US3177936A - Fluted heat exchange tube with internal helical baffle - Google Patents

Fluted heat exchange tube with internal helical baffle Download PDF

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US3177936A
US3177936A US285733A US28573363A US3177936A US 3177936 A US3177936 A US 3177936A US 285733 A US285733 A US 285733A US 28573363 A US28573363 A US 28573363A US 3177936 A US3177936 A US 3177936A
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diametric
tube
tubes
heat exchange
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Walter Gustave
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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F28HEAT EXCHANGE IN GENERAL
    • F28FDETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
    • F28F1/00Tubular elements; Assemblies of tubular elements
    • F28F1/02Tubular elements of cross-section which is non-circular
    • F28F1/06Tubular elements of cross-section which is non-circular crimped or corrugated in cross-section
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F28HEAT EXCHANGE IN GENERAL
    • F28FDETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
    • F28F13/00Arrangements for modifying heat-transfer, e.g. increasing, decreasing
    • F28F13/06Arrangements for modifying heat-transfer, e.g. increasing, decreasing by affecting the pattern of flow of the heat-exchange media
    • F28F13/12Arrangements for modifying heat-transfer, e.g. increasing, decreasing by affecting the pattern of flow of the heat-exchange media by creating turbulence, e.g. by stirring, by increasing the force of circulation
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F28HEAT EXCHANGE IN GENERAL
    • F28FDETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
    • F28F9/00Casings; Header boxes; Auxiliary supports for elements; Auxiliary members within casings
    • F28F9/02Header boxes; End plates
    • F28F9/04Arrangements for sealing elements into header boxes or end plates
    • F28F9/06Arrangements for sealing elements into header boxes or end plates by dismountable joints

Definitions

  • the present invention relates to marine heat exchanger for engine coolant, and has for an object, among other objects and purposes, to provide a novel heat exchange unit for use in such engine cooling devices and systems as disclosed in my prior Patents 2,258,526, granted October 7, 1941, and 2,415,154, granted February 4, 1947.
  • finned cooling tubes increase the outside surface area
  • the inside surfaces remain plain and round or cylindrical so that as a whole such tubes have been found insufiicient to provide sufficiently increased external surface cooling area to the fresh water inside the tubes.
  • this available tubing has fins formed in a thread-like fashion which, when fastened to the bottom of the hull, are at right angles to the flow of the external cooling water over the tubes with the result that the flow over the external surfaces of the tubes is not desirably efficient since some of the particles of the water surrounding the fins are carried with the tubing at a reduced surface friction which diminishes the heat exchange.
  • a further object of the invention is to provide tubing of the smaller diameter referred to so that the same neatly fits to the bottom of the boat offering little drag or resistance to the speed of the boat.
  • a still further object of the invention is to provide in such a tubing a baffle or mixing device so constructed and arranged as to agitate the engine coolant water while flowing through the tubes in a manner to cause all of the engine coolant water flowing through the tubes to move toward and from the inner surfaces tubes for good heat exchange.
  • a still further object of the invention is to provide a novel form of baflle or mixing device that partitions the tubes into at least two stream passages of a tortuous or serpentine form for increasing the paths of the coolant water longitudinally from end-to-end of the tubes, which of the cooling.
  • FIGURE 1 is a side elevational view of an improved marine heat exchanger for engine coolants constructed in accordance with the present invention and shown as applied to a boat hull or keel indicated in broken lines.
  • FIGURE 2 is a bottom plan view of the same.
  • FIGURE 3 is an enlarged sectional view through one of the headers and one of the novel tubes showing a preferred form of tube mounting.
  • FIGURE 4 is a cross-sectional view taken through a preferred form of tubing.
  • FIGURE 5 is a view similar to FIGURE 4, showing a preferred form of bafiie or mixing device installed in the tube.
  • FIGURE 6 is a side elevational view of a blank from which a form of baffie or mixing device may be constructed in any desired length to accommodate the selected length of tubing.
  • FIGURE 7 is a partial side elevational view of a form of baffle or mixing device which may be constructed from such blank.
  • FIGURE 8 is a side elevational view of another form of baflle or mixing device in a completed stage.
  • FIGURE 9 is a fragmentary longitudinal sectional view of a tube taken on an enlarged scale and illustrating the application of the battle or mixing device to the internal structure of the tube.
  • FIGURE 10 is an end elevational view of the baffle according to FIGURE 7, taken from the left end thereof.
  • FIGURE 11 is an end elevational view of the form of baffle shown in FIGURE 8, taken from the left end thereof.
  • FIGURE 1 designates the hull or keel of a boat
  • 16, 17, 13 and 19 designate a cooling unit of four heat ex change tubes constructed in accordance wtih the preferred.
  • terminal header fittings 24 and 21 which are affixed to the boat by end supports 22 and 23.
  • Intermediate clamps 24 and 25 embrace the tube assembly and are also connected by bolts 26 or other fastenings beneath the keel or hull 15 of the boat so that the tubing and headers are exposed externally to the sea or other water.
  • a stem or stand pipe rises through the hull 15 from one of the headers 21.
  • this stand pipe are chambers 23 and 29 separated by a partition 30.
  • One of these chambers, for instance the chamber 28 receives hot water from the engine water jacket, which hot water is circulated through certain of the tubes from the header 21 to the header 20 and thereupon in a return flow.
