US3907028A - Concentric cylinder heat exchanger - Google Patents

Concentric cylinder heat exchanger Download PDF

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US3907028A
US3907028A US466351A US46635174A US3907028A US 3907028 A US3907028 A US 3907028A US 466351 A US466351 A US 466351A US 46635174 A US46635174 A US 46635174A US 3907028 A US3907028 A US 3907028A
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annular space
annular
adjacent
helical
fluid
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Drew B Lawson
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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F28HEAT EXCHANGE IN GENERAL
    • F28DHEAT-EXCHANGE APPARATUS, NOT PROVIDED FOR IN ANOTHER SUBCLASS, IN WHICH THE HEAT-EXCHANGE MEDIA DO NOT COME INTO DIRECT CONTACT
    • F28D7/00Heat-exchange apparatus having stationary tubular conduit assemblies for both heat-exchange media, the media being in contact with different sides of a conduit wall
    • F28D7/10Heat-exchange apparatus having stationary tubular conduit assemblies for both heat-exchange media, the media being in contact with different sides of a conduit wall the conduits being arranged one within the other, e.g. concentrically
    • F28D7/103Heat-exchange apparatus having stationary tubular conduit assemblies for both heat-exchange media, the media being in contact with different sides of a conduit wall the conduits being arranged one within the other, e.g. concentrically consisting of more than two coaxial conduits or modules of more than two coaxial conduits
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F28HEAT EXCHANGE IN GENERAL
    • F28DHEAT-EXCHANGE APPARATUS, NOT PROVIDED FOR IN ANOTHER SUBCLASS, IN WHICH THE HEAT-EXCHANGE MEDIA DO NOT COME INTO DIRECT CONTACT
    • F28D7/00Heat-exchange apparatus having stationary tubular conduit assemblies for both heat-exchange media, the media being in contact with different sides of a conduit wall
    • F28D7/02Heat-exchange apparatus having stationary tubular conduit assemblies for both heat-exchange media, the media being in contact with different sides of a conduit wall the conduits being helically coiled
    • F28D7/022Heat-exchange apparatus having stationary tubular conduit assemblies for both heat-exchange media, the media being in contact with different sides of a conduit wall the conduits being helically coiled the conduits of two or more media in heat-exchange relationship being helically coiled, the coils having a cylindrical configuration
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F28HEAT EXCHANGE IN GENERAL
    • F28DHEAT-EXCHANGE APPARATUS, NOT PROVIDED FOR IN ANOTHER SUBCLASS, IN WHICH THE HEAT-EXCHANGE MEDIA DO NOT COME INTO DIRECT CONTACT
    • F28D7/00Heat-exchange apparatus having stationary tubular conduit assemblies for both heat-exchange media, the media being in contact with different sides of a conduit wall
    • F28D7/10Heat-exchange apparatus having stationary tubular conduit assemblies for both heat-exchange media, the media being in contact with different sides of a conduit wall the conduits being arranged one within the other, e.g. concentrically
    • F28D7/12Heat-exchange apparatus having stationary tubular conduit assemblies for both heat-exchange media, the media being in contact with different sides of a conduit wall the conduits being arranged one within the other, e.g. concentrically the surrounding tube being closed at one end, e.g. return type
    • 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

