Device for diagnosing valve failure of fuel cell system
US-2024347748-A1 · Oct 17, 2024 · US
US2025070208A1 · US · A1
| Field | Value |
|---|---|
| Publication number | US-2025070208-A1 |
| Application number | US-202318724905-A |
| Country | US |
| Kind code | A1 |
| Filing date | Jan 6, 2023 |
| Priority date | Jan 7, 2022 |
| Publication date | Feb 27, 2025 |
| Grant date | — |
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The present disclosure generally relates to systems and methods for operating a fuel cell system including operating a fuel cell comprising a membrane electrode assembly, dynamically operating an air handling system comprising an air compressor which controls stack pressure and air flow in the fuel cell stack system, determining a parasitic loss in the fuel cell system based on the air handling system, and operating the fuel cell system in transient conditions based on a transient system curve. The transient system curve may be based on a relationship between the stack pressure and stack temperature, and the parasitic loss.
Opening claim text (preview).
The invention claimed is: 1 . A method of operating a fuel cell system comprising: operating a fuel cell comprising a membrane electrode assembly, flowing fuel through the fuel cell at an operating fuel pressure, dynamically operating an air handling system comprising an air compressor, wherein the air compressor controls a stack pressure and an air flow in the fuel cell system, determining a parasitic loss in the fuel cell system based on the air handling system, and operating the fuel cell system under transient conditions with a transient air flow, wherein the transient air flow is based on the stack pressure, a stack temperature, and the parasitic loss in the fuel cell system. 2 . The method of claim 1 , further comprising determining the parasitic loss in the fuel cell system based on a radiator fan or a cooling pump. 3 . The method of claim 1 , further comprising operating the fuel cell system under the transient conditions wherein the transient air flow is based on a maximum net power objective. 4 . The method of claim 1 , wherein the transient air flow is determined based on a time required to warm-up the fuel cell system and subsequently increase stack pressure, and wherein the transient air flow is indicated by a transient system curve. 5 . The method of claim 4 , further comprising operating the fuel cell system under transient conditions wherein the transient system curve is based on a maximum air flow, and wherein the maximum air flow is based on a maximum amount of air that can be supplied by the air handling system of the fuel cell system. 6 . The method of claim 4 , further comprising operating the fuel cell system under transient conditions wherein the transient system curve converges to a steady state air flow, and wherein the steady state air flow is an amount of air that can be supplied by the air handling system of the fuel cell system under steady state conditions. 7 . The method of claim 4 , wherein the transient air flow exceeds a steady state air flow and increases current density output to compensate for a lack in voltage, wherein as the stack temperature of the fuel cell system increases, the stack pressure increases and the transient air flow converges to equal the steady state air flow, and wherein the steady state air flow is an amount of air that can be supplied by the air handling system of the fuel cell system under steady state conditions. 8 . The method of claim 4 , wherein the transient air flow of the fuel cell system does not exceed the steady state air flow, and wherein the steady state air flow is an amount of air that can be supplied by the air handling system of the fuel cell system under steady state conditions. 9 . The method of claim 8 , wherein the fuel cell system is supported by auxillary components comprising a DC/DC converter or a battery system. 10 . The method of claim 1 , comprising controlling the transient air flow of air to be below a steady state air flow and a maximum air flow, wherein the steady state air flow is an amount of air that can be supplied by the air handling system of the fuel cell system under steady state conditions, and wherein the maximum air flow is based on a maximum amount of air that can be supplied by the air handling system of the fuel cell system. 11 . The method of claim 1 , wherein the transient system curve is a hybrid curve controlled to be within a steady state flow curve and a maximum flow curve, wherein the steady state flow curve is based on an amount of air that can be supplied by the air handling system of the fuel cell system under steady state conditions and the maximum flow curve is based on a maximum amount of air that can be supplied by the air handling system of the fuel cell system, and wherein a warming time of the fuel cell system corresponds closely to a response time of the air handling system. 12 . The method of claim 1 , wherein the transient system curve is located to the left of a steady state flow curve based on an amount of air that can be supplied by the air handling system of the fuel cell system under steady state conditions, and wherein the fuel cell system is configured to undergo a rapid cool-down. 13 . The method of claim 12 , wherein heat rejection from the fuel cell system is slower than a ramp-down time of the air compressor. 14 . The method of claim 12 , wherein ambient temperature of the fuel cell system ranges from about 35° C. to about 45° C. 15 . The method of claim 1 , wherein the fuel cell system is supported by a fuel handling system that varies the operating fuel pressure in accordance with the air handling system and the stack pressure. 16 . A method of operating a fuel cell system comprising: operating a fuel cell comprising a membrane electrode assembly, dynamically operating an air handling system comprising an air compressor, wherein the air compressor is configured to operate with a transient response to an input signal, wherein the air compressor is configured to control stack pressure and air flow in the fuel cell system, determining a parasitic loss in the fuel cell system based on the air handling system, controlling the air compressor by a controller, operating the fuel cell system under transient conditions with a transient air flow, wherein the transient air flow is based on the stack pressure and stack temperature. 17 . The method of claim 16 , wherein the controller is configured to compare an actual revolutions per minute (RPM) of the air compressor to a target RPM of the air compressor and supply electrical power until the target RPM is achieved. 18 . The method of claim 16 , wherein performance of the air compressor depends on altitude, and wherein operating range of the fuel cell system, a steady state flow curve of the fuel cell system, and a maximum flow curve of the fuel cell stack system is configured to change with altitude. 19 . The method of claim 16 , wherein performance of the air compressor depends on aging of the fuel cell, and wherein current density and the air flow are increased to compensate for a decrease in voltage in the fuel cell. 20 . The method of claim 16 , further comprising determining the parasitic losses in the fuel cell system based on the air handling system, a radiator fan or a cooling pump.
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