Entwined tubular arrangements for heat exchangers and counterflow heat transfer systems

Patent metadata

Field	Value
Publication number	US-11897015-B2
Application number	US-202117459078-A
Country	US
Kind code	B2
Filing date	Aug 27, 2021
Priority date	May 25, 2017
Publication date	Feb 13, 2024
Grant date	Feb 13, 2024

Abstract

A counterflow heat transfer system comprises a heat exchanger and a flow controller arranged to convey a first fluid through the heat exchanger in a first flow direction and a second fluid through the heat exchanger in a second counterflow direction. The heat exchanger comprises at least one first thermally conductive tube conveying the first fluid and at least one second thermally conductive tube conveying the second fluid. The first and second tubes are wound around one another and in contact with one another in an entwined tubular arrangement.

First claim

The invention claimed is:

1. An additive manufacturing method of making an entwined tubular arrangement for a heat exchanger, comprising:
using an additive manufacturing technique to build up one or more thermally conductive materials layer-by-layer from a Computer-Aided Design (CAD) model;
building a support structure and the entwined tubular arrangement out of the one or more thermally conductive materials, wherein the entwined tubular arrangement comprises first and second tubes wound around one another and in contact with one another; and
retaining the support structure after the entwined tubular arrangement has been built;
wherein the support structure comprises a lattice support structure, the lattice support structure at least partially filled with a thermally insulative material.

2. The method of claim 1 , wherein the support structure and the entwined tubular arrangement are made of a same thermally conductive material.

3. The method of claim 1 , wherein building the entwined tubular arrangement comprises placing a thermally conductive filler material between the first and second tubes where they are in contact with each other.

4. The method of claim 1 , wherein the thermally conductive filler material is made of the same thermally conductive material as the first and/or second tubes.

5. The method of claim 1 , wherein building the entwined tubular arrangement comprises forming fins on an inside or outside surface of the first and/or second tubes.

6. The method of claim 1 , wherein the first and second tubes are helically wound around a common axis in contact with one another in the entwined tubular arrangement.

7. The method of claim 1 , wherein the first and second tubes have different diameters.

8. The method of claim 1 , wherein one or more of the first and second tubes comprises a non-circular cross-section.

9. The method of claim 1 , wherein one or more of the first and second tubes comprises a flattened or concave surface area where the first and second tubes are in contact with one another.

10. The method of claim 1 , wherein the additive manufacturing technique is one of: powder bed fusion (PBF), Selective Laser Melting (SLM), Selective Laser Melting (SLM), Direct Metal Laser Sintering (DMLS), Selective Laser Sintering (SLS), and electron beam melting (EBM) processes.

Assignees

• Hs Marston Aerospace Ltd

Inventors

• Phillips Paul
• Pollard Berwyn

Classifications

• B21D11/06 Primary

  Bending into helical or spiral form; Forming a succession of return bends, e.g. serpentine form (making helically seamed tubing B21C37/12) · CPC title

• B21D53/06

  of metal tubes · CPC title

• B23P15/26

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

• F28D7/0016 Primary

  the conduits for one medium or the conduits for both media being bent (F28D7/0033 takes precedence) · CPC title

• F28D7/026

  the conduits of only one medium being helically coiled and formed by bent members, e.g. plates, the coils having a cylindrical configuration · CPC title