Additive manufactured ducted heat exchanger system with additively manufactured fairing

Patent metadata

Field	Value
Publication number	US-10450956-B2
Application number	US-201514887430-A
Country	US
Kind code	B2
Filing date	Oct 20, 2015
Priority date	Oct 21, 2014
Publication date	Oct 22, 2019
Grant date	Oct 22, 2019

Abstract

A ducted heat exchanger system for a gas turbine engine includes an additive manufactured heat exchanger core with a contoured external and/or internal geometry. A method of additively manufacturing a heat exchanger for a gas turbine engine includes additively manufacturing a core of a heat exchanger to set a ratio of local surface area to flow area to control a pressure drop per unit length along the core.

First claim

The invention claimed is:

1. A ducted heat exchanger system for a gas turbine engine, comprising:
a duct within the gas turbine engine; and
a heat exchanger core within the duct;
wherein said duct includes a fairing upstream or downstream of the heat exchanger core, the fairing having an interior surface configured so that airflow is communicated over the interior surface and into the heat exchanger core within the duct, a portion of said interior surface comprising an additively manufactured surface exposed to the airflow, wherein the additively manufactured surface is manufactured of a material that facilitates heat transfer and includes a surface pattern to facilitate heat transfer as well as airflow control.

2. The ducted heat exchanger system as recited in claim 1 , wherein said additively manufactured surface is flush with the interior surface of said fairing.

3. The ducted heat exchanger system as recited in claim 2 , wherein said additively manufactured surface is at least partially arcuate.

4. The ducted heat exchanger system as recited in claim 1 , wherein said additively manufactured surface extends from said heat exchanger core.

5. The ducted heat exchanger system as recited in claim 1 , wherein said additively manufactured surface is an extension of a frame that at least partially supports said heat exchanger core.

6. The ducted heat exchanger system as recited in claim 1 , wherein said additively manufactured surface is an extension of a mount arrangement for said heat exchanger core.

7. The ducted heat exchanger system as recited in claim 1 , wherein said heat exchanger core is additively manufactured, at least one of a front face, a rear face, an upper surface, and a lower surface of said heat exchanger core is non-planar.

8. The ducted heat exchanger system as recited in claim 1 , wherein a front face of said heat exchanger core is non-planar and said core is at least partially arcuate.

9. The ducted heat exchanger system as recited in claim 8 , wherein said front face of said heat exchanger core is contoured such that the airflow enters said front face over an entirety of said front face.

10. The ducted heat exchanger as recited in claim 9 , wherein said front face of said core extends into an inlet diffusion area of the duct within which said heat exchanger core is located.

11. The ducted heat exchanger system as recited in claim 8 , wherein said front face of said core is contoured.

12. The ducted heat exchanger system as recited in claim 1 , wherein a rear face of said core is non-planar.

13. The ducted heat exchanger system as recited in claim 12 , wherein said rear face of said core is contoured such that said airflow exits said rear face over an entirety of said rear face.

14. The ducted heat exchanger system as recited in claim 13 , wherein said rear face of said core extends into an exit contraction area of the duct within which said core is located.

15. The ducted heat exchanger system as recited in claim 1 , wherein said surface patterns comprise chevrons.

16. The ducted heat exchanger system as recited in claim 1 , wherein said surface patterns comprise dimples.

17. A method of manufacturing a fairing for a ducted heat exchanger system according to claim 1 comprising:
additively manufacturing the fairing to provide the additively manufactured surface of the fairing.

18. The method as recited in claim 17 , wherein the additively manufactured surface operates as a heat exchanger.

19. A ducted heat exchanger system for a gas turbine engine, comprising:
a duct within the gas turbine engine;
a heat exchanger core within the duct;
an additively manufactured inlet fairing of the duct upstream of said heat exchanger core, the additively manufactured inlet fairing comprising an interior surface configured such that airflow is communicated over the interior surface, through the duct and into the heat exchanger core; wherein a portion of the interior surface comprises an additively manufactured surface that is exposed to the airflow, is manufactured of a material that facilitates heat transfer, and includes a surface pattern to facilitate heat transfer as well as airflow control; and
an additively manufactured exit fairing of the duct downstream of said heat exchanger core, said additively manufactured exit fairing comprising an interior surface configured such that the airflow is communicated from the heat exchanger core, through the duct and over the interior surface of the exit fairing; wherein a portion of the interior surface comprises an additively manufactured surface that is exposed to the airflow, is manufactured of a material that facilitates heat transfer, and includes a surface pattern to facilitate heat transfer as well as airflow control.

20. The ducted heat exchanger system as recited in claim 19 , wherein an external geometry of said heat exchanger core is non-planar.

21. The ducted heat exchanger system as recited in claim 19 , wherein at least one of a front face, a rear face, an upper surface, and a lower surface of said heat exchanger core is non-planar.

22. The ducted heat exchanger system as recited in claim 19 , wherein a front face, a rear face, an upper surface, and a lower surface of said heat exchanger core is non-planar.

23. The ducted heat exchanger system as recited in claim 19 , wherein a front face of said heat exchanger core is non-planar and is contoured and wherein said inlet fairing comprises a diffusion area.

24. The ducted heat exchanger system as recited in claim 19 , wherein a rear face of said heat exchanger core is non-planar and is contoured and wherein said exit fairing comprises a contraction area.

25. The ducted heat exchanger system as recited in claim 19 , wherein a front face of said heat exchanger core is contoured such that the airflow enters said heat exchanger core over an entirety of said front face.

Assignees

• United Technologies Corp

Inventors

• Schmitz John T

Classifications

• F28F7/02

  Blocks traversed by passages for heat-exchange media {(F28D7/0008 takes precedence)} · CPC title

• F02C7/10 Primary

  by means of regenerative heat-exchangers · CPC title

• F28F13/08

  by varying the cross-section of the flow channels · CPC title

• F28F2255/00

  Heat exchanger elements made of materials having special features or resulting from particular manufacturing processes · CPC title

• F05D2230/53

  by integrally manufacturing a component, e.g. by milling from a billet or one piece construction · CPC title