CPC F02C 7/12 (2013.01) [F02C 7/06 (2013.01); F05D 2240/50 (2013.01); F05D 2260/20 (2013.01)] | 19 Claims |
1. A thermal management system of a gas turbine engine, the thermal management system comprising:
a thermal transport bus configured to have a heat exchange fluid flowing therethrough and comprising a pump comprising a plurality of bearings;
an auxiliary thermal bus in thermal communication with the plurality of bearings; and
an auxiliary heat exchanger in thermal communication with the auxiliary thermal bus.
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