Definitions

  • Field of the Invention- relates generally to heat exchangers and more particularly to concentric tube heat exchangers having waved, helical-shaped vanes.
  • a heat exchanger is a device that transfers heat from one fluid to another fluid..Large surface areas between fluids,- turbulence in the fluids, and fluids flowing in opposite directions enhance heat transfer.
  • the general purposes of the present invention are to provide a concentric tube heat exchanger that maximizes the surface area between fluids, causes fluids in adjacent annular spaces to flow in opposite directions, and creates turbulence in the fluids.
  • the present invention provides a plurality of concentric cylinders having annular spaces therebetween. Waved, helical-shaped vanes are disposed in the annular spacespManifolds at both ends of the concentric cylinders contain the required flow passages necessary to create opposite fluid flow in adjacent annular spaces.
  • one object of the present invention is to provide fluid flow in adjacent fluid flow paths in opposite directions.
  • Another object of the present invention is to induce turbulence in the field in all fluid flow paths.
  • Another object of the present invention is to maximize the surface area between adjacent fluid flow paths.
  • Another object of the present invention is to maximize heat exchange properties.
  • Another object of the present invention is to maximize the efficiency of heat exchange.
  • Another object of the present invention is to-provide improved and easier maintenance.
  • Another object of the present invention is to provide economy of fabrication and operation.
  • FIG. I is a specific embodiment of the present invention.
  • FIG. 1 shows a heat exchanger 10 having a cylindrical casing 12 and a series of concentric cylinders 14, I6, l8 20 and 22 enclosed therein.
  • Annular space 24 is formed between cylindrical casing 12 and concentric cylinder 14.
  • Annular spaces 26, 28, 30 and 32 are formed between concentric cylinders l4 and l6, l6 and 18, 18 and 20, and 20 and 22, respectively.
  • Annu lar space 34 is the innermost annular space and is formed by concentric cylinder 22.
  • Annular space 24 is the outermost annular space.
  • Manifolds 36 and 38 are connected to opposite ends of heat exchanger 10. Manifolds 36 and 38 provide in terconnections between annular spaces 24, 26, 28, 30, 32 and 34 so .thatfluid paths 40 and 42- are'defined. Note that fluid-path 40 is adjacent to and in an opposite direction from fluid path 42'. Fluid path 40 begins at inlet 44 in manifold 36 and terminatesat outlet 46 in" manifold 38. Fluid path 42 begins at inlet 48 in manifold 38 and terminates at outlet 50 in manifold 36.
  • manifolds j 36 and 38 connectevery other annular space in series to define fluidic'paths 40 and 42.
  • F165 2 is a'sectional view along lines 2-2 of FIG. 1.
  • FIG. 3 is a sectional view along lines 3 of FIG.
  • Fluid in fluid path 40 enters manifold 36 at inlet 44 and passes into annular space 24 through opening 72.
  • the fluid then passes down annular sp'ace 24 through manifoild 38Iof FIG. I and back down annular space 28.
  • The-flluidjthen passes through opening 74 and .76 in manifold 36 and into annular spaces 32.
  • the fluid in fluid path 42 enters manifold 38 at inlet 48 of FIG. I.
  • the fluid flows down annular space 26, enters manifold 36 at opening 78, and exits manifold 36 at opening. 80 into .annularspace 30.
  • the fluid then passesdown annularspace 30 through manifold 38 and back down annularspace 34.
  • the fluid then exits manifold 3a through outlet 50.
  • Manifold38 is constructed with the requisite opcnings in like manner to manifold 36. Also, additional concentric cylinders over the number shown in FIGS. 1, 2 and 3 may be utilized. Of course, larger manifolds with additional openings will be required in order to correctly define the proper fluid paths.
  • helical-shaped vane 70 having wave-shaped surfaces, and helical-shaped vane 72 are illustrated.