  • adapters 31 arerprovided with outstanding flanges 33 adapted to abut against the ends of the headers at 'one side and to receive at the other side the-abutting ends of the tubing which is afiixed to the adapters and/ or to the,
  • the broken circular line 41 indicates the mean circumference of the tube, the external projections 35 and the internal projections 37 extending respectively outside and inside this circumferential line 41 in a configuration resembling a sine curve resulting in a Wave-like effect which is prob-ably best described as a fluted tube wall.
  • this preferred form of tube may be of any desired material and produced in any suitable manner, it is recommended that the tubes be seamless, thin-walled, for example of .025 inch thickness of Monel stainless corrosion resistant material. Such material will discourage barnacles and is of great strength. Initially a plain walled cylindrical tube of approximately 1 /2 inches outside diameter is selected and shaped or formed over a mandrel having an external wave-like pattern by rollers which reduce the diameter to approximately 1 /8 inches outside diameter.
  • This stock strip comprises generally an axial succession of diametric plates in any suitable number designated 44, 44 44 44, 44 44 44 et cetera, separated by an axial succession of twist joint strips 45, 45 45 45 45 45*, et cetera.
  • the plates 44, 44 et ceter-a are flat throughout their length and breadth or height in order to slidably fit into the diametric paths of internal grooves 38 of the tube,
  • the plates being of a Width or height approximately that of the length of the diametric line 39 illustrated in FIG- URE 4 with suitable tolerance to permit of the plate sliding freely'in the diametric pairs of grooves 38 into which it is initially slidably fitted.
  • the plate is flanked at both diametric opposed edges by internal projections 37 which therefore stabilize the plates against the reaction of the cooling water flowing through the tubes and in general hold the plates to alignment.
  • twist strips 45, 45 45*, et cetera which twist strips are of lesser wall width or have cut away portions 46 to clear the internal projections 37 of the tube at cross-over points to permit the twist strips 45, 45, etlcetera, to connect adjacent diametric plates 44, 44 et cetera, at theirrear and forward edges 51 and 52 respectively.
  • twist strips may be fashioned in any suitable form so as to join such rearand front edges 51 and 52,.
  • twist strips be comprised of leading sections 47, 4'7 47 et cetera, and trailing sections 48, 43 48 48 et cetera, in which the sections fl et cetera and .8 et cetera are approximately triangular in form, being joined together by hypotenuse lines of division 49.
  • the hypotenuse lines 49 are common to the pairs of triangles 47, 48 and 47 .48, et cetera, so that these triangular sections are in the form of mutual triangles.
  • FIGURE 11 three diametric plates 44 44 and 44 sutfice where the diametric plates are successively displaced angularly from one another through angles defined by every second diametric pair of internal grooves 38.
  • the numeral 59 indicates the free edge of the diametric plate 44, first or last in the order of succession.
  • the tubes fabricated as indicated or otherwise, are mounted between the headers and the heat exchanger fixed in place on a boat, being connected to the water cooling system of the engine in a circulation system.
  • the mixing baflies are of course inserted in the fluted tubes before the latter are mounted in the headers, or at least beforethe tubes are mounted in one of the headers.
  • Such bafi'les are introduced into the open ends of the tubes by axial sliding motion in which the leading diametric plate is fitted into selected diametric pairs of internal grooves 33.
  • the baffle is thereupon moved axially inward with the reduced diameter following twist strip entering the tube unimpeded by the internal projections 37 so that the next diametric plate will be correctly alined with the next diametric pair of internal grooves 38, or the next diametric pair of such internal grooves 38 as may be selected to receive the next diametric plate dependent upon the.
  • the device With the baffles in place and the tubes connected to both headers, the device is ready to receive streams of water in each tube separated by itsbaflle with the baffles imposing on the two streams tortuous or serpentine patterns of flow both in the same rotative direction, that is, clockwise or counterclockwise dependent upon whether viewed from one or the other end of the tube.
  • the heat exchanger is thus reduced in over-all dimensions, the tubes admit of closer grouping and of shorter lengthwhile maintaining adequate heat exchange. With the device the pressure drop is less with more heat exchange.
  • the tubing can be reduced, for instance from a length of ten inches to a length of six inches.
  • the mixing bafie may also be of Monel or other metal.
  • the twist strips impart the swirl pattern to the two streams on opposite sides of the battle or partition, while the diametric plates support the twist strips and stabilize such strips in position against the reaction of the Water currents.
  • the twist strips may also receive some support and orientation at cross-over points from the internal projections with which they may be in contacting relation.
  • FIGURE 8 With reference to FIGURE 8 in comparison with FIG- URE 11, it will be noted from FIGURE 11 that the length of the mixing bathe will extend from diametric plate 44 to the third plate in order 44 although FIGURE 8 shows an additional twist strip 47" 48 and an additional diametric plate 44 These last two elements have been added in FIGURE 8 to show that where the tube is longer than from 44 to 44 the sequence may begin all over with a twist strip 47*, 48* leading to the diametric plate 44 which corresponds in position and orientation with the initial diametric plate 44 The series of course may be added to, as indicated in FIGURE 6, any length desired.
  • the unit length 44 to 44 is much shorter in FIGURE 8 than the unit length 44 to 44 in FIGURE 7 due to the fact that the twist strips in FIGURE 8 go through a greater angle of turning because the plates are stepped through angles corresponding to two of the internal grooves 38 of the tube; whereas in FIGURES 7 and the twist strips are turned through the smaller angles between adjacent internal grooves 38.
  • FIGURE 9 corresponds to FIGURE 7 except that the scale is larger and FIGURE 9 is fragmentary.
