US2535721A - Cylindrical heat exchanger - Google Patents

Cylindrical heat exchanger Download PDF

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US2535721A
US2535721A US752094A US75209447A US2535721A US 2535721 A US2535721 A US 2535721A US 752094 A US752094 A US 752094A US 75209447 A US75209447 A US 75209447A US 2535721 A US2535721 A US 2535721A
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Prior art keywords
fins
sleeve
heat
fin
arms
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US752094A
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Chausson Gaston
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Chausson Usines SA
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Chausson Usines SA
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    • H—ELECTRICITY
    • H01—ELECTRIC ELEMENTS
    • H01J—ELECTRIC DISCHARGE TUBES OR DISCHARGE LAMPS
    • H01J19/00—Details of vacuum tubes of the types covered by group H01J21/00
    • H01J19/28—Non-electron-emitting electrodes; Screens
    • H01J19/32—Anodes
    • H01J19/36—Cooling of anodes
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F28—HEAT EXCHANGE IN GENERAL
    • F28F—DETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
    • F28F2215/00—Fins
    • F28F2215/10—Secondary fins, e.g. projections or recesses on main fins
    • H—ELECTRICITY
    • H01—ELECTRIC ELEMENTS
    • H01J—ELECTRIC DISCHARGE TUBES OR DISCHARGE LAMPS
    • H01J2893/00—Discharge tubes and lamps
    • H01J2893/0001—Electrodes and electrode systems suitable for discharge tubes or lamps
    • H01J2893/0012—Constructional arrangements
    • H01J2893/0027—Mitigation of temperature effects

