Method for the production of a heat exchanger having a tubulator insert
09539676 · 2017-01-10
Assignee
Inventors
Cpc classification
F28F2275/04
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F28F1/40
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F28F9/162
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F28F2275/06
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Y10T29/49391
GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
International classification
F28F1/40
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
B21C37/15
PERFORMING OPERATIONS; TRANSPORTING
F28F9/16
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Abstract
In a method for the production of a heat exchanger, a turbulator insert is placed into a heat exchanging tube, with the turbulator insert having a solder applied thereon in at least one region. Weld spots using resistance welding are formed on an inner surface of the heat exchanging tube with the turbulator insert, and the inner surface of the heat exchanging tube is interlinked with the turbulator insert through brazing.
Claims
1. A method for the production of a heat exchanger, comprising: placing a turbulator insert into a heat exchanging tube, with the turbulator insert having a solder applied thereon in at least one region; forming weld spots using resistance welding on an inner surface of the heat exchanging tube to form a connection with the turbulator insert, wherein the turbulator insert is fixed in position in the heat exchanging tube substantially air-gap free by the resistance welding; and interlinking the inner surface of the heat exchanging tube with the turbulator insert through brazing.
2. The method of claim 1, wherein the turbulator insert is configured in the form of a finned plate having fins configured to point in a longitudinal direction of the heat exchanging tube.
3. The method of claim 1, further comprising forming depressions in the heat exchanging tube.
4. The method of claim 3, wherein the depressions are configured as notches.
5. The method of claim 3, wherein the depressions are formed in the heat exchanging tube in one of two ways, a first way before the turbulator insert is placed into the heat exchanging tube, a second way after the turbulator insert is placed into the heat exchanging tube.
6. The method of claim 3, wherein a first depression is formed in an end region or midsection of the heat exchanging tube before the turbulator insert is placed in the heat exchanging tube, and subsequently a second depression is formed in a remaining region of the heat exchanging tube.
7. The method of claim 6, wherein the first depression is sized to project into the heat exchanging tube to a lesser extent than the second depression.
8. The method of claim 1, wherein the turbulator insert is securely fixed in the heat exchanging tube.
9. The method of claim 8, wherein the turbulator insert is clamped in the heat exchanging tube.
10. The method of claim 1, further comprising applying a welding current to a top side and to an underside of the heat exchanging tube.
11. The method of claim 10, further comprising forming depressions in the heat exchanging tube, wherein the welding current is applied at such intensity to establish a welded joint between an inner side of the depressions and the turbulator insert.
12. The method of claim 1, further comprising arranging the heat exchanging tube in an outer tube, and placing an inner flange in an end region of the outer tube for fixedly securing the heat exchanging tube.
13. The method of claim 12, further comprising brazing at least one region of at least one combination selected from the group consisting of heat exchanging tube and inner flange, and outer tube and inner flange.
Description
BRIEF DESCRIPTION OF THE DRAWING
(1) Other features and advantages of the present invention will be more readily apparent upon reading the following description of currently preferred exemplified embodiments of the invention with reference to the accompanying drawing, in which:
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DETAILED DESCRIPTION OF PREFERRED EMBODIMENTS
(5) Throughout all the figures, same or corresponding elements may generally be indicated by same reference numerals. These depicted embodiments are to be understood as illustrative of the invention and not as limiting in any way. It should also be understood that the figures are not necessarily to scale and that the embodiments are sometimes illustrated by graphic symbols, phantom lines, diagrammatic representations and fragmentary views. In certain instances, details which are not necessary for an understanding of the present invention or which render other details difficult to perceive may have been omitted.
(6) Turning now to the drawing, and in particular to
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(9) While the invention has been illustrated and described in connection with currently preferred embodiments shown and described in detail, it is not intended to be limited to the details shown since various modifications and structural changes may be made without departing in any way from the spirit and scope of the present invention. The embodiments were chosen and described in order to explain the principles of the invention and practical application to thereby enable a person skilled in the art to best utilize the invention and various embodiments with various modifications as are suited to the particular use contemplated.