Cooling system for power cables in a gas turbine engine
A cooling system for a plurality of conductive cables in a gas turbine engine includes a cooling source and an electric motor disposed in a tail cone. The cooling source may comprise an electric fan or an oil pump. The cooling source may be configured for active cooling of the plurality of conductive cables. The electric fan may be in fluid communication with ambient air during operation of the gas turbine engine.
1. A gas turbine engine with a cooling system, the gas turbine engine comprising:
an electric motor;
a conduit;
a plurality of conductive cables extending from the electric motor;
an external air source in fluid communication with the conduit, the cooling system configured to flow air from the external air source through the conduit to cool the plurality of conductive cables after shutdown of the gas turbine engine;
a pylon and a strut, wherein the strut extends from a tail cone to the pylon, wherein the electric motor is disposed in the tail cone, and wherein the conduit extends through the strut and the pylon to the external air source, wherein the plurality of conductive cables extend from the electric motor through a portion of the conduit and into the pylon aft of a turbine of the gas turbine engine.
2. The gas turbine engine of claim 1 , wherein the cooling system comprises an electric fan.
3. The gas turbine engine of claim 2 , wherein the electric fan is configured to actively cool the plurality of conductive cables.
4. The gas turbine engine of claim 2 , wherein the external air source is in fluid communication with the electric fan.
5. The gas turbine engine of claim 4 , wherein the external air source is disposed radially outward from a bypass airflow path of the gas turbine engine.
6. The gas turbine engine of claim 1 , further comprising:
a processor; and
a non-transitory computer readable storage medium in electronic communication with the processor, the non-transitory computer readable storage medium having instructions stored thereon that, in response to execution by the processor cause the processor to perform operations comprising:
detecting, by the processor, a shutdown of the gas turbine engine;
activating, by the processor, the cooling system; and
in response to the activating the cooling system, pulling the air from the external air source through the conduit having the plurality of conductive cables disposed therein.
7. The gas turbine engine of claim 6 , wherein the cooling system includes an electric fan, and wherein activating further comprises increasing a speed of the electric fan.
8. The gas turbine engine of claim 6 , wherein the cooling system includes an electric fan, and wherein the operations further comprise opening, by the processor, a vent in fluid communication with the external air source.
9. The gas turbine engine of claim 6 , wherein the cooling system includes an electric fan, wherein the plurality of conductive cables are disposed at least partially in the conduit, and wherein the conduit is in fluid communication with the electric fan.