  • the main purpose of my invention is to reduce the length and bulkiness of cooling tubes in an outboard marine engine cooling system. It is of utmost importance to obtain a simple and eflicient system as unobtrusive as possible.
  • the average modern motorboat, particularly the pleasure cruiser, is shorter and faster than its predecessor; its engine or engines are more powerful, thus, in order to fresh water cool this engine or engines, the cooling tubes of the outboard cooling systems must be more efl'icient to fit in a shorter space on the bottom of the boat hull and, at the same time, small enough in diameter to present minimum drag to the speed of the vessel.
  • a 1% inch diameter tube having a surface area of 4.71 square inches for every inch of length its diameter can be reduced to 1% inches without losing any cooling area, whereas the plain 1% inch diameter tubing has only 3.53 square inches area per inch of length or approximately 75% of the same diameter folded or fluted tube.
  • a marine engine requiring twenty feet of 1%; inch cooling tubes for proper heat exchange can thus be effectively cooled with fifteen feet of the same diameter folded or fluted tube.
  • this folded or fluted tube can be reduced by 25%, namely, from twenty to fifteen feet, the resistance to the flow of the water through this tubing is then also reduced. For instance, to circulate a large amount of cooling water through the engine jackets, then through the keel cooler,
  • a low pressure centrifugal circulating pump is best suited for this purpose.
  • a pump will cavitate an increasing amount of water as the resistance to the flow of water increases and volume of circulation diminishes. Assuming that the cross-sectional area of the cooling tubes does not restrict the volume of circulation, then the length of cooling tubes is of utmost importance.
  • a 25% reduction in the length of the cooling tubes will substantially decrease the resistance to the flow of. the cooling water through the cooling system and engine water jackets, resulting in a higher volume of cooling water circulation and additional cooling efliciency.
  • a heat exchange unit comprising (a) -a tube having (b) a fluted wall with (c) axially running circumferentially spaced external projections forming therebetween (d) external spaced grooves opening outwardly and (e) axially running circumferentially spaced internal projections forming therebetween internal spaced grooves opening inwardly,
  • a mixing baffle dividing the tube internally and 1ongitudinally comprising (k) an axial succession of diametric plates having side edge portions received in diametric pairs of the internal grooves and held by adjacent internal projections against angular shifting movements,
  • said strips comprising (p) leading and trailing triangular sections bent in relatively opposite directions along hypotenuse lines,

Description

G. WALTER A ril 13, 1965 FLUTED HEAT EXCHANGE TUBE WITH INTERNAL HELICAL BAFFLE 2 Sheets-Sheet 1 Filed June 5, 1963 FIG mu M W m 9 ATTORNEYS April '13, 1965 G. 'WA'LTER 3,177,936
FLUTED HEAT EXCHANGE .TUBE WITH INTERNAL HELICAL BAFFLE Filed June '5, 1963 2 Sheets-Sheet 2 INVENTOR. Gustave Walter ATTORNEYS United States atent Ofiice 3,177,935 Patented Apr. 13, 1965 3,177,936 FLUTED HEAT EXCHANGE TUBE WITH ETERNAL IELICAL RAFFLE Gustave Walter, Theme St., Jersey City, NJ. Filed June 5, 1963, Ser. No. 285,733 1 illaim. (Cl. 165-179) The present invention relates to marine heat exchanger for engine coolant, and has for an object, among other objects and purposes, to provide a novel heat exchange unit for use in such engine cooling devices and systems as disclosed in my prior Patents 2,258,526, granted October 7, 1941, and 2,415,154, granted February 4, 1947.
Those prior patents provided keel cooling systems for marine engines in which heat exchangers were afiixed beneath the hull of a boat involving closed fresh Water cooling systems to protect the marine engines from the contamination and corrosion of raw water.
With the development of more powerful engines and fast power boats, the length of cooling tubes necessary to provide suflicient heat exchange for these engines, when installed in fast but comparatively short boats, is becoming prohibitive to fit available lengths beneath the boats, which reduced lengths also have raised problems of fastening conventional long cooling tubes to the keel or other portions of the bottoms of the boats.
In order to increase the rate of heat exchange experiments have been made with commercially available finned cooling tubes with the purpose to decrease the lengths of the cooling tubes while at the same time increasing the heat exchange capacity of the tubing.
However, while such finned cooling tubes increase the outside surface area, the inside surfaces remain plain and round or cylindrical so that as a whole such tubes have been found insufiicient to provide sufficiently increased external surface cooling area to the fresh water inside the tubes. Furthermore, this available tubing has fins formed in a thread-like fashion which, when fastened to the bottom of the hull, are at right angles to the flow of the external cooling water over the tubes with the result that the flow over the external surfaces of the tubes is not desirably efficient since some of the particles of the water surrounding the fins are carried with the tubing at a reduced surface friction which diminishes the heat exchange.
It is the object and purpose of the invention to overcome the above diificulties by the development of a new form of tubing which admits of shorter length and smaller diameter while developing greater heat exchange capacity.
It is another object of the invention to provide fluted tubing in which the flutes on the tubing run lengthwise relatively to the movement of the tubes with the boat through the sea or other cooling water, thereby resulting in an efiicient flow of this cooling water over the surface of the tubing.
A further object of the invention is to provide tubing of the smaller diameter referred to so that the same neatly fits to the bottom of the boat offering little drag or resistance to the speed of the boat.
A still further object of the invention is to provide in such a tubing a baffle or mixing device so constructed and arranged as to agitate the engine coolant water while flowing through the tubes in a manner to cause all of the engine coolant water flowing through the tubes to move toward and from the inner surfaces tubes for good heat exchange.
