US349060A - P- serve - Google Patents
P- serve Download PDFInfo
- Publication number
- US349060A US349060A US349060DA US349060A US 349060 A US349060 A US 349060A US 349060D A US349060D A US 349060DA US 349060 A US349060 A US 349060A
- Authority
- US
- United States
- Prior art keywords
- tube
- fins
- wings
- transverse section
- tubes
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Lifetime
Links
- 239000007787 solid Substances 0.000 description 14
- 229910052751 metal Inorganic materials 0.000 description 12
- 239000002184 metal Substances 0.000 description 12
- 230000005540 biological transmission Effects 0.000 description 4
- 230000000875 corresponding Effects 0.000 description 4
- 239000007789 gas Substances 0.000 description 4
- 238000004519 manufacturing process Methods 0.000 description 4
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 4
- 210000004185 Liver Anatomy 0.000 description 2
- 230000003416 augmentation Effects 0.000 description 2
- 230000015572 biosynthetic process Effects 0.000 description 2
- 230000005494 condensation Effects 0.000 description 2
- 238000009833 condensation Methods 0.000 description 2
- 238000010276 construction Methods 0.000 description 2
- 238000005755 formation reaction Methods 0.000 description 2
- 239000000446 fuel Substances 0.000 description 2
- 150000002739 metals Chemical class 0.000 description 2
- 238000005096 rolling process Methods 0.000 description 2
Images
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F28—HEAT EXCHANGE IN GENERAL
- F28F—DETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
- F28F1/00—Tubular elements; Assemblies of tubular elements
- F28F1/10—Tubular elements and assemblies thereof with means for increasing heat-transfer area, e.g. with fins, with projections, with recesses
- F28F1/42—Tubular elements and assemblies thereof with means for increasing heat-transfer area, e.g. with fins, with projections, with recesses the means being both outside and inside the tubular element
-
- Y—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
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/4935—Heat exchanger or boiler making
- Y10T29/49377—Tube with heat transfer means
- Y10T29/49378—Finned tube
-
- Y—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
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/4935—Heat exchanger or boiler making
- Y10T29/49377—Tube with heat transfer means
- Y10T29/49378—Finned tube
- Y10T29/49384—Internally finned
Definitions
- the object of my invention is to increase the capability of transmission of heat, and also to increase the rigidity of the tubes without proportionately reducing the area of the tubes intheir transverse section. I obtain this result by constructing or providing the tubes with longitudinal solid and massive wings or fins,-either internal or external to the tubes. Tubes with such wings or fins employed in surface-condensers present to the water of condensation the greatest heating-surface possible and to steam the greatest cooling-surface possible, and
- These wingsor fins may have a rectilinear f0rm-- that is to say, may be arranged along the tube; or they may be arranged spirally around the tube.
- the dimensions, the form, the position, and'the number of the said fins or wings are Variable, and they may be applied or provided on the tubes,whatever be the construction of the latter, by any known means of manufacture-that is to ,say, in certain cases the fins or wings may be obtained directly by the rolling of a sheet of metal which is to be afterward rolled up to form the tube.
- the wings may be obtained by folding the sheet. In. other cases they maybe applied after the completion of the tube; and in other cases yet they may be obtained directly in the operation of drawing the tube when that mode of manufacture is employed.
- the wings are, however, always solid and massive, as distinguished from concave-convex dates or corrugations.
- My invention has for its principal advantages, first, the augmentation, in a very great proportion, of the transmission of heat by reason of the increase of the heating-surface, and consequently the diminution in aconsiderable degree of the expense of fuel; second, the incrcasedrigidity of the tubes, which permits the employment for their manufacture of certain metals which could not otherwise be used.
- Figure 1 of the drawings represents a transverse section of a seamless tube with internal fins.
- Fig. 2 represents a transverse section of a seamless tube with external fins.
- Fig. 3 represents a transverse section of a seamless tube with internal and external fins.
- Fig. 4 is a transverse section of a seamed tube with internal fins.
- Fig. 5 is a transverse section of a seamed tube with internal and external fins; and
- Fig. 6 is a transverse section of a seamed tube with specially constructed internal and external fins.
- the seamless drawn tube and the fins are obtained directly by the drawing operation. They may be only, as at a, in the in-- terior of the tube 1), Fig. 1, or they may be only on the exterior, as at c, Fig. 2, or both, as at a and c, in the interior and on the exterior, Fig. 3.
- the tube is seamed-that is to say, formed of a sheet or strip of metal, I), rolled and soldered in the joint (I.
- the fins are simply constituted by folds a, all formed onsame side of the sheet 12, and of which the two thicknesses are soldered one to the other at e, as in the joint (1 of the tube.