Definitions

  • My invention relates to cylindrical heatexchangers comprising a sleeve on which is mounted a circular bundle of radial fins which are used in particular for dissipating the heat produced by the anode of thermionic valves for radio or for high-frequency heating, by causing said heat to be absorbed by another fluid, generally air.
  • the invention is however not limited to this application and covers all heat-exchangers of this type, in particular for heat engines.
  • Such apparatus have been constructed by providing slits intended for the air to pass in a mass of copper or other metal of generally cylindrical shape.
  • This method of manufacture has the drawback of requiring a large mass of metal, a considerable part of which is converted into chips, of requiring a long and costly machine and of only providing narrow air passages which are therefore not favourable for a turbulent flow, and also passage cross-sections for the heat through the metal which are not rationally arranged since they increase as they are more remote from the sleeve.
  • a cylindrical sleeve has also been constructed which is provided along its periphery with groove in which were mounted fins comprising radiating blades.
  • This device has the drawback that the fins are very close together adjacent the sleeve and are very far apart near the periphery of the bundle, so that as the air pas sages become considerably wider towards the periphery, the rates of flow of air through the various zones of the bundle of blades do not correspond to the cross-sections of metal conducting the heat.
  • My invention overcomes the drawbacks of air passages are provided whose cross-section varies but little, both near the sleeve and in the peripheral zone and the heat-exchange surface provided for the air is considerably increased relatively to the known apparatus.
  • each fin comprises a metal sheet which is cut out and folded on itself, the fold forming a base being intended to be fixed in a slot of a supporting sleeve, the two folded portions being contiguous in the zone adjacent the sleeve and then parting and forming a fork in the peripheral zone.
  • the brazing that fixes the fin to the sleeve cannot spread uselessly between the two parts of the fin into which capillarity might draw it, thereby also economising the brazing.
  • the fins do not penetrate far enough into the grooves of said sleeve to make it possible to have the arms of the fins equidistant at the periphery.
  • combs which hold the fins in their relative position during the brazing operation. Said combs are fragile, they have to be constructed of the same metal as the fins for expansion purposes, they are expensive and their life is short owing to their frequent insertions in the brazing furnace.
  • the present invention also provides means which enable said combs to be dispensed with.
  • tongues cut out in the arms of the fork of the fins are bent so as to retain the spacing between the two arms of a fin and between the arms of successive fins.
  • Tongues may also be formed in the body of the fins at the end portions, i. e. at the inlet and at the outlet of the draught of air.
  • Several tongues may moreover be formed on the periphery in the direction of the height of the fin.
  • the tongues also have the advantage of producing a division in the air current and a tur bulence of the air stream which favour the heat exchange.
  • the fins instead of forming the fins by means of a metal sheet bent on itself, they may be obtained by shaping, for example by drawing, spinning, forging, extruding, planing and any other methods of machining.
  • Such fins may have a base provided with two radial side faces relatively to the central cylindrical passage, so that when said bases are juxtaposed and assembled, for example by brazing, they themselves form the sleeve bounding said passage.
  • the forked fins according to the invention may also be provided with secondary fins or be corrugated or be given any other shape which enables the extent of the heat-exchange surfaces to be increased and the heat-exchange coefiicient to be increased by division or turbulence of the air stream.
  • Fig. 1 is an elevation of a cylindrical heatexchanger serving for cooling a transmitter valve.
  • Figs. 2 and 3 are partial transverse sections along the line A-B of Fig. 1 showing diagrammatically two embodiments of the invention.
  • Fig. 4 is a side view of the heat-exchanger, partially in elevation and partially in cross-section to show the profile of the fins.
  • valve 5 serving for example for a radio transmitter
  • said valve is mounted on a heat-exchanger 2 comprising a cylindrical bundle of radial fins held on a central sleeve.
  • a sleeve 5 is provided having slots 6 in which the forked fin bases are engaged.
  • Said fins in this case comprise a. metal sheet which is cut out and folded; the two portions 7, 8 located in the zone near the sleeve 5 are pressed against one another, so as to form, between the adjacent fins, passages 9 of substantial cross-section. Then, periphery, the portions 7, 8 of the folded sheet are bent apart to form a fork, so as to provide further passages it between them, so that in the peripheral zone the number of passages is doubled, since it includes not only the spaces 9 provided between the double fins, but also the spaces it formed between the arms of each fin. In this manner, the air passages are substantially of the same cross-section throughout the mass of the fins, thereby producing an even cut-flow of the heat.
  • tongues ll, 12 are cut out and bent in the metal sheet forming the fins, in such a manner that the tongues ll cut out in one arm 8' of a fin bear against the arm 7 of said fin, then the tongues 12 cut out in the arm 7' of one fin bear against the arm 8 of the adjacent fin.
  • Similar tongues 3 may also be cut out and bent on the periphery of the bodies 1, 3.
  • the tongues IE, 12, 3 may be staggered in such a manner that one of them is not located opposite a perforation of the other.
  • Fig. 3 shows a modification.
  • forked fins I3, 14 with arms I3 l3" and 1%, M" which are obtained by means of a shaping process such as a drawing or other like process.
  • a base l5, having two radial sides, is formed on said fins so that their juxtaposed bases form the sleeve which defines the internal cylindrical passage and it is not necessary to use a sleeve 5 as in the case of Fig. 2.
  • These fins may be calculated so as to obtain air passage cross-sections which are substantially uniform, on the one hand, in the passages it provided between their bodies 53, M, and on the other hand in the passages ll provided between their arms l3, 13'', then in the passages 58 pro vided between the arms 13", i l of two adjacent forked fins.
  • secondary fins I 9 may be formed on the arms of the forked fins so as to increase the heat exchange. Similar secondary fins may also be formed on the bodies l3, l4.
  • the invention can be applied to all heat-exchangers comprising bundles of radial fins, whatever be the application of such heat-exchangers.
  • a cylindrical heat exchanger part cularly adapted for dissipating heat produced by high frequency heating, comprising a passage forming sleeve and a plurality of fins extending outwardly from the periphery of said sleeve, said fins being closely and evenly juxtapositioned about said sleeve and extending radially therefrom to provide narrow substantially uniform spaces therebetween, each of said fins being formed by a sheet that is folded upon itself with the fold forming the base of the fin and being secured to the periphery of the sleeve, the folded portions being contiguous throughout their base portion to form a single body portion extending radially outward from the sleeve, said folded portion being bent apart to form a forked body portion spaced outwardly from said sleeve, and lugs struck from one of the folded portions of each fin and within both the contiguous and forked portions thereof, said lugs extending laterally into engagement with the adjacent fin to maintain said fins in uniformly spaced relation,