A still further object of the invention is to provide a novel form of baflle or mixing device that partitions the tubes into at least two stream passages of a tortuous or serpentine form for increasing the paths of the coolant water longitudinally from end-to-end of the tubes, which of the cooling.
paths are in efiect therefore longer-than the lengths of such tubes.
With the foregoing and other objects in view, the. invention will be more fully described hereinafter, and will be more particularly pointed out in the claim appended hereto.
In the drawings, wherein like symbols refer to like or corresponding parts throughout the several views:
FIGURE 1 is a side elevational view of an improved marine heat exchanger for engine coolants constructed in accordance with the present invention and shown as applied to a boat hull or keel indicated in broken lines.
FIGURE 2 is a bottom plan view of the same.
FIGURE 3 is an enlarged sectional view through one of the headers and one of the novel tubes showing a preferred form of tube mounting.
FIGURE 4 is a cross-sectional view taken through a preferred form of tubing.
FIGURE 5 is a view similar to FIGURE 4, showing a preferred form of bafiie or mixing device installed in the tube.
FIGURE 6 is a side elevational view of a blank from which a form of baffie or mixing device may be constructed in any desired length to accommodate the selected length of tubing.
FIGURE 7 is a partial side elevational view of a form of baffle or mixing device which may be constructed from such blank.
FIGURE 8 is a side elevational view of another form of baflle or mixing device in a completed stage.
FIGURE 9 is a fragmentary longitudinal sectional view of a tube taken on an enlarged scale and illustrating the application of the battle or mixing device to the internal structure of the tube.
FIGURE 10 is an end elevational view of the baffle according to FIGURE 7, taken from the left end thereof.
FIGURE 11 is an end elevational view of the form of baffle shown in FIGURE 8, taken from the left end thereof.
Referring more particularly to the drawings, 15 in FIGURE 1 designates the hull or keel of a boat, and 16, 17, 13 and 19 designate a cooling unit of four heat ex change tubes constructed in accordance wtih the preferred.
form of the invention.
These tubes are fitted at their opposite ends into terminal header fittings 24 and 21 which are affixed to the boat by end supports 22 and 23. Intermediate clamps 24 and 25 embrace the tube assembly and are also connected by bolts 26 or other fastenings beneath the keel or hull 15 of the boat so that the tubing and headers are exposed externally to the sea or other water.
A stem or stand pipe rises through the hull 15 from one of the headers 21. In this stand pipe are chambers 23 and 29 separated by a partition 30. One of these chambers, for instance the chamber 28, receives hot water from the engine water jacket, which hot water is circulated through certain of the tubes from the header 21 to the header 20 and thereupon in a return flow.
adapters 31 arerprovided with outstanding flanges 33 adapted to abut against the ends of the headers at 'one side and to receive at the other side the-abutting ends of the tubing which is afiixed to the adapters and/ or to the,
flanges'33 by silver solder 34 or otherwise.
tudinally running circumferentially spaced internal pro-' jections 37 separated by internal grooves 38 which also run parallel with the axis of the tube. The internal groove diameter is indicated at, 39 and the internal projection diameter at 4%, from which it will be seen that the internal grooves 38 and the internal projections 37 are arranged in diametric pairs, which pairs are angularly displaced around the circumference of the tube.
The broken circular line 41 indicates the mean circumference of the tube, the external projections 35 and the internal projections 37 extending respectively outside and inside this circumferential line 41 in a configuration resembling a sine curve resulting in a Wave-like effect which is prob-ably best described as a fluted tube wall.
Although this preferred form of tube may be of any desired material and produced in any suitable manner, it is recommended that the tubes be seamless, thin-walled, for example of .025 inch thickness of Monel stainless corrosion resistant material. Such material will discourage barnacles and is of great strength. Initially a plain walled cylindrical tube of approximately 1 /2 inches outside diameter is selected and shaped or formed over a mandrel having an external wave-like pattern by rollers which reduce the diameter to approximately 1 /8 inches outside diameter.
It will be noted that the flutes of the tubing run lengthindicated in FIGURE 6 and cut off into desired lengths to accommodate the selected length of the tubing into which it is to be inserted. This stock strip comprises generally an axial succession of diametric plates in any suitable number designated 44, 44 44 44, 44 44 44 et cetera, separated by an axial succession of twist joint strips 45, 45 45 45 45 45*, et cetera.
The plates 44, 44 et ceter-a, are flat throughout their length and breadth or height in order to slidably fit into the diametric paths of internal grooves 38 of the tube,
the plates being of a Width or height approximately that of the length of the diametric line 39 illustrated in FIG- URE 4 with suitable tolerance to permit of the plate sliding freely'in the diametric pairs of grooves 38 into which it is initially slidably fitted. In this condition the plate is flanked at both diametric opposed edges by internal projections 37 which therefore stabilize the plates against the reaction of the cooling water flowing through the tubes and in general hold the plates to alignment.
