COMBINED CERAMIC MATRIX COMPOSITE AND THERMOELECTRIC STRUCTURE FOR ELECTRIC POWER GENERATION

• US 20150364667A1
• Filed: 01/18/2013
• Published: 12/17/2015
• Est. Priority Date: 01/18/2013
• Status: Abandoned Application

• Current Assignee: United Technologies Corporation (Raytheon Technologies Corporation d/b/a RTX)
• Original Assignee: United Technologies Corporation (Raytheon Technologies Corporation d/b/a RTX)
• Inventors: Jarmon, David C.
• Application Number:
  US14/759,678
• Publication Number:
  US 20150364667A1
• Time in Patent Office: Days
• US Class Current: 1/1
• CPC Class Codes: F05D 2220/76 an electrical generator
• CPC Class Codes: H10N 10/01 Manufacture or treatment
• CPC Class Codes: H10N 10/13 characterised by the heat-exchanging means at the junction
• CPC Class Codes: H10N 10/17 characterised by the structure or configuration of the cell or thermocouple forming the device
• CPC Class Codes: H10N 10/813 the junction being separable, e.g. using a spring
• CPC Class Codes: Y10T 29/49119 Brush

Abstract

An electrical power generation system consists of a ceramic hot face liner of a gas path enclosure thermally and mechanically connected to thermoelectric elements mounted on a conformal thermally conducting layer on the liner. Cooling channels connected to the backside of the thermoelectric elements provide a thermal gradient across the elements and resulting electrical power output. Clamps to maintain thermal and physical contact of all elements in the system are provided to maximize power generation.

Claims

1. An electric power generation system comprising:

a ceramic liner of a hot gas path enclosure;

a thermally conductive conformal layer on the liner shaped to provide a plurality of conformal mounting surfaces;

thermoelectric elements mounted on the thermally conductive conformal layer with an inner surface of each thermoelectric element adjacent one of the conformal mounting surfaces of the thermally conductive conformal layer;

cooling channels connected to an outer surface of the thermoelectric elements; and

a clamp that surrounds the ceramic liner, thermally conductive conformal layer, thermoelectric elements, and cooling channels for applying a compressive clamping force to maintain thermal and physical contact between the ceramic liner, thermally conductive conformal layer, thermoelectric elements and cooling channels.

2. The system of claim 1, wherein the ceramic liner comprises a ceramic matrix composite (CMC).

3. The system of claim 2, wherein the ceramic matrix composite is selected from the group consisting of carbon fiber reinforced silicon carbide (C/SiC), carbon fiber reinforced carbon(C/C), silicon carbide fiber reinforced silicon carbide (SiC/SiC), silicon melt infiltrated silicon carbide reinforced silicon carbide (MI SiC/SiC) and mixtures thereof.

4. The system of claim 1, wherein the thermally conductive conformal layer comprises silicon.

5. The system of claim 1, wherein the cooling channels comprise metal channels for carrying a fluid coolant.

6. The system of claim 1, wherein the clamp to maintain thermal and physical contact between the components comprises springs surrounding the enclosure thereby putting the components under compression.

7. The system of claim 6, wherein the springs are canted coil springs.

8. The system of claim 1 further comprising a reaction barrier layer between the conformal layer and the thermoelectric elements.

9. The system of claim 1 further comprising a compliant layer between the thermoelectric elements and the cooling channels.

10. The system of claim 1 further comprising an outer protective metal shell.

11. A method comprising:

fabricating a ceramic hot gas path liner;

depositing a layer of thermally conducting material on the liner;

forming flat conformal surfaces on the thermally conducting layer;

adding thermoelectric elements to the flat conformal surfaces of the thermally conducting layer such that an inner surface of the thermoelectric elements is in direct thermal and physical contact with the flat conformal surfaces of the thermally conducting layer;

adding metal cooling ducts to the outer surface of the thermoelectric elements such that the surfaces of the metal cooling ducts are in direct thermal and physical contact with the outer surfaces of the thermoelectric elements; and

applying a compressive clamping force to the metal cooling ducts, thermoelectric elements, thermally conducting layer, and hot gas path liner to maintain thermal and physical contact between them that creates a thermal gradient in the thermoelectric elements and forms an electric power generation system.

12. The method of claim 11, wherein the ceramic hot gas path liner comprises a ceramic matrix composite (CMC).

13. The method of claim 12, wherein the ceramic matrix composite comprises at least one of carbon fiber reinforced silicon carbide (C/SiC), carbon fiber reinforced carbon (C/C), silicon carbide fiber reinforced silicon carbide (SiC/SiC), silicon melt infiltrated silicon carbide fiber reinforced silicon carbide (MI SiC/SiC), and mixtures thereof.

14. The method of claim 11, wherein the thermally conducting material comprises silicon.

15. The method of claim 11, wherein the cooling channels comprise metal channels carrying a fluid coolant.

16. The method of claim 11, wherein the clamp to maintain thermal and physical contact between the components comprises springs surrounding the enclosure, thereby putting the components under compression.

17. The method of claim 16, wherein the springs are canted coil springs.

18. The method of claim 11, further comprising forming a reaction barrier layer between the conformal layer and the thermoelectric elements.

19. The method of claim 11, further comprising forming a compliant layer between the thermoelectric elements and the cooling channels.

20. The method of claim 11, further comprising positioning an outer protective metal shell around the electric power generation system.