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  • Heat-Exchange Devices With Radiators And Conduit Assemblies (AREA)

Description

Dec. 26, 1950 e. CHAUSSON CYLINDRICAL HEAT EXCHANGER Filed June 3, 1947 INVENTOR GASTON CHAUSS'ON ATTK Patented Dec. 26, 1950 CYLINDRICAL HEAT EXCHAN GER Gaston Chausson, Asnieres, France, assignor to Societe Anonyme des Usines Chausson, Asnieres, France, a company of France Application JuneB, 1947, Serial No. 752,094 In France June 14, 1946 My invention relates to cylindrical heatexchangers comprising a sleeve on which is mounted a circular bundle of radial fins which are used in particular for dissipating the heat produced by the anode of thermionic valves for radio or for high-frequency heating, by causing said heat to be absorbed by another fluid, generally air.
The invention is however not limited to this application and covers all heat-exchangers of this type, in particular for heat engines.
In such exchangers, it is necessary to arrange about the anode a suflicient area of surfaces for the ccefficient per unit of heat-exchange surface not to be too high and consequently not to re-- quire a speed and a rate of flow of air such that a high power i needed to produce them.
Such apparatus have been constructed by providing slits intended for the air to pass in a mass of copper or other metal of generally cylindrical shape. This method of manufacture has the drawback of requiring a large mass of metal, a considerable part of which is converted into chips, of requiring a long and costly machine and of only providing narrow air passages which are therefore not favourable for a turbulent flow, and also passage cross-sections for the heat through the metal which are not rationally arranged since they increase as they are more remote from the sleeve.
A cylindrical sleeve has also been constructed which is provided along its periphery with groove in which were mounted fins comprising radiating blades. This device has the drawback that the fins are very close together adjacent the sleeve and are very far apart near the periphery of the bundle, so that as the air pas sages become considerably wider towards the periphery, the rates of flow of air through the various zones of the bundle of blades do not correspond to the cross-sections of metal conducting the heat.
1 Claim. (Cl. 257--2.63)
My invention overcomes the drawbacks of air passages are provided whose cross-section varies but little, both near the sleeve and in the peripheral zone and the heat-exchange surface provided for the air is considerably increased relatively to the known apparatus.
According to an embodiment, each fin comprises a metal sheet which is cut out and folded on itself, the fold forming a base being intended to be fixed in a slot of a supporting sleeve, the two folded portions being contiguous in the zone adjacent the sleeve and then parting and forming a fork in the peripheral zone. In this manner, the brazing that fixes the fin to the sleeve cannot spread uselessly between the two parts of the fin into which capillarity might draw it, thereby also economising the brazing. In the manufacture of apparatus of this type comprising fins or blades arranged radially about a sleeve, the fins do not penetrate far enough into the grooves of said sleeve to make it possible to have the arms of the fins equidistant at the periphery. In order to effect the brazing it was therefore necessary to use combs which hold the fins in their relative position during the brazing operation. Said combs are fragile, they have to be constructed of the same metal as the fins for expansion purposes, they are expensive and their life is short owing to their frequent insertions in the brazing furnace.
The present invention also provides means which enable said combs to be dispensed with.
For this purpose, tongues cut out in the arms of the fork of the fins are bent so as to retain the spacing between the two arms of a fin and between the arms of successive fins. Tongues may also be formed in the body of the fins at the end portions, i. e. at the inlet and at the outlet of the draught of air. Several tongues may moreover be formed on the periphery in the direction of the height of the fin. Thus the fins are held in the suitable relative position before they are inserted in the brazing furnace without use having to be made of retaining combs. The tongues also have the advantage of producing a division in the air current and a tur bulence of the air stream which favour the heat exchange.
According to a modification, instead of forming the fins by means of a metal sheet bent on itself, they may be obtained by shaping, for example by drawing, spinning, forging, extruding, planing and any other methods of machining. Such fins may have a base provided with two radial side faces relatively to the central cylindrical passage, so that when said bases are juxtaposed and assembled, for example by brazing, they themselves form the sleeve bounding said passage.
The forked fins according to the invention may also be provided with secondary fins or be corrugated or be given any other shape which enables the extent of the heat-exchange surfaces to be increased and the heat-exchange coefiicient to be increased by division or turbulence of the air stream.
Further objects and advantages of my invention will be apparent from the description and claim.
In the drawing, in which an embodiment of my invention is illustrated- Fig. 1 is an elevation of a cylindrical heatexchanger serving for cooling a transmitter valve.