As shown in FIGURES 7 and 10, successive plates 44, 44 44 44 44 and 44 are displaced angularly from one another about the axis of the tube in the order stated by the angles subtended by the various diametrie pairs of internal grooves 38 ofthe tube. Thus these diametric plates 44, 44 et cetera, are progressively stepped angularly around the circumference of the tube,
the same being connected together by the twist strips 45, 45 45*, et cetera, which twist strips are of lesser wall width or have cut away portions 46 to clear the internal projections 37 of the tube at cross-over points to permit the twist strips 45, 45, etlcetera, to connect adjacent diametric plates 44, 44 et cetera, at theirrear and forward edges 51 and 52 respectively. 7
While the twist strips may be fashioned in any suitable form so as to join such rearand front edges 51 and 52,.
of adjacent angularly disposed diametric plates 44, 44 et cetera, it is preferred that these twist strips be comprised of leading sections 47, 4'7 47 et cetera, and trailing sections 48, 43 48 48 et cetera, in which the sections fl et cetera and .8 et cetera are approximately triangular in form, being joined together by hypotenuse lines of division 49. The hypotenuse lines 49 are common to the pairs of triangles 47, 48 and 47 .48, et cetera, so that these triangular sections are in the form of mutual triangles.
These two triangular sections between each pair of diametric plates slope from the hypotenuse line 49 in substantially opposite directions to the edges 51 and 52 of the diametric plates so that the twist strips not only connect adjacent diametric plates which partake of no curvature but they also present to the streams of coolant water in the tube on opposite sides of the mixing baflie oflset inclined surfaces diverting and directing the coolant water from the core throughout all strata to and against the internal fluted walls of the tubes thereby bringing all portions of the internally circulating coolant into circulating contact with such walls at which maximum cooling elfect takes place.
From FIGURE 10 it appears that six of the diametric plates sufiice to comprehend the entire 360 degrees of the circle where twelve pairs of internal grooves 38 are embodied the tube wall.
in FIGURE 11 three diametric plates 44 44 and 44 sutfice where the diametric plates are successively displaced angularly from one another through angles defined by every second diametric pair of internal grooves 38.
In FIGURE 7 the numeral 59 indicates the free edge of the diametric plate 44, first or last in the order of succession.
In the use of the device the tubes, fabricated as indicated or otherwise, are mounted between the headers and the heat exchanger fixed in place on a boat, being connected to the water cooling system of the engine in a circulation system.
The mixing baflies are of course inserted in the fluted tubes before the latter are mounted in the headers, or at least beforethe tubes are mounted in one of the headers. Such bafi'les are introduced into the open ends of the tubes by axial sliding motion in which the leading diametric plate is fitted into selected diametric pairs of internal grooves 33. The baffle is thereupon moved axially inward with the reduced diameter following twist strip entering the tube unimpeded by the internal projections 37 so that the next diametric plate will be correctly alined with the next diametric pair of internal grooves 38, or the next diametric pair of such internal grooves 38 as may be selected to receive the next diametric plate dependent upon the.
amount of angular twist given the intermediate twist strip, thereupon'the lateral edges of this next diametric plate are entered into the diametric pair of internal grooves 38 presented thereto, it being understood that the relative angular positioning of the diametric plates will be such that each successive plate will accurately fit and easily slide in its designated diametric pair of grooves 38 with intermediate twist strips freely clearing the internal projections 37 at crossover points and between adjacent diametric pairs of internal grooves 38.
With the baffles in place and the tubes connected to both headers, the device is ready to receive streams of water in each tube separated by itsbaflle with the baffles imposing on the two streams tortuous or serpentine patterns of flow both in the same rotative direction, that is, clockwise or counterclockwise dependent upon whether viewed from one or the other end of the tube.
The heat exchanger is thus reduced in over-all dimensions, the tubes admit of closer grouping and of shorter lengthwhile maintaining adequate heat exchange. With the device the pressure drop is less with more heat exchange. The tubing can be reduced, for instance from a length of ten inches to a length of six inches.
The mixing bafie may also be of Monel or other metal.
The twist strips impart the swirl pattern to the two streams on opposite sides of the battle or partition, while the diametric plates support the twist strips and stabilize such strips in position against the reaction of the Water currents. The twist strips may also receive some support and orientation at cross-over points from the internal projections with which they may be in contacting relation.
With reference to FIGURE 8 in comparison with FIG- URE 11, it will be noted from FIGURE 11 that the length of the mixing bathe will extend from diametric plate 44 to the third plate in order 44 although FIGURE 8 shows an additional twist strip 47" 48 and an additional diametric plate 44 These last two elements have been added in FIGURE 8 to show that where the tube is longer than from 44 to 44 the sequence may begin all over with a twist strip 47*, 48* leading to the diametric plate 44 which corresponds in position and orientation with the initial diametric plate 44 The series of course may be added to, as indicated in FIGURE 6, any length desired.
The unit length 44 to 44 is much shorter in FIGURE 8 than the unit length 44 to 44 in FIGURE 7 due to the fact that the twist strips in FIGURE 8 go through a greater angle of turning because the plates are stepped through angles corresponding to two of the internal grooves 38 of the tube; whereas in FIGURES 7 and the twist strips are turned through the smaller angles between adjacent internal grooves 38.
FIGURE 9 corresponds to FIGURE 7 except that the scale is larger and FIGURE 9 is fragmentary.
The main purpose of my invention is to reduce the length and bulkiness of cooling tubes in an outboard marine engine cooling system. It is of utmost importance to obtain a simple and eflicient system as unobtrusive as possible. The average modern motorboat, particularly the pleasure cruiser, is shorter and faster than its predecessor; its engine or engines are more powerful, thus, in order to fresh water cool this engine or engines, the cooling tubes of the outboard cooling systems must be more efl'icient to fit in a shorter space on the bottom of the boat hull and, at the same time, small enough in diameter to present minimum drag to the speed of the vessel.
