Integrated PEMFC Flow Field Design Concept for Gravity Independent Passive Water Removal

Award Information
Agency:
National Aeronautics and Space Administration
Branch
n/a
Amount:
$70,000.00
Award Year:
2006
Program:
SBIR
Phase:
Phase I
Contract:
NNJ06JD71C
Award Id:
77528
Agency Tracking Number:
054145
Solicitation Year:
n/a
Solicitation Topic Code:
n/a
Solicitation Number:
n/a
Small Business Information
400 West Cummings Park, Woburn, MA, 01801
Hubzone Owned:
N
Minority Owned:
N
Woman Owned:
N
Duns:
161844204
Principal Investigator:
MichaelPien, Ph.D.
Principal Investigator
(781) 938-5300
mpien@fuelcell.com
Business Contact:
RadhaJalan
President / CEO
(781) 938-5300
jbernier@fuelcell.com
Research Institute:
n/a
Abstract
The primary power systems for Space Shuttles and future space vehicles are based on fuel cells. Due to inherent fundamental performance, safety and reliability, NASA is interested in replacing the present alkaline fuel cell system with PEM systems. However, the conventional use by PEM systems of O2 reactant gas recirculation to remove product water, enhance cell uniformity, and control humidity could pose a serious safety concern. A fundamentally new PEM fuel cell design concept is proposed that removes liquid product water by controlled convection and wicking through layered porous structures that are integrated into each cell separator plate. This unique integrated flow field (IFF) concept also automatically and passively clears channels blocked by droplets. Furthermore, the same design includes transport of product water back to the entire flow field for humidification and greater cell performance. The IFF design enables high pressure and high voltage operation resulting in higher efficiency. For removal of product water vapor from the cell, the design concept includes ejectors to passively generate a modest gas circulation. In conclusion, this design innovation will significantly simplify the PEM operating system while generating higher performance and foster greater long-term safety in zero-g as well as ordinary gravity applications.

* information listed above is at the time of submission.

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