Heat exchanger system with spatially varied additively manufactured heat transfer surfaces

Patent metadata

Field	Value
Publication number	US-10907500-B2
Application number	US-201514615753-A
Country	US
Kind code	B2
Filing date	Feb 6, 2015
Priority date	Feb 6, 2015
Publication date	Feb 2, 2021
Grant date	Feb 2, 2021

Abstract

A heat exchanger system includes a plurality of additively manufactured heat transfer surfaces in a plurality of sectors, a first of the plurality of sectors including a first subset of the plurality of the additively manufactured heat transfer surfaces having a characteristic different than a characteristic in a second of the plurality of sectors.

First claim

What is claimed:

1. A heat exchanger system for an engine nacelle of a gas turbine engine, comprising:
an additively manufactured curved heat exchanger that comprises a first of a multiple of heat exchanger core flow passages formed between curved plates, a second of the multiple of heat exchanger core flow passages formed between curved plates radially outboard of the first of the multiple of heat exchanger core flow passages, the cross-sectional area of the second of the multiple of heat exchanger core flow passage defining a larger flow passage cross-sectional area than the cross-sectional area of the first of the multiple of heat exchanger core flow passages to maintain a consistent flow rate through each of the multiple of heat exchanger core flow passages during operation, and wherein the longitudinal axis of the first of the multiple of heat exchanger core flow passages is parallel to the longitudinal axis of the second of the multiple of heat exchanger core flow passages.

2. The heat exchanger system as recited in claim 1 , wherein each of the multiple of heat exchanger core flow passages radially outboard of an adjacent one of the multiple of heat exchanger core flow passages, defines a larger flow passage than the adjacent one of the multiple of heat exchanger core flow passages.

3. The heat exchanger system as recited in claim 1 , further comprising a plurality of additively manufactured heat transfer surfaces in a plurality of sectors within each of the multiple of heat exchanger core flow passages.

4. The heat exchanger system as recited in claim 3 , wherein the heat transfer surfaces are fins.

5. The heat exchanger system as recited in claim 3 , wherein the heat transfer surfaces extend from the curved plates.

6. The heat exchanger system as recited in claim 1 , further comprising a plurality of additively manufactured heat transfer surfaces in a corner sector within each of the multiple of heat exchanger core flow passages.

7. The heat exchanger system as recited in claim 6 , wherein the plurality of additively manufactured heat transfer surfaces have an aspect ratio which is lower than the aspect ratio of a non-corner sector.

8. The heat exchanger system as recited in claim 6 , wherein the plurality of additively manufactured heat transfer surfaces have a fin density which is lower than the fin density of a non-corner sector.

9. The heat exchanger system as recited in claim 1 , wherein the plurality of additively manufactured heat transfer surfaces in the corner sector provide structural support for the curved plates.

10. The heat exchanger system as recited in claim 1 , wherein the additively manufactured curved heat exchanger is located within a duct in the nacelle.

Assignees

• United Technologies Corp
• Raytheon Tech Corp

Inventors

• Wong Eva
• Whiton John H

Classifications

• F28F3/02 Primary

  Elements or assemblies thereof with means for increasing heat-transfer area, e.g. with fins, with recesses, with corrugations (F28F3/08 takes precedence) · CPC title

• F28F3/04

  the means being integral with the element · CPC title

• F28F2215/04

  Assemblies of fins having different features, e.g. with different fin densities · CPC title

• F28D2021/0021

  for aircrafts or cosmonautics · CPC title

• B23P15/26

  heat exchangers {or the like (making heat exchangers by methods covered by other subclasses B21D53/02)} · CPC title