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NASA NTRS · 20180008610

Advanced Manifolds for Improved Solid Oxide Electrolyzer Performance

Abstract

An investigation was conducted to see if additive manufacturing could be used to fabricate more efficient manifold designs for improved flow, reduced stresses, and decreased number of joints to be sealed for a solid oxide electrolyzer used to convert carbon dioxide to oxygen. Computational flow and mechanical modeling were conducted on a NASA Glenn Research Center patented cell and stack design with the potential to achieve a 3-4 times mass reduction. Various manifold designs were modeled, and two were downselected to be fabricated and tested. Some benefit was seen in a baffled manifold design, which directed incoming flow more effectively into the flow channels, compared to the original design, where the flow spent more time within the manifold itself. Flow measurements indicated some non-uniformity of flow across the channels at higher flow rates, which were not predicted by the model. Some possible explanations for the differences are discussed.

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BibTeXRIS

Linne, Diane L., Kuczmarski, Maria A., Johnston, James C., Farmer, Serence C., Green, Robert D., Mital, Subodh K., Setlock, John A.. 2018-09-17. Advanced Manifolds for Improved Solid Oxide Electrolyzer Performance. https://ntrs.nasa.gov/citations/20180008610

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