Details
Originalsprache | Englisch |
---|---|
Aufsatznummer | 121014 |
Seitenumfang | 8 |
Fachzeitschrift | Journal of Engineering for Gas Turbines and Power |
Jahrgang | 144 |
Ausgabenummer | 12 |
Frühes Online-Datum | 7 Okt. 2022 |
Publikationsstatus | Veröffentlicht - Dez. 2022 |
Abstract
This paper focuses on the design, construction, and the experimental testing of an anode recirculation blower (ARB) based on a turbocompressor for PEM-FCs. The blower presented consists of a high-speed centrifugal compressor, driven by a so-called media-gap motor. Additionally, it includes a droplet separator to eliminate liquid water from the anode loop. The aerodynamic design is based on one-dimensional-correlations and three-dimensional-numerical CFD simulations. Different gas compositions of hydrogen, nitrogen, and water vapor are considered in the design, depending on the operating points of a PEM-FC. The gas composition has a significant influence on the achievable pressure ratio at constant compressor speeds, depending mainly on the specific heat capacity of the gas. Performance maps for different gas compositions are calculated using CFD for the designed ARB. A prototype is built and tested. The results validate the CFD predictions and show that the operating range of a PEM fuel cell can be covered with the present blower. In addition, it could be shown that an enthalpy-based approach using common characteristic numbers of turbomachines, allows converting performance maps-acquired with different gas compositions-into one another. This allows the performance map prediction for different gas compositions based on existing performance maps. This approach is illustrated by numerical and experimental results.
ASJC Scopus Sachgebiete
- Ingenieurwesen (insg.)
- Maschinenbau
- Ingenieurwesen (insg.)
- Luft- und Raumfahrttechnik
- Energie (insg.)
- Energieanlagenbau und Kraftwerkstechnik
- Energie (insg.)
- Feuerungstechnik
- Energie (insg.)
- Kernenergie und Kernkraftwerkstechnik
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in: Journal of Engineering for Gas Turbines and Power, Jahrgang 144, Nr. 12, 121014, 12.2022.
Publikation: Beitrag in Fachzeitschrift › Artikel › Forschung › Peer-Review
}
TY - JOUR
T1 - Experimentally Validated Design of an Anode Recirculation Blower for Polymer-Electrolyte-Membrane Fuel Cells Under Variable Fluid Composition
AU - Nachtigal, Philipp
AU - Kentschke, Thorge
AU - Seume, Joerg R.
N1 - Funding Information: This paper contains some of the results of the publicly funded project “REZEBT”, which has been supported by the German Federal Ministry for Economic Affairs and Climate Action, based on a resolution of the German Bundestag. The project is organized within the framework of the ZIM program. The authors want to thank GþL innotec for the cooperation in the REZEBT project and for the hard- ware of the anode recirculation blower provided for the acquisition of the experimental results presented in this paper.
PY - 2022/12
Y1 - 2022/12
N2 - This paper focuses on the design, construction, and the experimental testing of an anode recirculation blower (ARB) based on a turbocompressor for PEM-FCs. The blower presented consists of a high-speed centrifugal compressor, driven by a so-called media-gap motor. Additionally, it includes a droplet separator to eliminate liquid water from the anode loop. The aerodynamic design is based on one-dimensional-correlations and three-dimensional-numerical CFD simulations. Different gas compositions of hydrogen, nitrogen, and water vapor are considered in the design, depending on the operating points of a PEM-FC. The gas composition has a significant influence on the achievable pressure ratio at constant compressor speeds, depending mainly on the specific heat capacity of the gas. Performance maps for different gas compositions are calculated using CFD for the designed ARB. A prototype is built and tested. The results validate the CFD predictions and show that the operating range of a PEM fuel cell can be covered with the present blower. In addition, it could be shown that an enthalpy-based approach using common characteristic numbers of turbomachines, allows converting performance maps-acquired with different gas compositions-into one another. This allows the performance map prediction for different gas compositions based on existing performance maps. This approach is illustrated by numerical and experimental results.
AB - This paper focuses on the design, construction, and the experimental testing of an anode recirculation blower (ARB) based on a turbocompressor for PEM-FCs. The blower presented consists of a high-speed centrifugal compressor, driven by a so-called media-gap motor. Additionally, it includes a droplet separator to eliminate liquid water from the anode loop. The aerodynamic design is based on one-dimensional-correlations and three-dimensional-numerical CFD simulations. Different gas compositions of hydrogen, nitrogen, and water vapor are considered in the design, depending on the operating points of a PEM-FC. The gas composition has a significant influence on the achievable pressure ratio at constant compressor speeds, depending mainly on the specific heat capacity of the gas. Performance maps for different gas compositions are calculated using CFD for the designed ARB. A prototype is built and tested. The results validate the CFD predictions and show that the operating range of a PEM fuel cell can be covered with the present blower. In addition, it could be shown that an enthalpy-based approach using common characteristic numbers of turbomachines, allows converting performance maps-acquired with different gas compositions-into one another. This allows the performance map prediction for different gas compositions based on existing performance maps. This approach is illustrated by numerical and experimental results.
KW - droplet
KW - fuel cell applications
KW - hydrogen
KW - turbomachinery
UR - http://www.scopus.com/inward/record.url?scp=85144824164&partnerID=8YFLogxK
U2 - 10.1115/1.4055667
DO - 10.1115/1.4055667
M3 - Article
VL - 144
JO - Journal of Engineering for Gas Turbines and Power
JF - Journal of Engineering for Gas Turbines and Power
SN - 0742-4795
IS - 12
M1 - 121014
ER -