| CPC F16C 33/6685 (2013.01) [F01M 11/0004 (2013.01); F02C 7/06 (2013.01); F01M 2011/0091 (2013.01); F16C 2360/23 (2013.01)] | 19 Claims |

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1. A method to reduce heat load in a gas turbine engine, the method comprising:
applying an oleophobic coating to an internal wall of a sump, the sump located in proximity to a heat generating element of the gas turbine engine; and
applying an oleophilic coating to the heat generating element of the gas turbine engine.
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