  • Wave-surfaced, helical-shaped vane is disposed in annular space 28 between concentric cylinders l6 and 18.
  • Helical-shaped vane 72 is disposed in annular space 30 between concentric cylinders 18 and 20.
  • vane 72 in annular space 30 proceeds in a clockwise direction, as noted by arrow 82, while vane 70 in adjacent annular space 28 proceeds in a counterclockwise direction, as noted by arrow 84. Placing the helical-shaped vanes in such manner creates a cross flow between the fluids in adjacent annular spaces.
  • Arrow 100 indicates the direction of flow of fluid in annular space 30.
  • Arrow 102 indicates the direction of flow of fluid in annular space 28.
  • the helical-shaped vanes create a large surface area over which fluids in adjacent annular spaces flow, thus increasing the efficiency of heat transfer between the fluids in adjacent annular spaces.
  • the wavesurfaced, helical-shaped vanes 70 impart turbulence to the fluid in annular space 28, thereby increasing the efficiency of heat transfer between the fluids in adjacent annular spaces to an even greater extent.
  • wave-surfaced, helical-shaped vanes are disposed in annular spaces 24, 26, 28, 30 and 32 of FIGS. 1, 2 and 3 to simplify the drawings.
  • Wavesurfaced, helical-shaped vane 70 in annular space 28 forms a fluid-tight seal at its top edge 90 with concentric cylinder 16 and its bottom edge 92 with concentric cylinder 18.
  • all helicalshaped vanes in heat exchanger 10 are so sealed to their respective concentric cylinders.
  • Arrow 104 indicates the direction of fluid flow in annular space 30 while arrow 106 indicates the direction of fluid flow in annular space 28.
  • helical-shaped vanes 70, 72, 74 and 76 illustrate methods of placement in annular spaces 24, 26, 28, 30, 32 and 34 of FIGS. 1, 2 and 3 of helicalshaped vanes to achieve various directions of flow between fluids in the adjacent annular spaces.
  • Wavesurfaced, helical-shaped vanes 74 and 76 are sealed at their edges to the concentric cylinders, forming the annular space in which they are disposed in like manner to vanes 70 and 72 of FIG. 4.
  • FIG. 1 includes such suitable and necessary fluidic sealing means as to render the specific embodiment operable.
  • fluidic sealing means are not illustrated in FIGS. 1, 2, 3, 4 or 5.
  • a concentric tube heat exchanger for transferring heat from one fluid to another fluid comprising:
  • a cylindrical casing having a first and a second end;
  • each pair of adjacent concentric cylinders having an annular space therebetween, each said cylinder having a first and a second end;
  • a plurality of helical-shaped vanes having continuously wave shaped surfaces contacting said fluid flowing thereby connected between adjacent concentric cylinders with one vane being disposed in each said annular space, each said vane being attached to each of its respective concentric cylinders along its entire length, said attachments providing fluid-tight seals with said concentric cylinders, said wave shaped surfaces of said helical vanes imparting turbulence to heat exchange fluids flowing through said annular spaces;
  • first and second manifold means connected to the first and second ends, respectively, of said cylindrical casing and to said plurality of concentric cylinders for creating a first and a second fluidic path through said annular spaces, said first fluidic path being between said first inlet means and said first outlet means, said second fluidic path being between said second inlet means and said second outlet means, said first fluidic path being formed by connecting every other annular space in series, starting from the annular space adjacent to the outermost annular space and proceeding to the innermost annular space, said second fluidic path being formed by connecting every other annular space in series, starting from the outermost annular space and proceeding to the annular space adjacent the innermost annular space.

