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Please use this identifier to cite or link to this item: https://dspace.lboro.ac.uk/2134/13994

Title: Testing microtubular SOFCs in unmanned air vehicles (UAVs)
Authors: Meadowcroft, Antony D.
Howroyd, Simon R.
Kendall, Kevin
Kendall, Michaela
Issue Date: 2013
Publisher: © ECS - The Electrochemical Society
Citation: MEADOWCROFT, A.D. ... et al., 2013. Testing Micro-Tubular SOFCs in Unmanned Air Vehicles (UAVs). ECS Transactions, 57, (1), pp. 451-457.
Abstract: Unmanned Air Vehicles (UAVs) powered by microtubular SOFCs (mSOFCs) are described for comparison with polymer fuel cells (PEFCs). Using propane as fuel, 7mm diameter mSOFCs have been tested in a 2m wingspan aircraft with a total weight of 6kg. The start-up time was 12 minutes to deliver 250W in a fuel cell/battery hybrid drive system. Tubes were YSZ cermet anode supported, with 10 µm YSZ electrolyte, 6µm SDC interlayer coated with 50µm LSCF cathode. Silver wires were used as interconnects. Pure propane fuel gas was mixed with air in a CPOX reactor using catalytic fuel processing mesh. A polymeric fuel inlet manifold gave cold sealing at the tube inlet ends which projected out of the hot box. Cathode air was provided in counterflow, preheated over an anode off-gas catalyst. The fuel utilization was 55%, output power of 250W. The fuel cell was incorporated in a hybrid electrical system with lithium polymer battery and inserted in a Skywalker X8 UAV with 500g of propane in an aluminum tank.
Description: This article was published in the journal, ECS Transactions [© ECS - The Electrochemical Society].
Version: Published
DOI: 10.1149/05701.0451ecst
URI: https://dspace.lboro.ac.uk/2134/13994
Publisher Link: http://dx.doi.org/10.1149/05701.0451ecst
ISSN: 1938-5862
Appears in Collections:Published Articles (Aeronautical and Automotive Engineering)

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