Metal heat exchanger tube

Patent metadata

Field	Value
Publication number	US-11073343-B2
Application number	US-201515103193-A
Country	US
Kind code	B2
Filing date	Feb 10, 2015
Priority date	Feb 27, 2014
Publication date	Jul 27, 2021
Grant date	Jul 27, 2021

Abstract

A metal heat exchanger tube has integral ribs formed on the outside of the tube. The ribs have a rib base, rib flanks, and a rib tip. The rib base protrudes substantially radially from the tube wall. A channel is formed between the ribs, in which channel additional structures spaced apart from each other are arranged. The additional structures divide the channel between the ribs into segments. The additional structures reduce the cross-sectional area in the channel between two ribs through which flow is possible by at least 60% locally and, at least thereby, limit a fluid flow in the channel during operation.

First claim

The invention claimed is:

1. A metal heat exchanger tube comprising:
a tube wall;
a plurality of integrally encircling fins formed on the outside of the tube, wherein each fin has a fin foot, fin flanks and a fin tip, and the fin foot protrudes radially from the tube wall, and
a channel formed between two adjacent fins, wherein the channel has a throughflow cross-sectional area perpendicular to the course of the channel, and
spaced-apart additional structures arranged in portions of the channel,
a first total throughflow cross-sectional area A 1 being the minimum total throughflow cross-section area measured perpendicular to the course of the channel in the portions of the channel where the additional structures are arranged;
a second total throughflow cross-sectional area A 2 being the maximum total throughflow cross-section area measured perpendicular to the course of the channel in the portions of the channel where the additional structures are not arranged;
wherein the additional structures divide the channel into segments, and
wherein a reduction of the first total throughflow cross-sectional area A 1 relative to the second total throughflow cross-sectional area A 2 is at least 60% of the second total throughflow cross-sectional area A 2 .

2. The heat exchanger tube as claimed in claim 1 , wherein the additional structures reduce the throughflow cross-sectional area in the portions of the channel in which they are arranged by at least 80% as compared to the portions of the channel in which they are not arranged.

3. The heat exchanger tube as claimed in claim 2 , wherein the additional structures completely close the throughflow cross-sectional area in the portions of the channel in which they are arranged.

4. The heat exchanger tube as claimed in claim 1 , wherein the channel is closed radially outward except for individual openings.

5. The heat exchanger tube as claimed in claim 1 , wherein there is at least one individual opening per segment.

6. The heat exchanger tube as claimed in claim 5 , wherein the quotient of the number of individual openings to the number of segments is 1:1 to 6:1.

7. The heat exchanger tube as claimed in claim 1 , wherein the additional structures comprise first additional structures that are radially outwardly directed projections emerging from a base of the channel.

8. The heat exchanger tube as claimed in claim 7 , wherein the first additional structures are formed at least partially from material of the tube wall from the channel base.

9. The heat exchanger tube as claimed in claim 8 , wherein the first additional structures formed from the channel base have a height of between 0.15 and 1 mm.

10. The heat exchanger tube as claimed in claim 7 , wherein the additional structures comprise second additional structures that are formed at least from the fin flanks or fin tips of the integrally encircling fins via lateral projections.

11. The heat exchanger tube as claimed in claim 10 , wherein the second additional structures are formed at least from one fin emerging from the fin tip in the direction toward the channel base.

12. The heat exchanger tube as claimed in claim 1 , wherein additional structures are at least partially provided via additional material.

13. The heat exchanger tube as claimed in claim 1 , wherein the additional structures have asymmetric shapes.

14. The heat exchanger tube as claimed in claim 1 , wherein additional structures have a trapezoidal cross section in a section plane running perpendicularly to the tube axis.

15. The heat exchanger tube as claimed in claim 1 , wherein the respective throughflow cross-sectional area in the channel between two fins that is reduced by additional structures varies.

16. A metal heat exchanger tube comprising:
a tube wall;
a plurality of integrally encircling fins formed on the outside of the tube, wherein each fin has a fin foot, fin flanks and a fin tip, and the fin foot protrudes radially from the tube wall, and
a channel formed between two adjacent fins, wherein the channel has a through flow cross-sectional area perpendicular to the course of the channel, and
spaced-apart additional structures arranged in portions of the channel,
a first total throughflow cross-sectional area A 1 being the minimum total throughflow cross-section area measured perpendicular to the course of the channel in the portions of the channel where the additional structures are arranged;
a second total throughflow cross-sectional area A 2 being the maximum total throughflow cross-section area measured perpendicular to the course of the channel in the portions of the channel where the additional structures are not arranged;
wherein the additional structures divide the channel into segments,
wherein a reduction of the first total throughflow cross-sectional area A 1 relative to the second total throughflow cross-sectional area A 2 is at least 60% of the second total throughflow cross-sectional area A 2 .

17. A metal heat exchanger tube comprising:
a tube wall;
a plurality of integrally encircling fins formed on the outside of the tube, wherein each fin has a fin foot, fin flanks and a fin tip, and the fin foot protrudes radially from the tube wall, and
a channel formed between two adjacent fins, wherein the channel has a throughflow cross-sectional area perpendicular to the course of the channel, and
spaced-apart additional structures arranged in portions of the channel,
wherein the additional structures divide the channel into segments,
wherein first ones of the additional structures project from a base of the channel and second ones of the additional structures extend radially from the fin tip such that when the second ones of the additional structures lie above the first additional structures as viewed radially there is a reduction in the throughflow cross-sectional area in the channel between two adjacent fins in order to limit fluid flow in the channel by at least 60%.

Assignees

• Wieland Werke Ag

Inventors

• Gotterbarm Achim
• Lutz Ronald
• El Hajal Jean
• Knab Manfred

Classifications

• F28F13/187

  especially adapted for evaporator surfaces or condenser surfaces, e.g. with nucleation sites · CPC title

• F28F1/36 Primary

  the means being helically wound fins or wire spirals · CPC title

• F28F1/422

  with outside means integral with the tubular element and inside means integral with the tubular element (F28F1/424 takes precedence) · CPC title

• F25B39/00

  Evaporators; Condensers · CPC title

• F28F13/08

  by varying the cross-section of the flow channels · CPC title