Therefore, by folding or fluting, a 1% inch diameter tube having a surface area of 4.71 square inches for every inch of length, its diameter can be reduced to 1% inches without losing any cooling area, whereas the plain 1% inch diameter tubing has only 3.53 square inches area per inch of length or approximately 75% of the same diameter folded or fluted tube. A marine engine requiring twenty feet of 1%; inch cooling tubes for proper heat exchange can thus be effectively cooled with fifteen feet of the same diameter folded or fluted tube. By folding or fluting a 1% inch diameter tube, as above mentioned, to 1% inch diameter, the cross-sectional area of this fluted tube is then approximately the same as that of the 1%: inch diameter plain tube. However, since the length of this folded or fluted tube can be reduced by 25%, namely, from twenty to fifteen feet, the resistance to the flow of the water through this tubing is then also reduced. For instance, to circulate a large amount of cooling water through the engine jackets, then through the keel cooler,
a low pressure centrifugal circulating pump is best suited for this purpose. However, such a pump will cavitate an increasing amount of water as the resistance to the flow of water increases and volume of circulation diminishes. Assuming that the cross-sectional area of the cooling tubes does not restrict the volume of circulation, then the length of cooling tubes is of utmost importance.
A 25% reduction in the length of the cooling tubes will substantially decrease the resistance to the flow of. the cooling water through the cooling system and engine water jackets, resulting in a higher volume of cooling water circulation and additional cooling efliciency.
Although I have disclosed herein the best forms of the invention known to me at this time, I reserve the right to all such modifications and changes as may come within the scope of the following claim.
What is claimed is: t
A heat exchange unit comprising (a) -a tube having (b) a fluted wall with (c) axially running circumferentially spaced external projections forming therebetween (d) external spaced grooves opening outwardly and (e) axially running circumferentially spaced internal projections forming therebetween internal spaced grooves opening inwardly,
(g) said external and internal projections being angularly displaced from one another,
(h) said external and internal grooves being also angularly displaced from one another,
(i) said internal grooves being relatively arranged in diametric pairs,
(j) a mixing baffle dividing the tube internally and 1ongitudinally comprising (k) an axial succession of diametric plates having side edge portions received in diametric pairs of the internal grooves and held by adjacent internal projections against angular shifting movements,
(I) said diametric pairs relatively displaced about the axis of the tube through successively greater angles, and
(m) twist joint strips joining adjacent plates,
(n) said strips being of reduced diameter compared to I the plates to snugly clear the internal projections at cross-over areas,
(0) said strips comprising (p) leading and trailing triangular sections bent in relatively opposite directions along hypotenuse lines,
' (q) said leading sections connected with the rear edges of the plates and sloped from the planes of the plates laterally of said planes,
(r) said trailing sections sloped from the hypotenuse lines to the forward edges of the next successive plates.
References Cited by the Examiner UNITED STATES PATENTS 2,079,144 5/37 Appa -179 2,258,526 10/41 Walter 165--44 2,847,953 8/58 Ernest 138-42 2,960,114 11/60 Hinde 13838 References Cited by the Applicant UNITED STATES PATENTS 493,376 3/93 Eaves. 2,864,405 12/58 Young.
CHARLES SUKALO, Primary Examiner.
US285733A 1963-06-05 1963-06-05 Fluted heat exchange tube with internal helical baffle Expired - Lifetime US3177936A (en)

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Cited By (33)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3446032A (en) * 1967-03-10 1969-05-27 Edward W Bottum Heat exchanger
US3561524A (en) * 1969-10-08 1971-02-09 Satterthwaite James G Marine keel cooler
US3920383A (en) * 1974-06-20 1975-11-18 Electric Furnace Co Fluted surface heat exchanger
US4004634A (en) * 1975-05-06 1977-01-25 Universal Oil Products Company Automotive oil cooler
US4040476A (en) * 1975-07-09 1977-08-09 The Johnson Rubber Company Keel cooler with spiral fluted tubes
US4043289A (en) * 1975-08-22 1977-08-23 The Walter Machine Company, Inc. Marine keel cooler
FR2361619A1 (en) * 1976-08-10 1978-03-10 Uop Inc Liquid cooled oil cooler for motor vehicles - has helically ribbed tube for coolant and annular oil flow path
US4086959A (en) * 1976-07-19 1978-05-02 Uop Inc. Automotive oil cooler
