| CPC F02C 7/06 (2013.01) [F01M 5/002 (2013.01); F02C 7/14 (2013.01); F05D 2220/32 (2013.01); F05D 2260/213 (2013.01); F05D 2260/98 (2013.01)] | 18 Claims |
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1. An apparatus for a gas turbine engine, comprising:
a lubricant reservoir comprising an internal cavity for storing lubricant;
a heat exchanger including a heat exchange conduit and a compressed air passage, the heat exchange conduit arranged in the internal cavity, and the compressed air passage extending longitudinally through the heat exchange conduit;
a lubricant circuit fluidly coupled with the internal cavity; and
a compressed air circuit fluidly coupled with the compressed air passage;
wherein the lubricant reservoir includes a reservoir wall and an access panel, the access panel covers a port through the reservoir wall to the internal cavity, and the heat exchanger is connected to the access panel.
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