Solid Oxide Fuel Cell/Turbine Hybrid Power System for Advanced Aero-propulsion and Power

Award Information
Agency:
National Aeronautics and Space Administration
Branch
n/a
Amount:
$99,999.00
Award Year:
2004
Program:
STTR
Phase:
Phase I
Contract:
NNC04CA94C
Award Id:
72065
Agency Tracking Number:
030198
Solicitation Year:
n/a
Solicitation Topic Code:
n/a
Solicitation Number:
n/a
Small Business Information
3 Great Pasture Rd., Danbury, CT, 06813
Hubzone Owned:
N
Minority Owned:
N
Woman Owned:
N
Duns:
050627884
Principal Investigator:
PinakinPatel
Principal Investigator
(203) 825-6072
ppatel@fce.com
Business Contact:
RossLevine
Dir. Contracts & Cont. Counsel
(203) 825-6057
rlevine@fce.com
Research Institute:
Georgia Tech Research Corporation
Hendrickx Toussaint
505 Tenth Steet, N.W.
Atlanta, GA, 30332
(770) 528-7826
Nonprofit college or university
Abstract
Solid oxide fuel cell (SOFC)/ gas turbine hybrid power systems (HPSs) have been recognized by federal agencies and other entities as having the potential to operate at unprecedented levels of performance for terrestrial applications (e.g., 70% power generation efficiencies with significantly mitigated criteria pollutant and noise emissions). An innovative approach is proposed for leveraging competencies in high temperature fuel cell stack and system simulation/validation and manufacturing, in conjunction with robust aeronautical sub-system/system design capabilities, to optimize these promising systems for novel aerospace propulsion and power applications. NASA GRC?s ?Protect the Environment? and ?Explore New Aerospace Missions? initiatives are addressed via the proposed technical contributions to both alternative non-combustion and alternative fuels/combustion aeronautical power generation. SOFCs, the non-combustion alternative, serve as a promising fuel infrastructural bridge; because the technology engenders practical efficiencies between 45-60%, and it is amenable to a variety of fuel feeds (including hydrocarbons and hydrogen). The inclusion of the SOFCs into modified Brayton cycles also enhances combustion-based power/propulsion via its byproduct enhancement of the fuel quality and heating value upstream of the combustor. A rigorous conceptual design/validation study is proposed for Phase I, corresponding proof-of-concept enabling hardware development for Phase II, and NASA/non-NASA commercialization efforts for Phase III.

* information listed above is at the time of submission.

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