Fuel cell system having energy recuperation
A fuel cell system comprises a first fuel cell stack pair with a first fuel cell stack and a second fuel cell stack, a first compressor arrangement, and a first turbine arrangement, wherein the first compressor arrangement can be coupled to cathode inlets of the fuel cell stack of the first fuel cell stack pair, wherein the first turbine arrangement can be coupled to cathode outlets of the fuel cell stack of the first fuel cell stack pair, wherein the first turbine arrangement comprises a shaft, a first turbine which is connected to the shaft, a second turbine which is connected to the shaft, and a generator which is connected to the shaft, wherein the first compressor arrangement comprises at least one electrically operable compressor, and wherein the generator can be coupled to the at least one electrically operable compressor.
1. A fuel cell system ( 2 , 62 , 70 , 72 ) comprising:
at least one fuel cell stack ( 6 , 8 ) each having an anode inlet ( 40 ), an anode outlet ( 42 ), a cathode inlet ( 10 ), and a cathode outlet ( 12 ),
a turbine arrangement ( 14 ), and
an oxidant supply means for supplying an oxidant to the respective cathode inlet ( 10 ),
wherein the turbine arrangement ( 14 ) is arranged downstream of the respective cathode outlet ( 12 ) of at least one of the at least one fuel cell stack ( 6 , 8 , 64 ) and can be coupled to the cathode outlet ( 12 ),
wherein the turbine arrangement ( 14 ) comprises a shaft, at least one turbine ( 16 , 18 ) which is connected to the shaft, and a generator ( 22 ) which is connected to the shaft ( 20 ),
wherein the oxidant supply means and the turbine arrangement ( 14 ) can be operated independently of each other,
wherein the generator ( 22 ) of the turbine arrangement ( 14 ) is configured as a motor/generator unit and drives the at least one turbine ( 16 , 18 ) of the turbine arrangement ( 14 ) in an emergency operating mode in an event of failure of the oxidant supply means, by supplying an electrical voltage to the generator ( 22 ), and
wherein the at least one turbine ( 16 , 18 ) is configured to supply air in a reverse flow direction to at least one of the at least one fuel cell stack ( 6 , 8 , 64 ) in a driven state.
2. The fuel cell system ( 2 , 62 , 70 , 72 ) according to claim 1 ,
further comprising at least one selectively openable turbine bypass ( 26 ) for controlling a turbine output of the at least one turbine ( 16 , 18 ).
3. The fuel cell system ( 2 , 62 , 70 , 72 ) according to claim 1 ,
wherein at least one pressure control valve ( 28 ) is arranged upstream or downstream of the at least one turbine ( 16 , 18 ).
4. The fuel cell system ( 2 , 62 , 70 , 72 ) according to claim 1 ,
wherein the at least one fuel cell stack ( 6 , 8 , 64 ) comprises at least one cathode bypass ( 38 ) which is configured to supply an oxidant flow provided by the oxidant supply means at least partially directly to the respective turbine ( 16 , 18 ) of the turbine arrangement ( 14 ).
5. The fuel cell system ( 2 , 62 , 70 , 72 ) according to claim 1 ,
wherein the turbine arrangement ( 14 ) comprises a first turbine ( 16 ) and a second turbine ( 18 ), and
wherein the first turbine ( 16 ) and the second turbine ( 18 ) can be coupled to the respective cathode outlet ( 12 ) of the at least one fuel cell stack ( 6 , 8 , 64 ).
6. The fuel cell system ( 2 , 62 , 70 , 72 ) according to claim 5 ,
wherein the at least one fuel cell stack ( 6 , 8 , 64 ) comprises two or more fuel cell stacks ( 6 , 8 , 64 ), and
wherein the two turbines ( 16 , 18 ) can each be coupled to the cathode outlets ( 12 ) of at least two of the fuel cell stacks ( 6 , 8 , 64 ).
7. The fuel cell system ( 2 , 62 , 70 , 72 ) according to claim 5 ,
wherein the at least one fuel cell stack ( 6 , 8 , 64 ) comprises at least two fuel cell stacks ( 6 , 8 , 64 ), and
wherein the two turbines ( 16 , 18 ) can each be coupled to different cathode outlets ( 12 ) of at least two fuel cell stacks ( 6 , 8 , 64 ).
8. The fuel cell system ( 2 , 62 , 70 , 72 ) according to claim 1 ,
wherein the at least one fuel cell stack ( 6 , 8 , 64 ) comprises at least one fuel cell stack ( 64 ), the cathode outlet ( 12 ) of which can be operated independently of the turbine arrangement ( 14 ).
9. The fuel cell system ( 2 , 62 , 70 , 72 ) according to claim 1 ,
wherein upstream of the cathode inlet ( 10 ) of at least one of the fuel cell stacks ( 6 , 8 , 64 ) there is a supply air heat exchanger ( 74 ) that is thermally connected to the respective cathode outlet ( 12 ) to transfer heat from air flowing into the cathode inlet ( 10 ) to exhaust air from the cathode outlet ( 12 ).