Systems and methods for driving an oil cooling fan of a gas turbine engine
Systems and methods for driving an oil cooling fan ( 36 ) of a gas turbine engine ( 10 ) during different modes of operation of the gas turbine engine ( 10 ) are described. A system may include a coupling device ( 40 ) configured to: transmit motive power from a power turbine shaft ( 22 ) of the gas turbine engine ( 10 ) to the oil cooling fan ( 36 ) during a first mode of operation where the power turbine shaft ( 22 ) is turning, and to decouple the oil cooling fan ( 36 ) from the power turbine shaft ( 22 ) during a second mode of operation where the power turbine shaft ( 22 ) is prevented from turning. An alternate source ( 42 ) of motive power may be configured to drive the oil cooling fan ( 36 ) during the second mode of operation.
1. A system for driving an oil cooling fan of a gas turbine engine, the system comprising:
a coupling device configured to:
transmit motive power from a power turbine shaft driven by a low pressure turbine of the gas turbine engine to the oil cooling fan during a first mode of operation where the power turbine shaft is turning, and to
decouple the oil cooling fan from the power turbine shaft during a second mode of operation where the power turbine shaft is prevented from turning; and
an alternate source of motive power configured to drive the oil cooling fan during the second mode of operation, the alternate source of motive power including a high pressure turbine of the gas turbine engine.
2. The system as defined in claim 1 , wherein engine is an aircraft-mounted engine.
3. The system as defined in claim 1 , wherein the alternate source of motive power includes an electric motor.
4. The system as defined in claim 3 , wherein the electric motor is driven by a source of electricity powered by the high pressure turbine of the gas turbine engine.
5. The system as defined in claim 1 , wherein an output of the alternate source of motive power is configured to be modulated based on a cooling load on an oil cooler of the gas turbine engine.
6. The system as defined in claim 1 , wherein the alternate source of motive power is configured to vary the speed of the oil cooling fan based on a cooling load on an oil cooler of the gas turbine engine.
7. A gas turbine engine comprising:
a low pressure turbine coupled to a power turbine shaft;
an oil cooler including an oil cooling fan;
a coupling device configured to:
transmit motive power from the power turbine shaft of the gas turbine engine to the oil cooling fan during a first mode of operation where the power turbine shaft is turning, and to
decouple the oil cooling fan from the power turbine shaft during a second mode of operation where the power turbine shaft is prevented from turning; and
an alternate source of motive power configured to drive the oil cooling fan during the second mode of operation, the alternate source of motive power including a high pressure turbine of the gas turbine engine.
8. The gas turbine engine as defined in claim 7 , wherein engine is an aircraft-mounted engine.
9. The gas turbine engine as defined in claim 7 , wherein the alternate source of motive power includes an electric motor.
10. The gas turbine engine as defined in claim 9 , wherein the electric motor is driven by a source of electricity powered by the high pressure turbine of the gas turbine engine.
11. The gas turbine engine as defined in claim 9 , wherein the electric motor is configured to vary the speed of the oil cooling fan based on a cooling load on the oil cooler.
12. The gas turbine engine as defined in claim 7 , wherein an output of the alternate source of motive power is configured to be modulated based on a cooling load on the oil cooler.
13. A method for driving an oil cooling fan of an oil cooler of a gas turbine engine, the method comprising:
driving the oil cooling fan using motive power extracted from a power turbine shaft driven by a low pressure turbine of the gas turbine engine during a first mode of operation where the power turbine shaft is turning; and
driving the oil cooling fan using motive power from an alternate source during a second mode of operation where the power turbine shaft is prevented from turning, the alternate source of motive power including a high pressure turbine of the gas turbine engine.
14. The method as defined in claim 13 , wherein the alternate source comprises an electric motor.
15. The method as defined in claim 14 , comprising driving the electric motor using power extracted from the high pressure turbine of the gas turbine engine.
16. The method as defined in claim 13 , comprising modulating an output of the alternate source based on a cooling load on the oil cooler.
17. The method as defined in claim 13 , wherein the second mode of operation comprises a hotel mode where the power turbine shaft is locked.