- folds are obtained by any mechanical means, and may be arranged either on the exterior or in the interior of the tube.
- the fins are formed of folds, as'has been described, and placcd'in the interior and on the exterior of the tube. Instead of being juxtaposited, as seen in the last-mentioned figure, the interior and exterior folds may be separated a certain distance.
- Fig. 6 I have represented an examp e in which the fins are both internal and external and formed of folds a, arranged in the inte" rior of the tube,as before described,but wider, and into this .I introduce bandsf, formed t enter the said folds and to project therefrom to form the external fins, the said bands being IOO soldered ate to the sides of the fold.
- fins may also be constituted by bands simply I applied and soldered or riveted upon the wall of the tube, the tube itself being in such case either seamless or seamed.
- the fins may have any forms and dimensions whatever. They may be arranged on the tube in any manner whatever, and obtained on the sheets of metal either before or after the formation of the tube, or directly by the drawing of the tnbe,whethcr the tubes are seamless or seamed.
- tubes have been made with a corrugated or undulating profile in their transverse section, thereby securing a cour paratively slight increase in their radiating- Surface, and with almost a corresponding re duction in the area of their transverse section,
- nil I do not include such a tubein myiuven tion.
- My tube is distinguished from those which have been before made in having, solid and massive wings which, when on the interior surfaces, project to a considerable dis tance into the tube and receive heat from the hottest gases which pass through the tube, and, whether upon. the interior or exterior surface, such wings very greatly increase the heatingsnrface of the tube and reduce but very little the transverse area of the tube-passage.
- the interior or exterior heating-surface, or both may be doubled or trebled without any proportionate reduction of the areal in transverse section, although, of course, the area will be slightly reduced by the interior wings.
Landscapes
- Physics & Mathematics (AREA)
- Engineering & Computer Science (AREA)
- Geometry (AREA)
- Thermal Sciences (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Heat-Exchange Devices With Radiators And Conduit Assemblies (AREA)
Description
(No Model.)
J.' P. SERVE.
BOILER TUBE.
UNITED warns,
JEAN PI EERJE SERVE,
OF GIVOR-S, FRANCE.
BOILER-TUBE.
' SPECIFICATION forming part of Letters Patent No. 349,060, dated September 14, 1886.
Application filed February 6, 1886. m-i=1 3T0. .iitflfri.
(No model.) Iainnlell in France Scpiemher20,1S8 I, No. 164,412.
To all whom it nutty concern.-
Be it known that I, J nan PIERRE SERVE, L citizen of the Republic of France, residing at (livers, in the said Republic, have invented a new and useful Improvement in Metallic Tubes for Steam Boilers and Condensers, of which the following is a specification, reference being had to the accompanying drawings.
The object of my invention is to increase the capability of transmission of heat, and also to increase the rigidity of the tubes without proportionately reducing the area of the tubes intheir transverse section. I obtain this result by constructing or providing the tubes with longitudinal solid and massive wings or fins,-either internal or external to the tubes. Tubes with such wings or fins employed in surface-condensers present to the water of condensation the greatest heating-surface possible and to steam the greatest cooling-surface possible, and
in a boiler they present the greatest surface to the water and to the gases of cor :buation. rho same result is obtained by them in other apparatus for transmitting heat or cold. These wingsor fins may have a rectilinear f0rm-- that is to say, may be arranged along the tube; or they may be arranged spirally around the tube. The dimensions, the form, the position, and'the number of the said fins or wings are Variable, and they may be applied or provided on the tubes,whatever be the construction of the latter, by any known means of manufacture-that is to ,say, in certain cases the fins or wings may be obtained directly by the rolling of a sheet of metal which is to be afterward rolled up to form the tube. In other cases the wings may be obtained by folding the sheet. In. other cases they maybe applied after the completion of the tube; and in other cases yet they may be obtained directly in the operation of drawing the tube when that mode of manufacture is employed. The wings are, however, always solid and massive, as distinguished from concave-convex dates or corrugations.
My invention has for its principal advantages, first, the augmentation, in a very great proportion, of the transmission of heat by reason of the increase of the heating-surface, and consequently the diminution in aconsiderable degree of the expense of fuel; second, the incrcasedrigidity of the tubes, which permits the employment for their manufacture of certain metals which could not otherwise be used.
Figure 1 of the drawings represents a transverse section of a seamless tube with internal fins. Fig. 2 represents a transverse section of a seamless tube with external fins. Fig. 3 represents a transverse section of a seamless tube with internal and external fins. Fig. 4 is a transverse section of a seamed tube with internal fins. Fig. 5 is a transverse section of a seamed tube with internal and external fins; and Fig. 6 is a transverse section of a seamed tube with specially constructed internal and external fins.