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  • Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Thermal Sciences (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Heat-Exchange Devices With Radiators And Conduit Assemblies (AREA)

Abstract

A heat exchanger formed by a plurality of concentric tubes having annular spaces therebetween. Helical-shaped vanes having waves therein are disposed in the annular spaces. Interconnection means are provided to create fluidic paths through the annular spaces.

Description

United States Patent 1 Lawson [451 Sept. 23, 1975 CONCENTRIC CYLINDER HEAT EXCHANGER [75] Inventor: Drew B. Lawson, Los Gatos, Calif.
[73] Assignee: The United States of America as represented by the Secretary of the Navy, Washington, DC.
[22] Filed: May 2, 1974 [21] Appl. No.: 466,351
{52] US. Cl. 165/156; 165/141; 138/38 [51] Int. Cl. F28D 7/00 [58] Field of Search 165/140, 141, 156;
[56] References Cited UNITED STATES PATENTS 2,300.57) 11/1942 Lenning 138/38 X Carter 165/156 X Pearson 138/38 Primary ExaminerCharles J. Myhre Assistant E.\'aminerTheophil W. Streule, Jr. Attorney, Agent, or Firrr'1Rich1ard S. Sciascia; .I. M. St. Amand; D'arrell E. Hollis [57] ABSTRACT A heat exchanger formed by a plurality of concentric tubes having annular spaces therebetween. Helicalshaped vanes having waves therein are disposed in the annular spaces. Interconnection means are provided to create fluidic paths through the annular spaces.
3 Claims, 5 Drawing Figures I; ICONCENTRIC CYLINDER HEAT EXCHANGEIR STATEMENT OF GOVERNMENT INTEREST The invention described herein may be manufac tured and used by or for the Government of the United States of America for governmental purposeswithout the payment of any royalties thereon or therefor.
BACKGROUND OFTHE INVENTION 1. Field of the Invention- The presentinvention relates generally to heat exchangers and more particularly to concentric tube heat exchangers having waved, helical-shaped vanes.
2. Description ofthe Prior Art.
A heat exchanger is a device that transfers heat from one fluid to another fluid..Large surface areas between fluids,- turbulence in the fluids, and fluids flowing in opposite directions enhance heat transfer.
There are a wide variety of heat exchangers in the prior art utilizing one or more helical paths. However, such prior art heat exchangers are designed for quick disassembly or easy cleaning with heat transfer being a secondary consideration. Hence, such prior art heat exchangers do not maximize the surface areas between fluids, nor cause fluids to flow in Opposite directions or create turbulence in the fluids.
SUMMARY OF THE INVENTION The general purposes of the present invention are to provide a concentric tube heat exchanger that maximizes the surface area between fluids, causes fluids in adjacent annular spaces to flow in opposite directions, and creates turbulence in the fluids. To attain this, the present invention provides a plurality of concentric cylinders having annular spaces therebetween. Waved, helical-shaped vanes are disposed in the annular spacespManifolds at both ends of the concentric cylinders contain the required flow passages necessary to create opposite fluid flow in adjacent annular spaces.
Accordingly, one object of the present invention is to provide fluid flow in adjacent fluid flow paths in opposite directions. I
Another object of the present invention is to induce turbulence in the field in all fluid flow paths.
Another object of the present invention is to maximize the surface area between adjacent fluid flow paths.
Another object of the present invention is to maximize heat exchange properties.
Another object of the present invention is to maximize the efficiency of heat exchange.
Another object of the present invention is to-provide improved and easier maintenance.
Another object of the present invention is to provide economy of fabrication and operation.
Othef objects and a more complete appreciation of the present invention and itsmany attendant advantages will become apparent as the same becomes better understood by reference to the following detailed description when considered in conjunction with the accompanying drawings wherein like reference numerals refer to like parts throughout the figures thereof and wherein:
