Heat transfer device with nested layers of helical fluid channels

Patent metadata

Field	Value
Publication number	US-11927402-B2
Application number	US-202117374860-A
Country	US
Kind code	B2
Filing date	Jul 13, 2021
Priority date	Jul 13, 2021
Publication date	Mar 12, 2024
Grant date	Mar 12, 2024

Abstract

Systems, apparatuses, and methods relating to heat transfer devices having nested layers of helical fluid channels. In some examples, a device for transferring heat includes a set of nested tubular walls and a plurality of helical walls intersecting each of the nested tubular walls to form one or more first channel layers nested with one or more second channel layers. Each of the first and second channel layers includes a plurality of helical fluid channels. A first intake and a first outtake are in fluid communication with one another via the plurality of helical fluid channels of each first channel layer, for flow of a first fluid through the device. A second intake and a second outtake are in fluid communication with one another via the plurality of helical fluid channels of each second channel layer, for flow of a second fluid through the device.

First claim

What is claimed is:

1. A device for transferring heat between a first fluid and a second fluid, the device comprising:
a set of nested tubular walls;
a plurality of helical walls intersecting each of the nested tubular walls to form one or more first channel layers nested with one or more second channel layers, each first channel layer and each second channel layer including a plurality of helical fluid channels;
a first intake and a first outtake in fluid communication with one another via the plurality of helical fluid channels of each first channel layer, for flow of the first fluid through the device from the first intake to the first outtake; and
a second intake and a second outtake in fluid communication with one another via the plurality of helical fluid channels of each second channel layer, for flow of the second fluid through the device from the second intake to the second outtake, wherein each of the plurality of helical walls extends radially outward, linearly, in a plane including a central axis of the device.

2. The device of claim 1 , wherein each helical fluid channel of the plurality of helical fluid channels of at least one first channel layer and at least one second channel layer has a pair of channel walls spaced radially from one another and formed by a pair of nested tubular walls of the set of nested tubular walls.

3. The device of claim 1 , wherein the one or more first channel layers and the one or more second channel layers are arranged in a radial series of at least two first channel layers alternating with at least two second channel layers.

4. The device of claim 1 , wherein at least one of the first intake and the second intake includes one or more flow-steering vanes configured to encourage swirling flow of fluid passing through the at least one of the first intake and the second intake.

5. The device of claim 1 , further comprising a first inflow manifold providing fluid communication between the first intake and each helical fluid channel of the plurality of helical fluid channels of each first channel layer, the first inflow manifold including a plenum and a distribution channel extending from the plenum, the plenum being in direct fluid communication with only a subset of the plurality of helical fluid channels of a first channel layer of the one or more first channel layers, the distribution channel providing fluid communication between the plenum and another subset of the plurality of helical fluid channels of the first channel layer of the one or more first channel layers.

6. The device of claim 5 , further comprising:
a second outflow manifold located adjacent the first inflow manifold and including a plenum, the second outflow manifold providing fluid communication between each helical fluid channel of the plurality of helical fluid channels of each second channel layer and the second outtake; and
an end cap located at an inlet end of the first channel layer of the one or more first channel layers, the end cap forming a wall of the distribution channel of the first inflow manifold and separating the plenum of the second outflow manifold from the distribution channel of the first inflow manifold.

7. The device of claim 6 , wherein the end cap is domed.

8. The device of claim 1 , wherein the set of nested tubular walls defines a central axis, and wherein the first intake, the first outtake, the second intake, and the second outtake define respective axes that are parallel to the central axis.

9. The device of claim 1 , wherein each helical wall of the plurality of helical walls provides a load path extending radially and continuously from an outermost tubular wall to an innermost tubular wall of the set of nested tubular walls.

10. The device of claim 1 , further comprising a flange projecting from a helical wall of the plurality of helical walls, or from a nested tubular wall of the set of nested tubular walls, and into a lumen of a helical fluid channel of the plurality of helical fluid channels of a first channel layer or a second channel layer.

11. The device of claim 1 , wherein the plurality of helical fluid channels of a first channel layer of the one or more first channel layers includes a pair of adjacent helical fluid channels having a pair of channel inlets and a pair of channel outlets, and wherein one of the helical walls defines an opening that provides fluid communication between the pair of adjacent helical fluid channels at a position intermediate the pair of channel inlets and the pair of channel outlets.

12. The device of claim 1 , wherein each helical wall tapers in thickness toward the central axis of the device.

13. An aerospace vehicle comprising:
a vehicle body;
an engine connected to the vehicle body and configured to power the vehicle body in a flight mode; and
a heat transfer device connected to the vehicle body and/or the engine and including
a set of nested tubular walls,
a plurality of helical walls intersecting each of the nested tubular walls to form one or more first channel layers nested with one or more second channel layers, each first channel layer and each second channel layer including a plurality of helical fluid channels,
a first intake and a first outtake in fluid communication with one another via the helical fluid channels of each first channel layer, for flow of a first fluid through the heat transfer device from the first intake to the first outtake, and
a second intake and a second outtake in fluid communication with one another via the plurality of helical fluid channels of each second channel layer, for flow of a second fluid through the heat transfer device from the second intake to the second outtake, wherein each of the plurality of helical walls extends radially outward, linearly, in a plane including a central axis of the device.

14. The aerospace vehicle of claim 13 , wherein the heat transfer device is configured to cool intake air for the engine.

15. The aerospace vehicle of claim 13 , wherein one of the first and second fluids is supercritical carbon dioxide.

16. The aerospace vehicle of claim 15 , wherein the heat transfer device is configured to heat the supercritical carbon dioxide for use as a working fluid in a thermodynamic cycle that converts heat to another form of energy.

17. The aerospace vehicle of claim 13 , wherein the heat transfer device is in fluid communication with a turbine.

18. A device for transferring heat between a first fluid and a second fluid, the device comprising:
a set of nested tubular walls;
a plurality of helical walls intersecting each of the nested tubular walls to form one or more first channel layers nested with one or more second channel layers, each first channel layer and each second channel layer including a plurality of helical fluid channels, wherein each helical fluid channel has a rectangular cross sectional shape;
a first intake and a first outtake in fluid communication with one another via the plurality of helical fluid channels of each first channel layer, for flow of the first fluid through the device from the first intake to the first outtake; and
a second intake and a second outtake in fluid communication with one another via the plurality of helical fluid channels of each second channel layer, for flow of the second fluid through the device from the second intake to the second outtake
wherein the first intake and the first outtake are on opposite sides of the device along a central axis of the device, and the second intake and the second outtake are on opposite sides of the device along the central axis.

Assignees

• Boeing Co

Inventors

• Van Affelen Douglas H
• Muley Arun
• Stoia Michael F

Classifications

• F28D7/022 Primary

  the conduits of two or more media in heat-exchange relationship being helically coiled, the coils having a cylindrical configuration · CPC title

• B64D33/02

  of combustion air intakes · CPC title

• F02C7/141

  of working fluid · CPC title

• F28F13/12

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

• B64D2033/024

  comprising cooling means · CPC title