TY - GEN
T1 - Assessing the performance of a microfabricated regenerator for Stirling space-power convertor
AU - Ibrahim, Mounir B.
AU - Keister, Jason
AU - Sun, Liyong
AU - Simon, Terry
AU - Mantell, Susan C.
AU - Gedeon, David
AU - Guidry, Dean
AU - Qiu, Songgang
AU - Wood, Gary
PY - 2005
Y1 - 2005
N2 - In this paper we provide a summary of accomplishments on phase I, and the early part of phase II, of our NASA regenerator microfabrication contract. We developed a microscale regenerator design based on state of the art analytical and computational tools. For this design we projected 6-9% efficiency improvement for the microfabricated regenerator. We were able to identify a manufacturing process and selected a vendor. This vendor completed EDM tools for fabricating the regenerator. The tool met specifications and they are ready to begin producing regenerators. We designed a Large Scale Mock-Up (LSMU) and began its fabrication. CFD modeling for fluid flow and heat transfer (both steady and oscillatory flow conditions) is proceeding for different geometries to assess: the effects of surface roughness, geometries such as a lenticular array, aligned parallel plates (equally and non-equally spaced), staggered parallel plates (equally and non-equally spaced), 3-D involute, and the LSMU model. Also, we examined adapting a test engine to incorporate the new microfabricated regenerator. The Sage code was used in this modeling exercise to compare computed results between the baseline random-fiber regenerator and the microfabricated regenerator. Sage modeled this new regenerator (the involute-element) as a simple foil-type regenerator. 3-D CFD analysis showed good agreement for fluid flow and heat transfer between parallel plates (foil-type), and involute geometries. Sage modeling showed an improved efficiency of 6-9%, the base line efficiency is 42.2% while that of the modified test engine with the new regenerator and 6% improvement is 44.8%. The Sage modeling indicates that even better efficiencies can be achieved if a space-power converter would be designed from the ground up to employ a microfabricated regenerator. In addition to the improved efficiency our structural analysis for the new microfabricated regenerator indicates a higher reliability and an increased potential for long-life high performance compared to the random-fiber regenerator.
AB - In this paper we provide a summary of accomplishments on phase I, and the early part of phase II, of our NASA regenerator microfabrication contract. We developed a microscale regenerator design based on state of the art analytical and computational tools. For this design we projected 6-9% efficiency improvement for the microfabricated regenerator. We were able to identify a manufacturing process and selected a vendor. This vendor completed EDM tools for fabricating the regenerator. The tool met specifications and they are ready to begin producing regenerators. We designed a Large Scale Mock-Up (LSMU) and began its fabrication. CFD modeling for fluid flow and heat transfer (both steady and oscillatory flow conditions) is proceeding for different geometries to assess: the effects of surface roughness, geometries such as a lenticular array, aligned parallel plates (equally and non-equally spaced), staggered parallel plates (equally and non-equally spaced), 3-D involute, and the LSMU model. Also, we examined adapting a test engine to incorporate the new microfabricated regenerator. The Sage code was used in this modeling exercise to compare computed results between the baseline random-fiber regenerator and the microfabricated regenerator. Sage modeled this new regenerator (the involute-element) as a simple foil-type regenerator. 3-D CFD analysis showed good agreement for fluid flow and heat transfer between parallel plates (foil-type), and involute geometries. Sage modeling showed an improved efficiency of 6-9%, the base line efficiency is 42.2% while that of the modified test engine with the new regenerator and 6% improvement is 44.8%. The Sage modeling indicates that even better efficiencies can be achieved if a space-power converter would be designed from the ground up to employ a microfabricated regenerator. In addition to the improved efficiency our structural analysis for the new microfabricated regenerator indicates a higher reliability and an increased potential for long-life high performance compared to the random-fiber regenerator.
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U2 - 10.2514/6.2005-5597
DO - 10.2514/6.2005-5597
M3 - Conference contribution
AN - SCOPUS:29144515696
SN - 1563477343
SN - 9781563477348
T3 - Collection of Technical Papers - 3rd International Energy Conversion Engineering Conference
SP - 830
EP - 845
BT - Collection of Technical Papers - 3rd International Energy Conversion Engineering Conference
PB - American Institute of Aeronautics and Astronautics Inc.
T2 - 3rd International Energy Conversion Engineering Conference
Y2 - 15 August 2005 through 18 August 2005
ER -