Figs. 2 and 3 are partial transverse sections along the line A-B of Fig. 1 showing diagrammatically two embodiments of the invention.
Fig. 4 is a side view of the heat-exchanger, partially in elevation and partially in cross-section to show the profile of the fins.
For cooling a valve 5 serving for example for a radio transmitter, said valve is mounted on a heat-exchanger 2 comprising a cylindrical bundle of radial fins held on a central sleeve.
In the embodiment of Fig. 2, a sleeve 5 is provided having slots 6 in which the forked fin bases are engaged. Said fins in this case comprise a. metal sheet which is cut out and folded; the two portions 7, 8 located in the zone near the sleeve 5 are pressed against one another, so as to form, between the adjacent fins, passages 9 of substantial cross-section. Then, periphery, the portions 7, 8 of the folded sheet are bent apart to form a fork, so as to provide further passages it between them, so that in the peripheral zone the number of passages is doubled, since it includes not only the spaces 9 provided between the double fins, but also the spaces it formed between the arms of each fin. In this manner, the air passages are substantially of the same cross-section throughout the mass of the fins, thereby producing an even cut-flow of the heat.
In order to retain the spacing between the fins and the forked arms, tongues ll, 12 are cut out and bent in the metal sheet forming the fins, in such a manner that the tongues ll cut out in one arm 8' of a fin bear against the arm 7 of said fin, then the tongues 12 cut out in the arm 7' of one fin bear against the arm 8 of the adjacent fin. Similar tongues 3 may also be cut out and bent on the periphery of the bodies 1, 3.
The tongues IE, 12, 3 may be staggered in such a manner that one of them is not located opposite a perforation of the other.
Fig. 3 shows a modification. In this case, use is made of forked fins I3, 14 with arms I3 l3" and 1%, M" which are obtained by means of a shaping process such as a drawing or other like process. A base l5, having two radial sides, is formed on said fins so that their juxtaposed bases form the sleeve which defines the internal cylindrical passage and it is not necessary to use a sleeve 5 as in the case of Fig. 2. The shape of these fins may be calculated so as to obtain air passage cross-sections which are substantially uniform, on the one hand, in the passages it provided between their bodies 53, M, and on the other hand in the passages ll provided between their arms l3, 13'', then in the passages 58 pro vided between the arms 13", i l of two adjacent forked fins.
towards the Furthermore, secondary fins I 9 may be formed on the arms of the forked fins so as to increase the heat exchange. Similar secondary fins may also be formed on the bodies l3, l4.
With this arrangement also, air passage crosssections are obtained which are substantially constant over the entire radial extent of the bundle of fins. In the case of 2, the bases of the fins are brazed in the slots 6 of the sleeve 5 and in the case of Fig. 3, the bases 15 of the fins are brazed against one another. Instead of brazing, the fixing of the fin bases in the sleeve or to one another may be effected by any method which provides mechanical fixing and a passage for the heat.
The invention can be applied to all heat-exchangers comprising bundles of radial fins, whatever be the application of such heat-exchangers.
Further modifications will be apparent to those skilled in the art and it is desired, therefore, that the invention be limited only by the prior art and the scope of the appended claim.
I claim:
A cylindrical heat exchanger part cularly adapted for dissipating heat produced by high frequency heating, comprising a passage forming sleeve and a plurality of fins extending outwardly from the periphery of said sleeve, said fins being closely and evenly juxtapositioned about said sleeve and extending radially therefrom to provide narrow substantially uniform spaces therebetween, each of said fins being formed by a sheet that is folded upon itself with the fold forming the base of the fin and being secured to the periphery of the sleeve, the folded portions being contiguous throughout their base portion to form a single body portion extending radially outward from the sleeve, said folded portion being bent apart to form a forked body portion spaced outwardly from said sleeve, and lugs struck from one of the folded portions of each fin and within both the contiguous and forked portions thereof, said lugs extending laterally into engagement with the adjacent fin to maintain said fins in uniformly spaced relation, the forked body portion bein initiated at a point intermediate the radial length of the fins to maintain the spaces between adjacent fins and their forks substantially constant and the fork forming arms extending radially of the sleeve and being spaced a distance substantially equal to the distance between adjacent fins and their forks, whereby the spaces between said fins and fork arms are substantially equal and said fins and their forks provide a large heat-exchange surface having a substantially uniform relatively low coefficient per surface unit.
GASTON CHAUSSON.
REFERENCES CITED The following references are of record in the file of this patent:
UNITED STATES PATENTS Number Name Date 2,405,317 McCollum Aug. 6, 1946 2,430,681 Eskra Nov. 11, 19 i? FOREIGN PATENTS Number Country Date 371,347 Great Britain Apr. 19, 1932 716,972 France Dec. 3, 1931 546,836 Germany Nov. 16, 1930
US752094A 1946-06-14 1947-06-03 Cylindrical heat exchanger Expired - Lifetime US2535721A (en)

