Heat exchanger

Patent metadata

Field	Value
Publication number	US-11029102-B2
Application number	US-201815867929-A
Country	US
Kind code	B2
Filing date	Jan 11, 2018
Priority date	Jan 13, 2017
Publication date	Jun 8, 2021
Grant date	Jun 8, 2021

Abstract

A heat exchanger includes a conduit, a header, and a swirler been formed as a unitary piece by additive manufacturing. The swirler is disposed within the conduit and the header and is arranged to disperse a flow from an inlet flow path a heat exchanger matrix. The swirler extends a only portion of the length of the header between the conduit and the heat exchanger matrix and thereby provides space within the header for fluid to diffuse before entering the heat exchanger matrix.

First claim

The invention claimed is:

1. A heat exchanger comprising:
a conduit defining an inlet flow path for a fluid;
a header disposed to receive a flow from the inlet flow path;
a heat exchanger matrix disposed to receive a flow from the header; and
a swirler disposed within the conduit and the header, wherein the swirler is arranged to disperse a flow from the inlet flow path over the heat exchanger matrix, and wherein the swirler extends over only a portion of the length of the header between the conduit and the heat exchanger matrix and thereby provides space within the header for fluid to diffuse before entering the heat exchanger matrix;
wherein the conduit, header, and swirler have been formed as a unitary piece by additive manufacturing; and
wherein the portion of the swirler in the header extends across the entire width of the heat exchanger matrix in two dimensions, and extends across the entire width of the header in two dimensions and joins integrally with opposing walls of the header, and is thereby arranged to provide structural support to the header during use and during formation of the header by additive manufacturing.

2. A heat exchanger as claimed in claim 1 , wherein the swirler divides the header into a plurality of equal volumes.

3. A heat exchanger as claimed in claim 1 , wherein the swirler comprises a plurality of curved blades arranged to direct a flow of fluid through the inlet flow path and the header.

4. A heat exchanger as claimed in claim 3 , wherein the blades are smooth between the conduit and the header.

5. A heat exchanger as claimed in claim 3 , wherein the swirler blades curve through 90 degrees along their entire length.

6. A heat exchanger as claimed in claim 1 , wherein the swirler is arranged to complement the shape of a cross section of the heat exchanger matrix.

7. An aircraft comprising a heat exchanger as claimed in claim 1 .

Assignees

• Hs Marston Aerospace Ltd

Inventors

• Basini Neil

Classifications

• F28F9/0268 Primary

  in the form of multiple deflectors for channeling the heat exchange medium · CPC title

• F28F9/028

  by using inserts for modifying the pattern of flow inside the header box, e.g. by using flow restrictors or permeable bodies or blocks with channels · CPC title

• F28F9/0246

  Arrangements for connecting header boxes with flow lines · CPC title

• F28F13/12 Primary

  by creating turbulence, e.g. by stirring, by increasing the force of circulation (F28F13/08 takes precedence) · CPC title

• F28F1/00

  Tubular elements; Assemblies of tubular elements (specially adapted for movement F28F5/00) · CPC title