Oxygen enrichment device comprising at least two molecular sieves for supplying a fuel cell system
원문보기
IPC분류정보
국가/구분
United States(US) Patent
등록
국제특허분류(IPC7판)
H01M-008/06
B01D-050/00
출원번호
US-0120001
(2008-05-13)
등록번호
US-8313868
(2012-11-20)
우선권정보
DE-10 2005 054 888 (2005-11-17)
발명자
/ 주소
Gruendel, Harald
Stolte, Ralf-Henning
출원인 / 주소
Airbus Operations GmbH
대리인 / 주소
Ingrassia Fisher & Lorenz P.C.
인용정보
피인용 횟수 :
0인용 특허 :
1
초록▼
A system is provided that combines an oxygen enrichment device (OBOGS) for generating oxygen-enriched air with a fuel cell system that includes, but is not limited to a fuel cell for using the oxygen-enriched air as a reaction gas within the fuel cell, as a result of which the output of the fuel cel
A system is provided that combines an oxygen enrichment device (OBOGS) for generating oxygen-enriched air with a fuel cell system that includes, but is not limited to a fuel cell for using the oxygen-enriched air as a reaction gas within the fuel cell, as a result of which the output of the fuel cell is improved while the size and weight of the fuel cell remain the same.
대표청구항▼
1. A system, comprising: an oxygen enrichment device for generating oxygen-enriched air; anda fuel cell system with a fuel cell using the oxygen-enriched air as a reaction gas within the fuel cell;wherein the oxygen enrichment device is an on board oxygen generation system on board oxygen generation
1. A system, comprising: an oxygen enrichment device for generating oxygen-enriched air; anda fuel cell system with a fuel cell using the oxygen-enriched air as a reaction gas within the fuel cell;wherein the oxygen enrichment device is an on board oxygen generation system on board oxygen generation system which is supplied with air by a first air supply source, a second air supply source, and a third air supply source, and which, by increasing particle pressure of the oxygen in the air supplies the oxygen-enriched air to the fuel cell system;wherein the first air supply source supplies cooled bleed air from an engine of an aircraft to the on board oxygen generation system;wherein the second air supply source is an air conditioning system that supplies conditioned air to the on board oxygen generation system;wherein the third air supply source supplies outgoing air from a cabin to the on board oxygen generation system, the first, second, and third air supply sources in parallel arrangement and operable to supply air separately or in combination with each other. 2. The system of claim 1, wherein an air supply source supplies external air that has been compressed by an electrical compressor to the on board oxygen generation system. 3. The system of claim 1, wherein the on board oxygen generation system comprises at least two molecular sieves for binding nitrogen and for letting oxygen pass, with both nitrogen and oxygen being present in the air supplied by the at least one of the first air supply source, the second air supply source, and the third air supply source so that on a first outlet (B) of the on board oxygen generation system the oxygen-enriched air is supplied. 4. The system of claim 3, wherein alternately one molecular sieve of the at least two molecular sieves binds the nitrogen and lets the oxygen pass so as to generate the oxygen-enriched air, while the other molecular sieve of the at least two molecular sieves uses this oxygen-enriched air for its regeneration and supplies nitrogen-enriched air to a second outlet of the on board oxygen generation system. 5. The system of claim 3, comprising a sensor that detects the oxygen in the oxygen-enriched air and if said oxygen drops below a predetermined threshold value, changes operation of the at least two molecular sieves from the one molecular sieve to the other molecular sieve. 6. The system of claim 5, wherein the oxygen-enriched air is used as an inert gas within a tank system and/or for nitrogen inerting a compartment in the fuel cell system. 7. The system of claim 1, wherein the oxygen-enriched air generated by the oxygen enrichment device is fed as an educt gas into a cathode inlet of the fuel cell. 8. The system of claim 3, wherein at least one molecular sieve of the at least two molecular sieves is a zeolite. 9. The system of claim 1, wherein the on board oxygen generation system filters out impurities in the air supplied by the at least one of the first air supply source, the second air supply source, and the third air supply source so as to prevent contamination of the fuel cell. 10. A system, comprising: an oxygen enrichment device for generating oxygen-enriched air; anda fuel cell system with a fuel cell using the oxygen-enriched air as a reaction gas within the fuel cell;wherein the oxygen enrichment device is an on board oxygen generation system which is supplied with air by a first air supply source, a second air supply source, and a third air supply source, and which, by increasing particle pressure of the oxygen in the air supplies the oxygen-enriched air to the fuel cell system;wherein the first air supply source supplies cooled bleed air from an engine of an aircraft to the on board oxygen generation system;wherein the second air supply source is an air conditioning system that supplies conditioned air to the on board oxygen generation system; andwherein the third air supply source supplies outgoing air from a cabin to the on board oxygen generation system, the first, second, and third air supply sources in parallel arrangement and operable to each supply air through a different air supply path, either separately or in combination with each other. 11. A system, comprising: an oxygen enrichment device for generating oxygen-enriched air; anda fuel cell system with a fuel cell using the oxygen-enriched air as a reaction gas within the fuel cell;wherein the oxygen enrichment device is an on board oxygen generation system which is supplied with air by a first air supply source, a second air supply source, and a third air supply source, and which, by increasing particle pressure of the oxygen in the air supplies the oxygen-enriched air to the fuel cell system;wherein the first air supply source supplies cooled bleed air from an engine of an aircraft to the on board oxygen generation system;wherein the second air supply source is an air conditioning system that supplies conditioned air to the on board oxygen generation system; andwherein the third air supply source supplies outgoing air from a cabin to the on board oxygen generation system, the first, second, and third air supply sources in parallel arrangement and operable in combination to each supply air through a different air supply path.
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이 특허에 인용된 특허 (1)
Werth John, Fuel cell or a partial oxidation reactor or a heat engine and an oxygen-enriching device and method therefor.
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