BRIEF DESCRIPTION OF THE DRAWINGS FIG. I is a specific embodiment of the present invention.
DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENT FIG. 1 shows a heat exchanger 10 having a cylindrical casing 12 and a series of concentric cylinders 14, I6, l8 20 and 22 enclosed therein. Annular space 24 is formed between cylindrical casing 12 and concentric cylinder 14. Annular spaces 26, 28, 30 and 32 are formed between concentric cylinders l4 and l6, l6 and 18, 18 and 20, and 20 and 22, respectively. Annu lar space 34 is the innermost annular space and is formed by concentric cylinder 22. Annular space 24 is the outermost annular space. I
Manifolds 36 and 38 are connected to opposite ends of heat exchanger 10. Manifolds 36 and 38 provide in terconnections between annular spaces 24, 26, 28, 30, 32 and 34 so .thatfluid paths 40 and 42- are'defined. Note that fluid-path 40 is adjacent to and in an opposite direction from fluid path 42'. Fluid path 40 begins at inlet 44 in manifold 36 and terminatesat outlet 46 in" manifold 38. Fluid path 42 begins at inlet 48 in manifold 38 and terminates at outlet 50 in manifold 36.
Note that adjacent annular spaces have fluids flowing in opposite' directions,"as indicated by arrows 52, 54,
56, 58, 60 and 62. As will be discussed supra, manifolds j 36 and 38 connectevery other annular space in series to define fluidic'paths 40 and 42.
Now turning to FIG;'2, fluid paths 40 and 42 are illustrated. F165 2 is a'sectional view along lines 2-2 of FIG. 1.
FIG. 3 is a sectional view along lines 3 of FIG.
1 illustrating manifold 36. Fluid in fluid path 40 enters manifold 36 at inlet 44 and passes into annular space 24 through opening 72. The fluid then passes down annular sp'ace 24 through manifoild 38Iof FIG. I and back down annular space 28. The-flluidjthen passes through opening 74 and .76 in manifold 36 and into annular spaces 32. The fluid then passes down annular space 32 throughmanifold 38 and =outlet 46 of FIG. 1. g
The fluid in fluid path 42 enters manifold 38 at inlet 48 of FIG. I. The fluid flows down annular space 26, enters manifold 36 at opening 78, and exits manifold 36 at opening. 80 into .annularspace 30. The fluid then passesdown annularspace 30 through manifold 38 and back down annularspace 34. The fluid then exits manifold 3a through outlet 50.
Manifold38 is constructed with the requisite opcnings in like manner to manifold 36. Also, additional concentric cylinders over the number shown in FIGS. 1, 2 and 3 may be utilized. Of course, larger manifolds with additional openings will be required in order to correctly define the proper fluid paths.
Now turning to FIG. 4, helical-shaped vane 70, having wave-shaped surfaces, and helical-shaped vane 72 are illustrated. Wave-surfaced, helical-shaped vane is disposed in annular space 28 between concentric cylinders l6 and 18. Helical-shaped vane 72 is disposed in annular space 30 between concentric cylinders 18 and 20.
Looking along the longitudinal axis of heat exchanger in the direction indicated by arrow 80 in FIG. 4, vane 72 in annular space 30 proceeds in a clockwise direction, as noted by arrow 82, while vane 70 in adjacent annular space 28 proceeds in a counterclockwise direction, as noted by arrow 84. Placing the helical-shaped vanes in such manner creates a cross flow between the fluids in adjacent annular spaces. Arrow 100 indicates the direction of flow of fluid in annular space 30. Arrow 102 indicates the direction of flow of fluid in annular space 28.
The helical-shaped vanes create a large surface area over which fluids in adjacent annular spaces flow, thus increasing the efficiency of heat transfer between the fluids in adjacent annular spaces. In addition, the wavesurfaced, helical-shaped vanes 70 impart turbulence to the fluid in annular space 28, thereby increasing the efficiency of heat transfer between the fluids in adjacent annular spaces to an even greater extent.
It is noted that wave-surfaced, helical-shaped vanes are disposed in annular spaces 24, 26, 28, 30 and 32 of FIGS. 1, 2 and 3 to simplify the drawings. Wavesurfaced, helical-shaped vane 70 in annular space 28 forms a fluid-tight seal at its top edge 90 with concentric cylinder 16 and its bottom edge 92 with concentric cylinder 18. Of course, in like manner, all helicalshaped vanes in heat exchanger 10 are so sealed to their respective concentric cylinders.