DE2916691A1 (en) 1979-04-25 1980-10-30 Bayerische Motoren Werke Ag COOLING DEVICE FOR LIQUID-COOLED COMBUSTION ENGINES, IN PARTICULAR FOR WATER VEHICLES WITH COMBINED LIQUID-SEAWATER COOLING OF THE COMBUSTION ENGINE
DE2954276C2 (en) * 1979-04-25 1985-06-13 Bayerische Motoren Werke AG, 8000 München Cooling device for internal combustion engines, in particular for watercraft drives
EP0181711A1 (en) * 1984-10-18 1986-05-21 A.O. Smith Corporation Heat exchanger having an improved turbulator construction
US5251452A (en) * 1992-03-16 1993-10-12 Cryoquip, Inc. Ambient air vaporizer and heater for cryogenic fluids
US5375654A (en) * 1993-11-16 1994-12-27 Fr Mfg. Corporation Turbulating heat exchange tube and system
US5590711A (en) * 1993-12-14 1997-01-07 Kabushiki Kaisha Kobe Seiko Sho Heat transfer tube for absorber
US5960870A (en) * 1997-01-27 1999-10-05 Kabushiki Kaisha Kobe Seiko Sho Heat transfer tube for absorber
US20030098141A1 (en) * 2001-11-27 2003-05-29 Fernstrum Todd S. Method and apparatus for enhancing the heat transfer efficiency of a keel cooler
US6575227B1 (en) * 1999-10-26 2003-06-10 Duramax Marine, Llc Heat exchanger
WO2003087691A1 (en) * 2002-04-09 2003-10-23 Duramax Marine, Llc Heat exchanger with beveled header
US20040079516A1 (en) * 2002-10-29 2004-04-29 Duramax Marine, Llc Keel cooler with fluid flow diverter
US20080148742A1 (en) * 2002-02-27 2008-06-26 Nierenberg Alan B Method and apparatus for the regasification of lng onboard a carrier
US20090145591A1 (en) * 2002-10-29 2009-06-11 Duramax Marine, Llc Keel cooler with fluid flow diverter
US7597599B1 (en) 2007-08-20 2009-10-06 Todd Boudreaux System for sealing a keel cooler to a vessel hull
US20100095905A1 (en) * 2008-10-16 2010-04-22 Lochinvar Corporation Gas Fired Modulating Water Heating Appliance With Dual Combustion Air Premix Blowers
US20100116225A1 (en) * 2008-10-16 2010-05-13 Lochinvar Corporation Integrated Dual Chamber Burner
US20100263389A1 (en) * 2009-04-17 2010-10-21 Excelerate Energy Limited Partnership Dockside Ship-To-Ship Transfer of LNG
US20110146594A1 (en) * 2009-12-22 2011-06-23 Lochinvar Corporation Fire Tube Heater
US9097436B1 (en) 2010-12-27 2015-08-04 Lochinvar, Llc Integrated dual chamber burner with remote communicating flame strip
US20160131122A1 (en) * 2014-11-12 2016-05-12 Leif Alexi Steinhour Convection pump and method of operation
US9464805B2 (en) 2013-01-16 2016-10-11 Lochinvar, Llc Modulating burner
US20170030652A1 (en) * 2015-07-30 2017-02-02 Senior Uk Limited Finned coaxial cooler
US9919774B2 (en) 2010-05-20 2018-03-20 Excelerate Energy Limited Partnership Systems and methods for treatment of LNG cargo tanks
US9957030B2 (en) 2013-03-14 2018-05-01 Duramax Marine, Llc Turbulence enhancer for keel cooler
US11774179B2 (en) 2017-06-22 2023-10-03 Rheem Manufacturing Company Heat exchanger tubes and tube assembly configurations

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US493376A (en) * 1893-03-14 William eaves
US2079144A (en) * 1935-06-17 1937-05-04 Reliable Refrigeration Co Inc Thermal fluid conduit and core therefor
US2258526A (en) * 1940-06-07 1941-10-07 Walter Gustave Engine cooling system
US2847953A (en) * 1956-04-13 1958-08-19 Meat Packers Equipment Co Flue for gas water heaters
US2864405A (en) * 1957-02-25 1958-12-16 Young Radiator Co Heat exchanger agitator
US2960114A (en) * 1957-04-26 1960-11-15 Bell & Gossett Co Innerfinned heat transfer tubes

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Publication number Priority date Publication date Assignee Title
US493376A (en) * 1893-03-14 William eaves
US2079144A (en) * 1935-06-17 1937-05-04 Reliable Refrigeration Co Inc Thermal fluid conduit and core therefor
US2258526A (en) * 1940-06-07 1941-10-07 Walter Gustave Engine cooling system
US2847953A (en) * 1956-04-13 1958-08-19 Meat Packers Equipment Co Flue for gas water heaters
US2864405A (en) * 1957-02-25 1958-12-16 Young Radiator Co Heat exchanger agitator
US2960114A (en) * 1957-04-26 1960-11-15 Bell & Gossett Co Innerfinned heat transfer tubes

Cited By (52)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3446032A (en) * 1967-03-10 1969-05-27 Edward W Bottum Heat exchanger
US3561524A (en) * 1969-10-08 1971-02-09 Satterthwaite James G Marine keel cooler
US3920383A (en) * 1974-06-20 1975-11-18 Electric Furnace Co Fluted surface heat exchanger
US4004634A (en) * 1975-05-06 1977-01-25 Universal Oil Products Company Automotive oil cooler
US4040476A (en) * 1975-07-09 1977-08-09 The Johnson Rubber Company Keel cooler with spiral fluted tubes
US4043289A (en) * 1975-08-22 1977-08-23 The Walter Machine Company, Inc. Marine keel cooler
US4086959A (en) * 1976-07-19 1978-05-02 Uop Inc. Automotive oil cooler
FR2361619A1 (en) * 1976-08-10 1978-03-10 Uop Inc Liquid cooled oil cooler for motor vehicles - has helically ribbed tube for coolant and annular oil flow path
