Fuel cell integral bundle assembly including ceramic open end seal and vertical and horizontal thermal expansion control
원문보기
IPC분류정보
국가/구분
United States(US) Patent
등록
국제특허분류(IPC7판)
H01M-008/12
H01M-008/24
출원번호
US-0543718
(2009-08-19)
등록번호
US-8163433
(2012-04-24)
발명자
/ 주소
Zafred, Paolo R.
Gillett, James E.
출원인 / 주소
Siemens Energy, Inc.
인용정보
피인용 횟수 :
3인용 특허 :
16
초록▼
A plurality of integral bundle assemblies contain a top portion with an inlet fuel plenum and a bottom portion containing a base support, the base supports a dense, ceramic air exhaust manifold having four supporting legs, the manifold is below and connects to air feed tubes located in a recuperator
A plurality of integral bundle assemblies contain a top portion with an inlet fuel plenum and a bottom portion containing a base support, the base supports a dense, ceramic air exhaust manifold having four supporting legs, the manifold is below and connects to air feed tubes located in a recuperator zone, the air feed tubes passing into the center of inverted, tubular, elongated, hollow electrically connected solid oxide fuel cells having an open end above a combustion zone into which the air feed tubes pass and a closed end near the inlet fuel plenum, where the open end of the fuel cells rest upon and within a separate combination ceramic seal and bundle support contained in a ceramic support casting, where at least one flexible cushion ceramic band seal located between the recuperator and fuel cells protects and controls horizontal thermal expansion, and where the fuel cells operate in the fuel cell mode and where the base support and bottom ceramic air exhaust manifolds carry from 85% to all of the weight of the generator.
대표청구항▼
1. An integral bundle assembly comprising: a top inlet fuel portion; an inlet fuel stream near the top portion; inverted, tubular, elongated, hollow, electrically connected solid oxide fuel cells disposed below the top portion, the fuel cells set to operate in the fuel cell mode; internal heat recup
1. An integral bundle assembly comprising: a top inlet fuel portion; an inlet fuel stream near the top portion; inverted, tubular, elongated, hollow, electrically connected solid oxide fuel cells disposed below the top portion, the fuel cells set to operate in the fuel cell mode; internal heat recuperator disposed below the fuel cells; an open end fuel cell seal between a combustion zone and fuel cells; two cushion ceramic band seal layers between the open end fuel cell seal and the recuperator which cushion band seal layers control horizontal thermal expansion between integral bundle assemblies; a bottom portion of dense ceramic casting having a plurality of bottom legs formed as a ceramic exhaust manifold supporting the recuperator and fuel cells; and inlet air feed tubes feeding to the fuel cells, the air feed tubes connecting with a bottom oxidant feed, where the open end fuel cell seal comprises a ceramic seal that conforms to the open ends of the fuel cells which fuel cells rest upon separate fuel cell bundle support beams. 2. The integral bundle assembly of claim 1, wherein a sliding pin is disposed in the inlet fuel top portion, and, along with the plurality of bottom legs of the bottom portion ceramic casting provide a vertical integral bundle assembly thermal expansion center and where the bottom portion of dense ceramic casting carries all of the internal weight of the integral bundle assembly. 3. The integral bundle assembly of claim 2, wherein the sliding pin is metallic. 4. The integral bundle assembly of claim 1, wherein both the ceramic seal and support beam are disposed in a separate support casting, all above a combustion zone, a recuperator, and at least one cushion ceramic band seal that accommodates thermal expansion. 5. A plurality of integral bundle assemblies each comprising: a top inlet fuel portion including a top plate and a top vertical metallic sliding pin which is slidable within the top plate of the assemblies, to accommodate assembly axial thermal expansion and a bottom portion receiving air inlet feed, which is made of dense, molded casting formed as a ceramic air exhaust manifold part which air exhaust manifold part is below and provides a receptacle for an air inlet box and inlet air feed tubes, the exhaust manifold located below an internal heat recuperator, said air feed tubes passing into the center of inverted, tubular, elongated, hollow electrically connected solid oxide fuel cells having an open end above the internal heat recuperator, through which the air feed tubes pass and a closed end near the inlet fuel portion, said fuel cells comprising a fuel cell stack bundle, where the fuel cells operate in the fuel cell mode and where the bottom ceramic air exhaust manifolds carry at least 85% of the internal weight of the integral bundle assembly, and ceramic exhaust manifold bottom four point ceramic legs (keyways) provide a central axis with the top sliding metallic pin to provide a vertical integral bundle assembly thermal expansion center, where each integral bundle assembly is separated from adjacent bundle assemblies by at least one flexible, circumferentially disposed, cushion ceramic band seal layer located between the recuperator and the fuel cells, and where a ceramic seal conforms to the open end of the fuel cells which rest upon a separate fuel cell bundle support beam, the combination seal and support beam disposed in a separate ceramic support casting, all disposed above the cushion ceramic band seal layer; and where the interior of the integral bundle assemblies contain primarily electrically generating components. 6. The integral bundle assembly of claim 5, wherein the dense ceramic air exhaust manifolds are plural, inorganic, laminated freeze molded castings. 7. The integral bundle assembly of claim 6, wherein the dense ceramic air exhaust manifold castings have interfacial bonds among plural inorganics used which withstand temperatures of 1,000° C. without delamination, and are 90 vol. % to 98 vol. % dense. 8. The integral bundle assembly of claim 5, wherein the dense ceramic air exhaust manifold castings are made from inorganic materials selected from the group consisting of aluminas, silicas, magnesias, chromites, spinels, clays and mixtures thereof. 9. The integral bundle assembly of claim 5, wherein the dense ceramic air exhaust manifold castings are made from alumina. 10. The integral bundle assembly of claim 5, wherein the solid oxide fuel cells are tubular. 11. The integral bundle assembly of claim 5, wherein the solid oxide fuel cells are of delta configuration. 12. The integral bundle assembly of claim 5, where the bottom ceramic air exhaust manifolds are mounted on a metallic base support. 13. The integral bundle assembly of claim 5, where the at least one flexible band seal layer accommodates horizontal thermal expansion between integral bundle assemblies. 14. The integral bundle assembly of claim 5, wherein a portion of the exterior of the fuel cells that fuel contacts, contain reforming coating, to reform hydrocarbon fuel in-situ on the fuel cell. 15. The integral bundle assembly of claim 5, wherein the only weight loads applied to the solid oxide fuel cells' are weight loads generated internally solely by the fuel cells' own weight. 16. The integral bundle assembly of claim 5, wherein the air inlet feed tubes which pass through a recuperator communicate with an air box below the solid oxide fuel cells and the air box is connected to bottom air inlet manifolds. 17. The integral bundle assembly of claim 5, wherein the solid oxide fuel cells have an open end above a combustion zone, which combustion zone is above a recuperator, and have a closed end near the inlet fuel plenum, and where the ceramic seal openings accommodate the fuel cell open ends are tapered to ensure a tight fit between the seal and the fuel cells. 18. The integral bundle assembly of claim 5, wherein a ceramic support casting supports a plurality of bundle support beams within it as well as a top compliant ceramic seal.
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