| タイトル | Development of a Solid-Oxide Fuel Cell/Gas Turbine Hybrid System Model for Aerospace Applications |
| 本文（外部サイト） | http://hdl.handle.net/2060/20040073483 |
| 著者（英） | Freeh, Joshua E.; Brouwer, Jacob; Pratt, Joseph W. |
| 著者所属（英） | NASA Glenn Research Center |
| 発行日 | 2004-05-01 |
| 言語 | eng |
| 内容記述 | Recent interest in fuel cell-gas turbine hybrid applications for the aerospace industry has led to the need for accurate computer simulation models to aid in system design and performance evaluation. To meet this requirement, solid oxide fuel cell (SOFC) and fuel processor models have been developed and incorporated into the Numerical Propulsion Systems Simulation (NPSS) software package. The SOFC and reformer models solve systems of equations governing steady-state performance using common theoretical and semi-empirical terms. An example hybrid configuration is presented that demonstrates the new capability as well as the interaction with pre-existing gas turbine and heat exchanger models. Finally, a comparison of calculated SOFC performance with experimental data is presented to demonstrate model validity. Keywords: Solid Oxide Fuel Cell, Reformer, System Model, Aerospace, Hybrid System, NPSS |
| NASA分類 | Computer Programming and Software |
| レポートNO | GT2004-53616
E-14490
NASA/TM-2004-213054 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/222111 |