Nowturning to FIG. 5, wave-surfaced, helical-shaped vanes 74 and 76 in annular spaces 30 and 28, respectively, proceed in a clockwise direction, as noted by arrows 96 and 98, when looking along the longitudinal axis of heat exchanger 10 in the direction indicated by arrow 94. Placing the helical-shaped vanes in such manner creates a counter flow or opposite flow be tween the fluids in adjacent annular spaces. Arrow 104 indicates the direction of fluid flow in annular space 30 while arrow 106 indicates the direction of fluid flow in annular space 28.
It is noted that the clockwise, counter-clockwise placements of helical-shaped vanes 70, 72, 74 and 76 illustrate methods of placement in annular spaces 24, 26, 28, 30, 32 and 34 of FIGS. 1, 2 and 3 of helicalshaped vanes to achieve various directions of flow between fluids in the adjacent annular spaces. Wavesurfaced, helical-shaped vanes 74 and 76 are sealed at their edges to the concentric cylinders, forming the annular space in which they are disposed in like manner to vanes 70 and 72 of FIG. 4.
It will be appreciated by those skilled in the art that the specific embodiment of FIG. 1 includes such suitable and necessary fluidic sealing means as to render the specific embodiment operable. Such fluidic sealing means are not illustrated in FIGS. 1, 2, 3, 4 or 5.
Obviously, many modifications and variations of the present invention are possible in light of the above teachings. It is therefore to be understood that within the scope of the appended claims the invention may be practiced otherwise than as specifically described herein.
I claim:
1. A concentric tube heat exchanger for transferring heat from one fluid to another fluid comprising:
a. a cylindrical casing having a first and a second end;
b. a plurality of concentric cylinders located inside said cylindrical casing, each pair of adjacent concentric cylinders having an annular space therebetween, each said cylinder having a first and a second end;
c. a plurality of helical-shaped vanes having continuously wave shaped surfaces contacting said fluid flowing thereby connected between adjacent concentric cylinders with one vane being disposed in each said annular space, each said vane being attached to each of its respective concentric cylinders along its entire length, said attachments providing fluid-tight seals with said concentric cylinders, said wave shaped surfaces of said helical vanes imparting turbulence to heat exchange fluids flowing through said annular spaces;
d. first inlet means;
e. first outlet means;
f. second inlet means;
g. second outlet means;
h. first and second manifold means connected to the first and second ends, respectively, of said cylindrical casing and to said plurality of concentric cylinders for creating a first and a second fluidic path through said annular spaces, said first fluidic path being between said first inlet means and said first outlet means, said second fluidic path being between said second inlet means and said second outlet means, said first fluidic path being formed by connecting every other annular space in series, starting from the annular space adjacent to the outermost annular space and proceeding to the innermost annular space, said second fluidic path being formed by connecting every other annular space in series, starting from the outermost annular space and proceeding to the annular space adjacent the innermost annular space.
2. The concentric tube heat exchanger of claim 1 wherein said plurality of helical-shaped vanes are disposed eounter-clockwise in the annular spaces of both said first and second fluidic paths, thereby creating counter-flow of fluids in adjacent annular spaces.
3. The concentric tube heat exchanger of claim 1' wherein said plurality of helical-shaped vanes are disposed counterclockwise in the annular spaces defining said first fluidic path and clockwise in the annular spaces defining said second fluidic path, thereby creating cross counter-flow of fluids in adjacent annular spaces.
l i I i

