The method of claim 17, wherein the fastener further includes a bolt and a nut.

19. The method of claim 18, wherein the bolt comprises a bolt head at a first end of the bolt and a threaded shank at a second end opposite the bolt head.

20. The method of claim 19, further comprising compressing the first flange of the first ceramic matrix composite component of the mid-turbine frame against the second flange of the second component of the mid-turbine frame by threadingly engaging the nut onto the threaded bolt shank.

21. The method of claim 17, further comprising disposing the spring assembly onto the bolt between at least one of the bolt head and the nut and the first flange of the first ceramic matrix composite component of the mid-turbine frame and the second flange of the second component of the mid-turbine frame.

22. The method of claim 17, wherein the spring assembly comprises at least one Belleville washer.

23. The method of claim 22, wherein the spring assembly comprises a plurality of Belleville washers.

24. The method of claim 23, wherein at least one of the plurality of Belleville washers faces concave away from and adjacent to the bolt head.

25. The method of claim 24, wherein the plurality of Belleville washers include Belleville washers facing in opposite directions.

26. The method of claim 17, wherein the second component comprises a ceramic matrix composite material.