[go: up one dir, main page]

US2532288A - Heat exchange unit - Google Patents

Heat exchange unit Download PDF

Info

Publication number
US2532288A
US2532288A US678464A US67846446A US2532288A US 2532288 A US2532288 A US 2532288A US 678464 A US678464 A US 678464A US 67846446 A US67846446 A US 67846446A US 2532288 A US2532288 A US 2532288A
Authority
US
United States
Prior art keywords
disk
vanes
tube
exchanger
disks
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Lifetime
Application number
US678464A
Inventor
Herman F Buschow
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Hydrocarbon Research Inc
Original Assignee
Hydrocarbon Research Inc
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Hydrocarbon Research Inc filed Critical Hydrocarbon Research Inc
Priority to US678464A priority Critical patent/US2532288A/en
Application granted granted Critical
Publication of US2532288A publication Critical patent/US2532288A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • 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
    • F28F1/10Tubular elements and assemblies thereof with means for increasing heat-transfer area, e.g. with fins, with projections, with recesses
    • F28F1/42Tubular elements and assemblies thereof with means for increasing heat-transfer area, e.g. with fins, with projections, with recesses the means being both outside and inside the tubular element
    • 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
    • F28F1/10Tubular elements and assemblies thereof with means for increasing heat-transfer area, e.g. with fins, with projections, with recesses
    • F28F1/42Tubular elements and assemblies thereof with means for increasing heat-transfer area, e.g. with fins, with projections, with recesses the means being both outside and inside the tubular element
    • F28F1/422Tubular elements and assemblies thereof with means for increasing heat-transfer area, e.g. with fins, with projections, with recesses the means being both outside and inside the tubular element with outside means integral with the tubular element and inside means integral with the tubular element

