Multi-fluid heat exchanger
A heat exchanger is provided. The heat exchanger includes a first wall manifold. The heat exchanger further includes a second wall manifold spaced apart from the first wall manifold. The heat exchanger further includes a plurality of vanes that extend generally circumferentially between the first wall manifold and the second wall manifold. The heat exchanger further includes a plurality of fluid circuits defined within the heat exchanger. Each fluid circuit in the plurality of fluid circuits includes an inlet channel portion and an outlet channel portion defined within the first wall manifold. A return channel portion defined within the second wall manifold. At least one passage portion of a plurality of passage portions defined within each vane of the plurality of vanes. The at least one passage portion extends between the return channel portion and one of the inlet channel portion and the outlet channel portion.
1. A heat exchanger for use in an aircraft engine, the heat exchanger comprising:
a first wall manifold;
a second wall manifold spaced apart from the first wall manifold;
a plurality of vanes extending generally circumferentially between the first wall manifold and the second wall manifold; and
a plurality of fluid circuits defined within the heat exchanger, each fluid circuit in the plurality of fluid circuits including a first channel portion defined within the first wall manifold, a second channel portion defined within the second wall manifold, and at least one passage portion of a plurality of passage portions defined within each vane of the plurality of vanes, each passage portion of the plurality of passage portions extending between a respective first channel portion and a respective second channel portion.
2. The heat exchanger of claim 1 , wherein both the first channel portion and the second channel portion are separately fluidly coupled to a respective fluid system, the respective fluid system including at least one motive fluid supply and at least one motive fluid return.
3. The heat exchanger of claim 2 , wherein each fluid circuit of the plurality of fluid circuits is independently operable to receive a motive fluid, via one of the first channel portion or the second channel portion, from the at least one motive fluid supply and convey the motive fluid to the at least one motive fluid return, via the other of the first channel portion or the second channel portion.
4. The heat exchanger of claim 1 , wherein the heat exchanger is integrally formed.
5. The heat exchanger of claim 1 , wherein the first wall manifold and the second wall manifold are integrally formed and welded to the plurality of vanes.
6. The heat exchanger of claim 1 , wherein each vane in the plurality of vanes includes a leading edge, a trailing edge, and side walls extending between the leading edge and the trailing edge.
7. The heat exchanger of claim 6 , wherein the plurality of vanes are spaced apart from one another along a radial direction to define airflow passages, and wherein each airflow passage is configured to receive and expel a flow of air in a direction generally perpendicular to the at least one passage portion of each fluid circuit of the plurality of fluid circuits.
8. The heat exchanger of claim 1 , wherein the at least one passage portion of the plurality of passage portions defines a constant width from the first wall manifold to the second wall manifold.
9. The heat exchanger of claim 1 , wherein the at least one passage portion of the plurality of passage portions defines a continuously varying width from the first wall manifold to the second wall manifold.
10. An engine comprising:
a fan section;
a core engine disposed downstream of the fan section;
a core cowl annularly encasing the core engine and at least partially defining a core duct;
a fan cowl disposed radially outward from the core cowl and annularly encasing at least a portion of the core cowl, the fan cowl and core cowl defining in part a fan duct; and
a heat exchanger disposed within a fan duct, wherein the heat exchanger provides for thermal communication between a coolant fluid flowing through the fan duct and at least one motive fluid flowing through the heat exchanger, the heat exchanger comprising:
a first wall manifold;
a second wall manifold spaced apart from the first wall manifold;
a plurality of vanes extending generally circumferentially between the first wall manifold and the second wall manifold; and
a plurality of fluid circuits defined within the heat exchanger, each fluid circuit in the plurality of fluid circuits including a first channel portion defined within the first wall manifold, a second channel portion defined within the second wall manifold, and at least one passage portion of a plurality of passage portions defined within each vane of the plurality of vanes, each passage portion of the plurality of passage portions extending between a respective first channel portion and a respective second channel portion.
11. The engine of claim 10 , wherein both the first channel portion and the second channel portion are separately fluidly coupled to a respective fluid system, the respective fluid system including at least one motive fluid supply and at least one motive fluid return.
12. The engine of claim 11 , wherein each fluid circuit of the plurality of fluid circuits is independently operable to receive a motive fluid, via one of the first channel portion or the second channel portion, from the at least one motive fluid supply and convey the motive fluid to the at least one motive fluid return, via the other of the first channel portion or the second channel portion.
13. The engine of claim 10 , wherein the heat exchanger is integrally formed.
14. The engine of claim 10 , wherein the first wall manifold and the second wall manifold are integrally formed and welded to the plurality of vanes.
15. The engine of claim 10 , wherein each vane in the plurality of vanes includes a leading edge, a trailing edge, and side walls extending between the leading edge and the trailing edge.
16. The engine of claim 15 , wherein the plurality of vanes are spaced apart from one another along a radial direction to define airflow passages, and wherein each airflow passage is configured to receive and expel a flow of air in a direction generally perpendicular to the at least one passage portion of each fluid circuit of the plurality of fluid circuits.
17. The engine of claim 10 , wherein the at least one passage portion of the plurality of passage portions defines a constant width from the first wall manifold to the second wall manifold.
18. The engine of claim 10 , wherein the at least one passage portion of the plurality of passage portions defines a continuously varying width from the first wall manifold to the second wall manifold.
19. The engine of claim 10 , wherein the fan section comprises an unducted fan.
20. The engine of claim 10 , further comprising an outer nacelle surrounding a fan of the fan section.