Gas turbine engine thermal management system
A thermal management system for a gas turbine engine includes a first heat exchanger that provides a first conditioned fluid, a second heat exchanger in series flow communication with the first heat exchanger and that exchanges heat with the first conditioned fluid to provide a second conditioned fluid, and a third heat exchanger in parallel flow communication with the second heat exchanger and that selectively exchanges heat with the first conditioned fluid to provide a third conditioned fluid. The second conditioned fluid and the third conditioned fluid combine to provide a mixed conditioned fluid. A first portion of the mixed conditioned fluid including a first temperature is communicated to a first engine system. A second portion of the mixed conditioned fluid including a second temperature is communicated to a second engine system. The second temperature includes a greater temperature than the first temperature.
1. A thermal management system comprising:
a first fluid circuit including a first heat exchanger, a second heat exchanger, and a third heat exchanger, the first fluid circuit is configured so that:
a first conditioned fluid exits the first heat exchanger;
a first portion of the first conditioned fluid enters the second heat exchanger;
a second portion of the first conditioned fluid enters the third heat exchanger;
fluid exiting the second and third heat exchangers combine to form a first mixed fluid, a first portion of which enters a first engine system of a gas turbine engine; and
a second portion of the first mixed fluid and a third portion of the first conditioned fluid enter a second engine system of the gas turbine engine.
2. The system as recited in claim 1 , wherein said first heat exchanger and said third heat exchanger are air/oil heat exchangers and said second heat exchanger is a fuel/oil heat exchanger.
3. The system as recited in claim 1 , comprising a valve that selectively modulates to split said first conditioned fluid into said first portion and said second portion.
4. The system as recited in claim 3 , comprising a sensor that communicates with a controller to selectively control a position of said valve.
5. The system as recited in claim 4 , wherein said controller modulates said valve to communicate said second portion of said first conditioned fluid to said third heat exchanger in response to said sensor sensing that a predefined threshold has been exceeded.
6. The system as recited in claim 1 , wherein said second heat exchanger is also incorporated into a second fluid circuit of the thermal management system.
7. An engine comprising the thermal management system as recited in claim 1 , wherein said first engine system includes a portion of a geared architecture of said gas turbine engine.
8. An engine comprising the thermal management system as recited in claim 1 , wherein said second engine system includes at least one of an engine bearing compartment, an engine gearbox and a drive mechanism of a geared architecture of the gas turbine engine.
9. The system as recited in claim 1 , wherein said first conditioned fluid first mixed fluid are oil.
10. The system as recited in claim 1 , comprising a fluid tank that communicates a fluid to an inlet of said first heat exchanger.
11. The system as recited in claim 10 , comprising a filter between said fluid tank and said first heat exchanger.
12. The system as recited in claim 10 , comprising a trim passage between said fluid tank and said first heat exchanger for returning a portion of said fluid to said fluid tank prior to entering said inlet of said first heat exchanger.
13. The system as recited in claim 1 , wherein a conditioned second fluid from said second heat exchanger is communicated to a combustor of the gas turbine engine.
14. The system as recited in claim 13 , wherein said conditioned second fluid is fuel and said fluid exiting said second heat exchanger is oil.
15. The system as recited in claim 1 , wherein said first heat exchanger and said second heat exchanger are continuously operated and said third heat exchanger is only selectively operated.
16. An engine comprising the thermal management system as recited in claim 1 , wherein said first engine system is a first portion of a geared architecture of a fan section of said gas turbine engine and said second engine system is a second, different portion of said geared architecture.