HEAT EXCHANGER
20180172361 ยท 2018-06-21
Inventors
Cpc classification
F28F2250/10
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F28D7/10
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F28F1/36
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F28F1/003
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F28F1/32
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F28F1/40
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F28F2250/08
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F28D7/0008
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
International classification
F28F1/32
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Abstract
A heat exchanger comprises a conduit with an interior surface which defines a first flow passage. A first plurality of fins project inwardly from the interior surface of the conduit. The first plurality of fins are angled relative to a longitudinal axis (X) of the conduit so as to form helical flowpaths for fluid flowing through the first flow passage. A second flow passage disposed outwardly of the interior surface and radially outwardly of the first plurality of fins.
Claims
1. A heat exchanger comprising: a conduit with an interior surface, wherein the interior surface defines a first flow passage; a first plurality of fins projecting inwardly from the interior surface of the conduit, wherein the plurality of fins are angled relative to a longitudinal axis (X) of the conduit so as to form helical flowpaths for fluid flowing through the first flow passage; and a second flow passage disposed outwardly of the interior surface and radially outwardly of the plurality of fins.
2. The heat exchanger of claim 1, wherein the first plurality of fins are straight along their length.
3. The heat exchanger of claim 1, wherein the first plurality of fins are at least partially curved along their length.
4. The heat exchanger of claim 1, wherein the first plurality of fins are corrugated along their length.
5. The heat exchanger of claim 1, wherein the first plurality of fins are distributed circumferentially around the interior surface of the conduit.
6. The heat exchanger of claim 1, wherein the first plurality of fins are distributed circumferentially around less than 50% of the interior surface of the conduit.
7. The heat exchanger of claim 1, wherein the second flow passage extends around less than 50% of the circumference of the conduit.
8. The heat exchanger of claim 1, wherein the conduit further comprises an exterior surface, and wherein the second flow passage is disposed between the interior surface and exterior surface of the conduit.
9. The heat exchanger of claim 1, wherein a second plurality of fins project into the second flow passage, wherein, optionally, the second plurality of fins are aligned with and/or are extensions of said first plurality of fins.
10. The heat exchanger of claim 1, wherein the conduit cross-section has a maximum diameter of less than 200 mm.
11. The heat exchanger of claim 1, wherein the conduit further comprises an outlet, and wherein an angle formed between the first plurality of fins and the longitudinal axis (X) of the conduit is between 10 and 45, optionally wherein the angle formed is between 10 and 20.
12. A system comprising: a heat exchanger that includes: a conduit with an interior surface, wherein the interior surface defines a first flow passage; a first plurality of fins projecting inwardly from the interior surface of the conduit, wherein the plurality of fins are angled relative to a longitudinal axis (X) of the conduit so as to form helical flowpaths for fluid flowing through the first flow passage; and a second flow passage disposed outwardly of the interior surface and radially outwardly of the plurality of fins; and a matrix with an inlet disposed downstream of the first flow passage to receive the flow from the first flow passage.
13. The system of claim 12, wherein the matrix is one of a heat exchanger matrix or an ozone converter matrix.
14. A method of operating the heat exchanger of claim 1, the method comprising the steps of: providing a first fluid flow to an inlet of the first flow passage, and a second fluid flow to an inlet of the second flow passage; swirling the fluid flow in the helical flowpaths in the first flow passage; and exchanging heat between the first fluid flow and the second fluid flow.
15. A method of operating the system of claim 12, the method comprising the steps of: providing a first fluid flow to an inlet of the first flow passage, and a second fluid flow to an inlet of the second flow passage; swirling the fluid flow in the helical flowpaths in the first flow passage; exchanging heat between the first fluid flow and the second fluid flow; and admitting the first fluid flow into the inlet of the matrix.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
[0029]
[0030]
[0031]
[0032]
[0033]
[0034]
DETAILED DESCRIPTION
[0035]
[0036] Heat exchange fins 26 project from the interior surface 18 into the first flow passage 22. The fins 26 are distributed around the circumference of the conduit 16, extending inwardly from the portion of the conduit 16 where the second flow passage 24 is disposed. Hence, the fins 26 also extend around less than 50% of the circumference of the conduit 16. In the example shown, the fins 26 extend less than 50% of the distance between the interior surface 18 and the centre of the conduit 16. For example, the fins may extend inwardly between 25 and 50% of the conduit radius.
[0037] Heat is exchanged between the first flow passage 22 and the second flow passage 24 through the fins 26. Hence, substantial heat exchange only occurs in the portion of the conduit 16 in which the fins 26 and the second flow passage 24 are disposed.
[0038]
[0039]
[0040] With reference to
[0041]
[0042] The fins 26 are angled relative to a longitudinal axis X of the conduit 16 in order to direct and swirl the flow in the first flow passage 22. The fins 26 form helical flowpaths 27 therebetween in order to direct the flow. The flow in the first flow passage 22 is imparted with an angular momentum in order to spin outward from the outlet 32 of the conduit 16 to an inlet of a downstream matrix (not shown). By this mechanism, the flow is more evenly distributed across an inlet of the matrix, particularly at the points of the matrix inlet furthest from the centre of the outlet 32 of the conduit 16. Such an arrangement is illustrated schematically in
[0043] The matrix could be for the purpose of heat exchange or facilitating a chemical reaction. It is envisaged that the matrix could form part of a heat exchanger or ozone converter for an environmental control system of an aircraft.
[0044] As can be seen in
[0045]
[0046] In an example not shown in the figures, the fins 26 could be corrugated along their length to provide increased heat-transfer interaction with the flow in the first flow passage 22. The fins would further be arranged to form a helical flowpath 27 in order to swirl the flow, as discussed above.
[0047] Although not shown, non-exchange fins 28 could have the form of either of the heat exchange fins 26 of
[0048] In further embodiments, a second set of fins 25 may project into the second flow passage 24. This would provide increased interaction with the fluid flow in the second flow passage 24 to improve heat exchange with a fluid therein. The second set of fins 25 may be aligned with the heat exchange fins 26, or be an extension of the heat exchange fins 26 through the interior surface 18 of the conduit 16. Such an embodiment is illustrated schematically by dotted lines in
[0049] In an arrangement not shown, the fins of the second set of fins 25 may be circumferentially offset from the first set of fins 26. For example, they may be positioned circumferentially between the first fins.
[0050] In accordance with the present disclosure, therefore, heat-exchanger fins can be arranged on the interior surface of a conduit which supplies a fluid to a matrix. The fins are angled to form a helical flowpath and thereby as a flow swirler. Hence, the conduit can swirl flow for a downstream matrix and provide for heat-exchange.
[0051] Although the figures and the accompanying description describe particular embodiments and examples, it is to be understood that the scope of this disclosure is not to be limited to such specific embodiments, and is, instead, to be determined by the following claims.