Similar letters of reference desgnatc corresponding parts in all the figures.
As may be seen by reference to the draw ings in the examples represented by Fig. 1, 2, and 3, the seamless drawn tube and the fins are obtained directly by the drawing operation. They may be only, as at a, in the in-- terior of the tube 1), Fig. 1, or they may be only on the exterior, as at c, Fig. 2, or both, as at a and c, in the interior and on the exterior, Fig. 3.
In the examples represented in Figs. 4, 5, and 6 the tubeis seamed-that is to say, formed of a sheet or strip of metal, I), rolled and soldered in the joint (I. In Fig. 4 the fins are simply constituted by folds a, all formed onsame side of the sheet 12, and of which the two thicknesses are soldered one to the other at e, as in the joint (1 of the tube. These folds are obtained by any mechanical means, and may be arranged either on the exterior or in the interior of the tube.
In the example shown in Fig. 5 the fins are formed of folds, as'has been described, and placcd'in the interior and on the exterior of the tube. Instead of being juxtaposited, as seen in the last-mentioned figure, the interior and exterior folds may be separated a certain distance.
In Fig. 6 I have represented an examp e in which the fins are both internal and external and formed of folds a, arranged in the inte" rior of the tube,as before described,but wider, and into this .I introduce bandsf, formed t enter the said folds and to project therefrom to form the external fins, the said bands being IOO soldered ate to the sides of the fold. The
fins may also be constituted by bands simply I applied and soldered or riveted upon the wall of the tube, the tube itself being in such case either seamless or seamed.
The fins may have any forms and dimensions whatever. They may be arranged on the tube in any manner whatever, and obtained on the sheets of metal either before or after the formation of the tube, or directly by the drawing of the tnbe,whethcr the tubes are seamless or seamed.
I am aware that tubes have been made with a corrugated or undulating profile in their transverse section, thereby securing a cour paratively slight increase in their radiating- Surface, and with almost a corresponding re duction in the area of their transverse section,
nil I do not include such a tubein myiuven tion. My tube is distinguished from those which have been before made in having, solid and massive wings which, when on the interior surfaces, project to a considerable dis tance into the tube and receive heat from the hottest gases which pass through the tube, and, whether upon. the interior or exterior surface, such wings very greatly increase the heatingsnrface of the tube and reduce but very little the transverse area of the tube-passage. By the solid and massive wings the interior or exterior heating-surface, or both, may be doubled or trebled without any proportionate reduction of the areal in transverse section, although, of course, the area will be slightly reduced by the interior wings.
What I claim as my invention,and d .zSllG to secureby Letters Patent, is-
1. The tube herein described for boil ers and condensers, having solid and massive wings upon its surface or surfaces, as distinguish d from a tube having awavy, corrugated vvor nu dnlating profile in transverse section, substantially as herein set forth.
2. The tube herein described for boilers and condensers, having its metal folded closely upon itself to form solid and massive wings upon its surface or surfaces, substantially as herein set forth.
3. The tube herein described for boil s and condensersdiaving its metal folded upon itself to form wings upon one surface, and having strips or pieces j" inserted within SUCK folds and projecting beyond the other surface. whereby are produced solid and massive wings projecting from both surfaces of the tulie, snlr stantially as herein described.
In testimony whereof I have sign d this specification in the presence of two subscribing witnesses.
JEAN PIERRE SE1" VE.