Claims (3)

1. A concentric tube heat exchanger for transferring heat from one fluid to another fluid comprising: a. a cylindrical casing having a first and a second end; b. a plurality of concentric cylinders located inside said cylindrical casing, each pair of adjacent concentric cylinders having an annular space therebetween, each said cylinder having a first and a second end; c. a plurality of helical-shaped vanes having continuously wave shaped surfaces contacting said fluid flowing thereby connected between adjacent concentric cylinders with one vane being disposed in each said annular space, each said vane being attached to each of its respective concentric cylinders along its entire length, said attachments providing fluid-tight seals with said concentric cylinders, said wave shaped surfaces of said helical vanes imparting turbulence to heat exchange fluids flowing through said annular spaces; d. first inlet means; e. first outlet means; f. second inlet means; g. second outlet means; h. first and second manifold means connected to the first and second ends, respectively, of said cylindrical casing and to said plurality of concentric cylinders for creating a first and a second fluidic path through said annular spaces, said first fluidic path being between said first inlet means and said first outlet means, said second fluidic path being between said second inlet means and said second outlet means, said first fluidic path being formed by connecting every other annular space in series, starting from the annular space adjacent to the outermost annular space and proceeding to the innermost annular space, said sEcond fluidic path being formed by connecting every other annular space in series, starting from the outermost annular space and proceeding to the annular space adjacent the innermost annular space.
2. The concentric tube heat exchanger of claim 1 wherein said plurality of helical-shaped vanes are disposed counter-clockwise in the annular spaces of both said first and second fluidic paths, thereby creating counter-flow of fluids in adjacent annular spaces.
3. The concentric tube heat exchanger of claim 1 wherein said plurality of helical-shaped vanes are disposed counterclockwise in the annular spaces defining said first fluidic path and clockwise in the annular spaces defining said second fluidic path, thereby creating cross counter-flow of fluids in adjacent annular spaces.
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Cited By (27)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4228852A (en) * 1979-02-28 1980-10-21 Akira Togashi Tubular body
US4245697A (en) * 1976-05-24 1981-01-20 Akira Togashi Tubular body
US4263878A (en) * 1978-05-01 1981-04-28 Thermo Electron Corporation Boiler
US4275289A (en) * 1980-02-04 1981-06-23 Western Electric Company, Inc. Uniformly cooled plasma etching electrode
US4361749A (en) * 1980-02-04 1982-11-30 Western Electric Co., Inc. Uniformly cooled plasma etching electrode
US5000253A (en) * 1988-03-31 1991-03-19 Roy Komarnicki Ventilating heat recovery system
US5327740A (en) * 1991-11-18 1994-07-12 Ckd Corporation Dehumidifier
US5340664A (en) * 1993-09-29 1994-08-23 Ceramatec, Inc. Thermally integrated heat exchange system for solid oxide electrolyte systems
US5568835A (en) * 1995-07-25 1996-10-29 The Babcock & Wilcox Company Concentric heat exchanger having hydraulically expanded flow channels
US6092590A (en) * 1996-05-03 2000-07-25 Daimlerchrysler Aerospace Airbus Gmbh Method and evaporator device for evaporating a low temperature liquid medium
US6347453B1 (en) * 1998-05-22 2002-02-19 Matthew P. Mitchell Assembly method for concentric foil regenerators
US20020084065A1 (en) * 2001-01-04 2002-07-04 Tamin Enterprises Fluid heat exchanger
WO2002093099A1 (en) * 2001-05-12 2002-11-21 Robert Bosch Gmbh Heat exchanger for heating a product, in particular a mass for production of confectionery
US20050082032A1 (en) * 2000-08-10 2005-04-21 Kankyo Co., Ltd. Heat exchanger, a method for producing the same and a dehumidifier containing the same
US20050150640A1 (en) * 2004-01-09 2005-07-14 Ranga Nadig Double-tube apparatus for use in a heat exchanger and method of using the same
WO2010139620A1 (en) * 2009-06-04 2010-12-09 Wuest Manfred Preheating device for preheating liquid and/or gaseous fuel for an internal combustion engine
EP2063208A3 (en) * 2007-11-20 2011-04-27 Consarctic Entwicklungs- und Handels GmbH Heat exchanger
ITMO20100123A1 (en) * 2010-04-21 2011-10-22 Cft Spa HEAT EXCHANGER WITH CORRUGATED TUBES FOR FOOD PRODUCTS.
US20140083667A1 (en) * 2012-09-27 2014-03-27 Tai-Her Yang Tri-Piece Thermal Energy Body Heat Exchanger Having Multi-Layer Pipeline And Transferring Heat To Exterior Through Outer Periphery Of Pipeline
US20140174557A1 (en) * 2011-08-25 2014-06-26 The Boeing Company Stagnant Fuel Thermal Insulation System
US8833076B2 (en) 2010-06-24 2014-09-16 Aerojet Rocketdyne Of De, Inc. Thermal storage system
CN104534909A (en) * 2014-12-19 2015-04-22 合肥市百胜科技发展股份有限公司 Water-cooled jacket
US20150252823A1 (en) * 2014-03-07 2015-09-10 General Electric Company Fluidic buffer volume device with reduced mixedness
US20190024821A1 (en) * 2013-03-15 2019-01-24 Flowserve Management Company Fluid flow control devices and systems, and methods of flowing fluids therethrough
US10495384B2 (en) 2015-07-30 2019-12-03 General Electric Company Counter-flow heat exchanger with helical passages
US10782072B2 (en) * 2014-04-16 2020-09-22 Enterex America LLC Counterflow helical heat exchanger
EP4119879A1 (en) * 2021-07-13 2023-01-18 The Boeing Company Heat transfer device with nested layers of helical fluid channels