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Cited By (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2680009A (en) * 1953-02-25 1954-06-01 Rca Corp Cooling unit
US2694554A (en) * 1948-12-30 1954-11-16 Rca Corp Cooling unit
US3147801A (en) * 1961-02-09 1964-09-08 Astro Dynamics Inc Heat radiator
US3881547A (en) * 1973-11-12 1975-05-06 Varian Associates Heat transfer device employing fins in a fluid stream
US5304845A (en) * 1991-04-09 1994-04-19 Digital Equipment Corporation Apparatus for an air impingement heat sink using secondary flow generators
US20050241800A1 (en) * 2004-04-30 2005-11-03 Shankar Hegde Twin fin arrayed cooling device
US20060054311A1 (en) * 2004-09-15 2006-03-16 Andrew Douglas Delano Heat sink device with independent parts
US20060102320A1 (en) * 2004-11-12 2006-05-18 Asustek Computer Inc. Heat sink
US20090052138A1 (en) * 2007-08-21 2009-02-26 Ching-Sung Kuo Wing-spanning thermal-dissipating device
US20090218079A1 (en) * 2008-02-29 2009-09-03 Sanyo Denki Co., Ltd. Heat-emitting element cooling apparatus
US20140034278A1 (en) * 2012-08-01 2014-02-06 Asia Vital Components Co., Ltd. Heat sink structure and manufacturing method thereof
US20140034277A1 (en) * 2012-08-01 2014-02-06 Asia Vital Components Co., Ltd. Heat sink structure and method of manufacturing same
US10830545B2 (en) 2016-07-12 2020-11-10 Fractal Heatsink Technologies, LLC System and method for maintaining efficiency of a heat sink
US10852069B2 (en) 2010-05-04 2020-12-01 Fractal Heatsink Technologies, LLC System and method for maintaining efficiency of a fractal heat sink
US11031312B2 (en) 2017-07-17 2021-06-08 Fractal Heatsink Technologies, LLC Multi-fractal heatsink system and method
US11598593B2 (en) 2010-05-04 2023-03-07 Fractal Heatsink Technologies LLC Fractal heat transfer device

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR716972A (en) * 1931-04-29 1931-12-30 Improvements to the fins of heat exchangers
DE546836C (en) * 1932-03-17 Rudolf Fries Laengsrippenrohr, which is composed of individual longitudinal segments
GB371347A (en) * 1930-01-20 1932-04-19 Henry Dieterlen Improvements relating to tubulous boilers economisers, and like heat exchange apparatus
US2405317A (en) * 1943-04-29 1946-08-06 Mccollum Thelma Heater
US2430631A (en) * 1944-09-11 1947-11-11 Pacific Metals Company Ltd Heat transfer fin