DE2916691A1 (en) 1979-04-25 1980-10-30 Bayerische Motoren Werke Ag COOLING DEVICE FOR LIQUID-COOLED COMBUSTION ENGINES, IN PARTICULAR FOR WATER VEHICLES WITH COMBINED LIQUID-SEAWATER COOLING OF THE COMBUSTION ENGINE
DE2954276C2 (en) * 1979-04-25 1985-06-13 Bayerische Motoren Werke AG, 8000 München Cooling device for internal combustion engines, in particular for watercraft drives
EP0181711A1 (en) * 1984-10-18 1986-05-21 A.O. Smith Corporation Heat exchanger having an improved turbulator construction
US5251452A (en) * 1992-03-16 1993-10-12 Cryoquip, Inc. Ambient air vaporizer and heater for cryogenic fluids
US5375654A (en) * 1993-11-16 1994-12-27 Fr Mfg. Corporation Turbulating heat exchange tube and system
US5590711A (en) * 1993-12-14 1997-01-07 Kabushiki Kaisha Kobe Seiko Sho Heat transfer tube for absorber
US5960870A (en) * 1997-01-27 1999-10-05 Kabushiki Kaisha Kobe Seiko Sho Heat transfer tube for absorber
US6575227B1 (en) * 1999-10-26 2003-06-10 Duramax Marine, Llc Heat exchanger
US7044194B2 (en) 1999-10-26 2006-05-16 Duramax Marine, Llc Heat exchanger with beveled header
US7328740B2 (en) 1999-10-26 2008-02-12 Duramax Marine, Llc Heat exchanger with beveled header
US20060201652A1 (en) * 1999-10-26 2006-09-14 Duramax Marine, Llc Heat exchanger with beveled header
US20030098141A1 (en) * 2001-11-27 2003-05-29 Fernstrum Todd S. Method and apparatus for enhancing the heat transfer efficiency of a keel cooler
US7055576B2 (en) 2001-11-27 2006-06-06 R.W. Fernstrum & Co. Method and apparatus for enhancing the heat transfer efficiency of a keel cooler
US20080148742A1 (en) * 2002-02-27 2008-06-26 Nierenberg Alan B Method and apparatus for the regasification of lng onboard a carrier
US20100192597A1 (en) * 2002-02-27 2010-08-05 Excelerate Energy Limited Partnership Method and Apparatus for the Regasification of LNG Onboard a Carrier
WO2003087691A1 (en) * 2002-04-09 2003-10-23 Duramax Marine, Llc Heat exchanger with beveled header
US6896037B2 (en) 2002-10-29 2005-05-24 Duramax Marine, Llc Keel cooler with fluid flow diverter
US7201213B2 (en) 2002-10-29 2007-04-10 Duramax Marine, Llc Keel cooler with fluid flow diverter
US20070187066A1 (en) * 2002-10-29 2007-08-16 Duramax Marine, Llc - A Limited-Liability Corporation Of The State Of Ohio Keel cooler with fluid flow diverter
US20040079516A1 (en) * 2002-10-29 2004-04-29 Duramax Marine, Llc Keel cooler with fluid flow diverter
US7481262B2 (en) 2002-10-29 2009-01-27 Duramax Marine, Llc Keel cooler with fluid flow diverter
US20090145591A1 (en) * 2002-10-29 2009-06-11 Duramax Marine, Llc Keel cooler with fluid flow diverter
US8376029B2 (en) 2002-10-29 2013-02-19 Duramax Marine, Llc Keel cooler with fluid flow diverter
US20050205237A1 (en) * 2002-10-29 2005-09-22 Leeson Jeffrey S Keel cooler with fluid flow diverter
US7597599B1 (en) 2007-08-20 2009-10-06 Todd Boudreaux System for sealing a keel cooler to a vessel hull
US8286594B2 (en) 2008-10-16 2012-10-16 Lochinvar, Llc Gas fired modulating water heating appliance with dual combustion air premix blowers
US20100116225A1 (en) * 2008-10-16 2010-05-13 Lochinvar Corporation Integrated Dual Chamber Burner
US20100095905A1 (en) * 2008-10-16 2010-04-22 Lochinvar Corporation Gas Fired Modulating Water Heating Appliance With Dual Combustion Air Premix Blowers
US8517720B2 (en) 2008-10-16 2013-08-27 Lochinvar, Llc Integrated dual chamber burner
US8807092B2 (en) 2008-10-16 2014-08-19 Lochinvar, Llc Gas fired modulating water heating appliance with dual combustion air premix blowers
US20100263389A1 (en) * 2009-04-17 2010-10-21 Excelerate Energy Limited Partnership Dockside Ship-To-Ship Transfer of LNG
US20110146594A1 (en) * 2009-12-22 2011-06-23 Lochinvar Corporation Fire Tube Heater
US8844472B2 (en) 2009-12-22 2014-09-30 Lochinvar, Llc Fire tube heater
US9919774B2 (en) 2010-05-20 2018-03-20 Excelerate Energy Limited Partnership Systems and methods for treatment of LNG cargo tanks
US9097436B1 (en) 2010-12-27 2015-08-04 Lochinvar, Llc Integrated dual chamber burner with remote communicating flame strip
US9464805B2 (en) 2013-01-16 2016-10-11 Lochinvar, Llc Modulating burner
US10208953B2 (en) 2013-01-16 2019-02-19 A. O. Smith Corporation Modulating burner
US9957030B2 (en) 2013-03-14 2018-05-01 Duramax Marine, Llc Turbulence enhancer for keel cooler
US10179637B2 (en) 2013-03-14 2019-01-15 Duramax Marine, Llc Turbulence enhancer for keel cooler
US20160131122A1 (en) * 2014-11-12 2016-05-12 Leif Alexi Steinhour Convection pump and method of operation
US9702351B2 (en) * 2014-11-12 2017-07-11 Leif Alexi Steinhour Convection pump and method of operation
US20170030652A1 (en) * 2015-07-30 2017-02-02 Senior Uk Limited Finned coaxial cooler
US11029095B2 (en) * 2015-07-30 2021-06-08 Senior Uk Limited Finned coaxial cooler
US11774179B2 (en) 2017-06-22 2023-10-03 Rheem Manufacturing Company Heat exchanger tubes and tube assembly configurations

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