ENGINE LUBRICATION SYSTEM USING DE-OXYGENATED FUEL
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United States of America Patent
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Mar 2, 2017
app pub date -
Apr 27, 2016
filing date -
May 21, 2015
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Abstract
A thermal management system for a gas turbine engine comprises a plurality of first heat generating sub-systems arranged in operable communication with the engine, a fuel supply sub-system, a fuel circulation sub-system, and one or more combustors. The fuel supply sub-system is adapted to supply a de-oxygenated fuel to the fuel circulation sub-system, and the fuel circulation sub-system is adapted to circulate the de-oxygenated fuel to lubricate and cool each of the plurality of first heat generating sub-systems, and then to combust the de-oxygenated fuel in the or each combustor.
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