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE546836C (en) * 1932-03-17 Rudolf Fries Laengsrippenrohr, which is composed of individual longitudinal segments
GB371347A (en) * 1930-01-20 1932-04-19 Henry Dieterlen Improvements relating to tubulous boilers economisers, and like heat exchange apparatus
FR716972A (en) * 1931-04-29 1931-12-30 Improvements to the fins of heat exchangers
US2405317A (en) * 1943-04-29 1946-08-06 Mccollum Thelma Heater
US2430631A (en) * 1944-09-11 1947-11-11 Pacific Metals Company Ltd Heat transfer fin

Cited By (26)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2694554A (en) * 1948-12-30 1954-11-16 Rca Corp Cooling unit
US2680009A (en) * 1953-02-25 1954-06-01 Rca Corp Cooling unit
US3147801A (en) * 1961-02-09 1964-09-08 Astro Dynamics Inc Heat radiator
US3881547A (en) * 1973-11-12 1975-05-06 Varian Associates Heat transfer device employing fins in a fluid stream
US5304845A (en) * 1991-04-09 1994-04-19 Digital Equipment Corporation Apparatus for an air impingement heat sink using secondary flow generators
US7497248B2 (en) * 2004-04-30 2009-03-03 Hewlett-Packard Development Company, L.P. Twin fin arrayed cooling device
US20050241800A1 (en) * 2004-04-30 2005-11-03 Shankar Hegde Twin fin arrayed cooling device
US20060054311A1 (en) * 2004-09-15 2006-03-16 Andrew Douglas Delano Heat sink device with independent parts
US20060102320A1 (en) * 2004-11-12 2006-05-18 Asustek Computer Inc. Heat sink
US20090052138A1 (en) * 2007-08-21 2009-02-26 Ching-Sung Kuo Wing-spanning thermal-dissipating device
US7905274B2 (en) * 2007-08-21 2011-03-15 Ching-Sung Kuo Wing-spanning thermal-dissipating device
US20090218079A1 (en) * 2008-02-29 2009-09-03 Sanyo Denki Co., Ltd. Heat-emitting element cooling apparatus
US10852069B2 (en) 2010-05-04 2020-12-01 Fractal Heatsink Technologies, LLC System and method for maintaining efficiency of a fractal heat sink
US11598593B2 (en) 2010-05-04 2023-03-07 Fractal Heatsink Technologies LLC Fractal heat transfer device
US11512905B2 (en) 2010-05-04 2022-11-29 Fractal Heatsink Technologies LLC System and method for maintaining efficiency of a fractal heat sink
US20140034278A1 (en) * 2012-08-01 2014-02-06 Asia Vital Components Co., Ltd. Heat sink structure and manufacturing method thereof
US9851158B2 (en) 2012-08-01 2017-12-26 Asia Vital Components Co., Ltd. Heat sink structure
US20140034277A1 (en) * 2012-08-01 2014-02-06 Asia Vital Components Co., Ltd. Heat sink structure and method of manufacturing same
US10830545B2 (en) 2016-07-12 2020-11-10 Fractal Heatsink Technologies, LLC System and method for maintaining efficiency of a heat sink
US11346620B2 (en) 2016-07-12 2022-05-31 Fractal Heatsink Technologies, LLC System and method for maintaining efficiency of a heat sink
US11609053B2 (en) 2016-07-12 2023-03-21 Fractal Heatsink Technologies LLC System and method for maintaining efficiency of a heat sink
US11913737B2 (en) 2016-07-12 2024-02-27 Fractal Heatsink Technologies LLC System and method for maintaining efficiency of a heat sink
US12339078B2 (en) 2016-07-12 2025-06-24 Fractal Heatsink Technologies LLC System and method for maintaining efficiency of a heat sink
US11031312B2 (en) 2017-07-17 2021-06-08 Fractal Heatsink Technologies, LLC Multi-fractal heatsink system and method
US11670564B2 (en) 2017-07-17 2023-06-06 Fractal Heatsink Technologies LLC Multi-fractal heatsink system and method
US12288731B2 (en) 2017-07-17 2025-04-29 Fractal Heatsink Technologies LLC Multi-fractal heatsink system and method

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