\Vi tnesses: F. J. Rsmrono,
N. HALL, Jr.
Publications (1)
Publication Number | Publication Date |
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US349060A true US349060A (en) | 1886-09-14 |
Family
ID=2418127
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US349060D Expired - Lifetime US349060A (en) | P- serve |
Country Status (1)
Country | Link |
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US (1) | US349060A (en) |
Cited By (15)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2656158A (en) * | 1948-07-23 | 1953-10-20 | Air Preheater | Plate type heat exchanger and method of manufacturing same |
US2930405A (en) * | 1955-05-31 | 1960-03-29 | Brown Fintube Co | Tube with internal fins and method of making same |
US3568766A (en) * | 1969-03-11 | 1971-03-09 | Atomic Energy Commission | Corrugated heat exchange member for evaporation and condensation |
US5186250A (en) * | 1990-05-11 | 1993-02-16 | Showa Aluminum Kabushiki Kaisha | Tube for heat exchangers and a method for manufacturing the tube |
US5441105A (en) * | 1993-11-18 | 1995-08-15 | Wynn's Climate Systems, Inc. | Folded parallel flow condenser tube |
US5655599A (en) * | 1995-06-21 | 1997-08-12 | Gas Research Institute | Radiant tubes having internal fins |
US5890288A (en) * | 1997-08-21 | 1999-04-06 | Ford Motor Company | Method for making a heat exchanger tube |
US5934365A (en) * | 1997-08-21 | 1999-08-10 | Ford Motor Company | Heat exchanger |
US6006826A (en) * | 1997-03-10 | 1999-12-28 | Goddard; Ralph Spencer | Ice rink installation having a polymer plastic heat transfer piping imbedded in a substrate |
US6209202B1 (en) | 1999-08-02 | 2001-04-03 | Visteon Global Technologies, Inc. | Folded tube for a heat exchanger and method of making same |
US6286465B1 (en) | 2000-04-28 | 2001-09-11 | Aos Holding Company | Water heater flue system |
US6422179B2 (en) | 2000-04-28 | 2002-07-23 | Aos Holding Company | Water heater flue system |
US20090294112A1 (en) * | 2008-06-03 | 2009-12-03 | Nordyne, Inc. | Internally finned tube having enhanced nucleation centers, heat exchangers, and methods of manufacture |
US7679096B1 (en) * | 2003-08-21 | 2010-03-16 | Opto Technology, Inc. | Integrated LED heat sink |
US20100300665A1 (en) * | 2009-06-02 | 2010-12-02 | Denoual Christophe | Heat Exchange Unit And Corresponding Heat Exchanger, Method Of Manufacturing A Heat Exchange Unit |
-
0
- US US349060D patent/US349060A/en not_active Expired - Lifetime
Cited By (19)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2656158A (en) * | 1948-07-23 | 1953-10-20 | Air Preheater | Plate type heat exchanger and method of manufacturing same |
US2930405A (en) * | 1955-05-31 | 1960-03-29 | Brown Fintube Co | Tube with internal fins and method of making same |
US3568766A (en) * | 1969-03-11 | 1971-03-09 | Atomic Energy Commission | Corrugated heat exchange member for evaporation and condensation |
US5186250A (en) * | 1990-05-11 | 1993-02-16 | Showa Aluminum Kabushiki Kaisha | Tube for heat exchangers and a method for manufacturing the tube |
US5386629A (en) * | 1990-05-11 | 1995-02-07 | Showa Aluminum Kabushiki Kaisha | Tube for heat exchangers and a method for manufacturing the tube |
US5441105A (en) * | 1993-11-18 | 1995-08-15 | Wynn's Climate Systems, Inc. | Folded parallel flow condenser tube |
US5655599A (en) * | 1995-06-21 | 1997-08-12 | Gas Research Institute | Radiant tubes having internal fins |
US6006826A (en) * | 1997-03-10 | 1999-12-28 | Goddard; Ralph Spencer | Ice rink installation having a polymer plastic heat transfer piping imbedded in a substrate |
US5934365A (en) * | 1997-08-21 | 1999-08-10 | Ford Motor Company | Heat exchanger |
US5890288A (en) * | 1997-08-21 | 1999-04-06 | Ford Motor Company | Method for making a heat exchanger tube |
US6209202B1 (en) | 1999-08-02 | 2001-04-03 | Visteon Global Technologies, Inc. | Folded tube for a heat exchanger and method of making same |
US6286465B1 (en) | 2000-04-28 | 2001-09-11 | Aos Holding Company | Water heater flue system |
US6422179B2 (en) | 2000-04-28 | 2002-07-23 | Aos Holding Company | Water heater flue system |
US7679096B1 (en) * | 2003-08-21 | 2010-03-16 | Opto Technology, Inc. | Integrated LED heat sink |
US20100149818A1 (en) * | 2003-08-21 | 2010-06-17 | Opto Technology Inc. | Integrated led heat sink |
US7923748B2 (en) * | 2003-08-21 | 2011-04-12 | Excelitas Technologies LED Solutions, Inc. | Integrated LED heat sink |
US20090294112A1 (en) * | 2008-06-03 | 2009-12-03 | Nordyne, Inc. | Internally finned tube having enhanced nucleation centers, heat exchangers, and methods of manufacture |
US20100300665A1 (en) * | 2009-06-02 | 2010-12-02 | Denoual Christophe | Heat Exchange Unit And Corresponding Heat Exchanger, Method Of Manufacturing A Heat Exchange Unit |
US9103604B2 (en) * | 2009-06-02 | 2015-08-11 | Valeo Systemes Thermiques | Heat exchange unit and corresponding heat exchanger, method of manufacturing a heat exchange unit |
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