| Type of Document |
Thesis |
| Author |
DeRoche, Peter Michael
|
| URN |
etd-07142008-121836 |
| Title |
A Microjet-based Reactant Delivery Method for PEM Fuel Cells |
| Degree |
Master of Science |
| Department |
Mechanical Engineering, Department of |
| Advisory Committee |
| Advisor Name |
Title |
| Anjaneyulu Krothapalli |
Committee Chair |
| Brenton Graska |
Committee Member |
| Juan Ordonez |
Committee Member |
|
| Keywords |
|
| Date of Defense |
2008-06-10 |
| Availability |
unrestricted |
Abstract
A microjet-based reactant delivery method was implemented in a prototype PEM fuel cell. A commercially available fuel cell was procured that utilizes a conventional reactant delivery method. The prototype was designed with an identical active area so that number of variables leading to differences in performance between the two fuel cells would be minimal. The MEAs inside each fuel cell were identical. Both the prototype and commercially available cell were tested under a variety of operating conditions. Conditions that were tested include: low air stoichiometry flow rates, high air stoichiometry flow rates, varying relative humidity, varying hydrogen stagnation pressure, varying stack temperatures, and varying air backpressure. The performance of each fuel cell was compared for each set of test conditions. The results show that the prototype microjet fuel cell experienced lower activation losses than the commercially available fuel cell. Testing revealed several design flaws in the prototype. Also, there are indications that the microjet design allows the fuel cell to be less affected by high stack temperatures.
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| Files |
| Filename |
Size |
Approximate Download Time
(Hours:Minutes:Seconds)
|
| 28.8 Modem |
56K Modem |
ISDN (64 Kb) |
ISDN (128 Kb) |
Higher-speed Access |
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DeRochePThesis.pdf |
9.89 Mb |
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00:23:32 |
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