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2300579A (en) * 1936-09-03 1942-11-03 Servel Inc Refrigeration
US2847193A (en) * 1954-08-30 1958-08-12 Richard H Carter Heat exchanger
US3394736A (en) * 1966-02-21 1968-07-30 Acme Ind Inc Internal finned tube

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2300579A (en) * 1936-09-03 1942-11-03 Servel Inc Refrigeration
US2847193A (en) * 1954-08-30 1958-08-12 Richard H Carter Heat exchanger
US3394736A (en) * 1966-02-21 1968-07-30 Acme Ind Inc Internal finned tube

Cited By (44)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4245697A (en) * 1976-05-24 1981-01-20 Akira Togashi Tubular body
US4263878A (en) * 1978-05-01 1981-04-28 Thermo Electron Corporation Boiler
US4228852A (en) * 1979-02-28 1980-10-21 Akira Togashi Tubular body
US4275289A (en) * 1980-02-04 1981-06-23 Western Electric Company, Inc. Uniformly cooled plasma etching electrode
US4361749A (en) * 1980-02-04 1982-11-30 Western Electric Co., Inc. Uniformly cooled plasma etching electrode
US5000253A (en) * 1988-03-31 1991-03-19 Roy Komarnicki Ventilating heat recovery system
US5327740A (en) * 1991-11-18 1994-07-12 Ckd Corporation Dehumidifier
US5340664A (en) * 1993-09-29 1994-08-23 Ceramatec, Inc. Thermally integrated heat exchange system for solid oxide electrolyte systems
US5568835A (en) * 1995-07-25 1996-10-29 The Babcock & Wilcox Company Concentric heat exchanger having hydraulically expanded flow channels
US6263678B1 (en) 1996-05-03 2001-07-24 Daimlerchrysler Aerospace Airbus Gmbh Method of evaporating a low temperature liquid medium
US6092590A (en) * 1996-05-03 2000-07-25 Daimlerchrysler Aerospace Airbus Gmbh Method and evaporator device for evaporating a low temperature liquid medium
US6347453B1 (en) * 1998-05-22 2002-02-19 Matthew P. Mitchell Assembly method for concentric foil regenerators
US6745822B1 (en) * 1998-05-22 2004-06-08 Matthew P. Mitchell Concentric foil structure for regenerators
US7147036B2 (en) 1999-04-16 2006-12-12 Kankyo Co., Ltd. Heat exchanger, a method for producing the same and a dehumidifier containing the same
US20060124286A1 (en) * 1999-04-16 2006-06-15 Hidetoshi Ike Heat exchanger, a method for producing the same and a dehumidifier containing the same
US7025119B2 (en) * 2000-08-10 2006-04-11 Kankyo Co., Ltd. Heat exchanger, a method for producing the same and a dehumidifier containing the same
US20050082032A1 (en) * 2000-08-10 2005-04-21 Kankyo Co., Ltd. Heat exchanger, a method for producing the same and a dehumidifier containing the same
US20020084065A1 (en) * 2001-01-04 2002-07-04 Tamin Enterprises Fluid heat exchanger
WO2002093099A1 (en) * 2001-05-12 2002-11-21 Robert Bosch Gmbh Heat exchanger for heating a product, in particular a mass for production of confectionery
US6880623B2 (en) 2001-05-12 2005-04-19 Robert Bosch Gmbh Heat exchanger for heating a product, in particular a composition for producing candies
US20040089441A1 (en) * 2001-05-12 2004-05-13 Johannes Gierlings Heat exchanger for heating a product, in particular a composition for producing candies
US20050150640A1 (en) * 2004-01-09 2005-07-14 Ranga Nadig Double-tube apparatus for use in a heat exchanger and method of using the same
EP2063208A3 (en) * 2007-11-20 2011-04-27 Consarctic Entwicklungs- und Handels GmbH Heat exchanger
WO2010139620A1 (en) * 2009-06-04 2010-12-09 Wuest Manfred Preheating device for preheating liquid and/or gaseous fuel for an internal combustion engine
ITMO20100123A1 (en) * 2010-04-21 2011-10-22 Cft Spa HEAT EXCHANGER WITH CORRUGATED TUBES FOR FOOD PRODUCTS.
US8833076B2 (en) 2010-06-24 2014-09-16 Aerojet Rocketdyne Of De, Inc. Thermal storage system
US9677716B2 (en) * 2011-08-25 2017-06-13 The Boeing Company Stagnant fuel thermal insulation system
US20140174557A1 (en) * 2011-08-25 2014-06-26 The Boeing Company Stagnant Fuel Thermal Insulation System
US20140083667A1 (en) * 2012-09-27 2014-03-27 Tai-Her Yang Tri-Piece Thermal Energy Body Heat Exchanger Having Multi-Layer Pipeline And Transferring Heat To Exterior Through Outer Periphery Of Pipeline
US10119769B2 (en) 2012-09-27 2018-11-06 Tai-Her Yang Tri-piece thermal energy body heat exchanger having multi-layer pipeline and transferring heat to exterior through outer periphery of pipeline
US9719733B2 (en) * 2012-09-27 2017-08-01 Tai-Her Yang Tri-piece thermal energy body heat exchanger having multi-layer pipeline and transferring heat to exterior through outer periphery of pipeline
US11287059B2 (en) 2013-03-15 2022-03-29 Flowserve Management Company Fluid flow control devices and systems, and methods of flowing fluids therethrough
US20190024821A1 (en) * 2013-03-15 2019-01-24 Flowserve Management Company Fluid flow control devices and systems, and methods of flowing fluids therethrough
US10941878B2 (en) * 2013-03-15 2021-03-09 Flowserve Management Company Fluid flow control devices and systems, and methods of flowing fluids therethrough
US11761558B2 (en) 2013-03-15 2023-09-19 Flowserve Pte. Ltd. Fluid flow control devices and systems, and methods of flowing fluids therethrough
US9494174B2 (en) * 2014-03-07 2016-11-15 General Electric Company Fluidic buffer volume device with reduced mixedness
US20150252823A1 (en) * 2014-03-07 2015-09-10 General Electric Company Fluidic buffer volume device with reduced mixedness
US10782072B2 (en) * 2014-04-16 2020-09-22 Enterex America LLC Counterflow helical heat exchanger
CN104534909A (en) * 2014-12-19 2015-04-22 合肥市百胜科技发展股份有限公司 Water-cooled jacket
US10495384B2 (en) 2015-07-30 2019-12-03 General Electric Company Counter-flow heat exchanger with helical passages
US10989480B2 (en) 2015-07-30 2021-04-27 General Electric Company Counter-flow heat exchanger with helical passages
EP4119879A1 (en) * 2021-07-13 2023-01-18 The Boeing Company Heat transfer device with nested layers of helical fluid channels
US20230015392A1 (en) * 2021-07-13 2023-01-19 The Boeing Company Heat transfer device with nested layers of helical fluid channels
US11927402B2 (en) * 2021-07-13 2024-03-12 The Boeing Company Heat transfer device with nested layers of helical fluid channels

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