Definitions

  • the present invention relates to an improved exchanger for recovering the cold content of the outgoing oxygen and nitrogen products of rectiflcation, which may be at a temperature of about 280 F., in the production of oxygen by the liquefaction and rectification of air, and more particularly to the construction and design of the cold exchangesurface areas providing for high cold transfer emclency between the oxygen and nitrogen products of rectification on the one hand and the air on the other.
  • Cold accumulators or regenerators (hereinafter referred to as cold exchangers) of large cold-absorbing capacity are well known.
  • cold exchangers the relatively warm incoming air and the relatively cold outgoing oxygen and nitrogen products of rectification are alternately passed with periodically reversed opi eration. so that streams of warm air are flowed through the same packing-filled spaces as, the
  • the high-boiling impurities deposited in these spaces during the passage of the air therethrough being removed therein a large number of tubes each provided with an interior accordion fin of foil-like metal and high heat conductivity disposed to form channels extending longitudinally through the tube and a somewhat similaraccordion fin on the exterior thereof.
  • These fins are usually made by folding thin sheets of copper into shape to produce the desired channels, and then bonding them to the interior and exterior walls of the tubes by coating these walls with soldering metal,
  • Another object is to provide a fin member 7 Claims. (Cl. 257-228) 2 r i which canreadily be produced, for example, by a simple stamping operation, and this without waste of heat-conducting metal, and which can readily be assembled within a tubular unit to produce longitudinally extending channels for turbulent flow of gaseous media.
  • Still another object is to provide such exchanger which is more efficient in operation in that the cold transfer rate is considerably greater than in prior known exchangers.
  • Fig. 1 is a fragmentary (one-quarter) plan view of a preferred form of disk which may be arranged with other like disks to produce a fin for the interior of a tubular unit of a coldexchanger embodying this invention;
  • Fig. 2 is an enlarged section taken in a plane normal to the disk fin and passing through line 2-2 ofFig.1;
  • Fig. 3 is a fragmentary (one-quarter) plan view of a preferred form of disk which may be arranged with other like disks to. produce a fin on the exterior of atubular exchanger unit embodying this invention; r
  • Fig. 3A is a fragmentary plan view of the disk of Fig. 3 showing the disk' as it appears after being cut from a foil-like sheet of metal and prior to the bending of the flanges and twisting of the vanes; i
  • Fig. 4 is an enlarged section taken. in a plane normal to thefin and passing through line H of Fig. 3; r l
  • Fig. 5 is a diagrammatic section through a preferred form of exchanger unit embodying this invention.
  • Fig. 6 is a fragmentary and diagrammatic vertical section through the exchanger unit of Fig. 5 taken through line 6-6 of Fig. 5;
  • Fig. 7 is a diagrammatic section through a modified form of exchanger unit embodying this invention.
  • Fig. 8 is a fragmentary and diagrammatic vertical section taken through line 8-8 of Fig. 7;
  • Fig. 9 is a diagrammatic sectionthrough a cold exchanger embodying this invention, involving a bundle or stack of the units of Figs/5 and 6;
  • Fig. 10 is a diagrammatic section through a cold exchanger embodying this invention, in-
  • Fig. 11 is a diagrammatic section through still another modified form of exchanger unit embodying this invention.
  • Fig. 12 is a fragmentary and diagrammatic vertical section through the exchanger unit of Fig. 11 taken through line I2--I2 cf Fig. 11;
  • Fig. 13 is a composite view of a cold exchanger embodying this invention, the lower half being a vertical section through the exchanger and the upper half a front elevation.
  • the cold exchange fin embodying this invention may be formed on the interior or exterior, or both the interior and exterior, of a tube such as the oxygen, nitrogen or air tubes of a cold exchanger of the type disclosed and claimed in the Scheibel application Serial No. 641,276, filed January 15, 1946. Also such fins may be employed in the unit of the cold exchanger disclosed more fully in copending application of Keith, Serial No. 676,142, which unit involves two concentric tubes each provided with longitudinally extending channels for flow of gaseous media.
  • such fins are made by assembling a multiplicity of platelike members or disks by simply stacking them in desired relation on the interior or exterior of the tube, as hereinafter more fully described.
  • Each plate-like member or disk may be made by stamping or otherwise shaping a foil-like sheet,
  • the disks II are disposed within tube In so that flange I2 on one disk substantially abuts the face of a contiguous disk within the tube III.
  • Fin 29 on the exterior of tube In is shown in detail in Figs. 3, 3A and 4. It is formed preferably of copper of foil-like thickness, say from .005 to .020" thick, and produced by a simple stamping operation. Each disk 29 has an interior circular outline 30 ada ted to conform to the shape of the tube III on which it is mounted, the interior edge 30 having an integral flange 3
  • the opposite edge 32 of the disk is preferably of polygonal shape, e. g., a hexagonal shape as shown in Figs. 3 and 5. Edge 32 is provided with an integral flange 33.
  • the face of the disk is out along pairs of closely spaced lines 34 and 35, and the material between these lines deflected or twisted about points 38 and 31, as pivots, to produce bafiies 38 which, as shown in Fig. 3, are at right angles to the plane of the disk fin 29.
  • baffles 38 as well as baffles 2I and 24 Each disk II has an integral flange I2 on the periphery thereof and has in the face thereof two series I3 and I4 of radially-disposed closelyspaced passages I5 and I6.
  • the two series of passa es I5 and I6 are se arated bv a flat area or portion ll of the disk of substantially circular outline. as indicated in Fig. 1.
  • the passages I5 are each formed by cutting the disk along pairs of substantially radially disposed lines I8 and I9, and then deflecting or twisting the material between each pair of lines so as to move this material out of the plane of the disk about points 2n as nivots.
  • each disk is preferably shaped to provide a circ lar flange 26 defining a central relatively small circular opening 27 the cross sectional area of which is substantiallv less than that of the passages I5.
  • the flange 26 defining this opening 21 increases the metal surface over which the gas sweeps and im roves the heat transfer between the gas passing through the tube in which the disks are disposed and that passing outside of the tube of each unit forming the heat exchanger of this invention.
  • each of the disks I I may easily be fabricated by a simple stamping and cutting operation in which the radial cuts IB, I9, 22 and 23 are first produced, thenthe material thereof disk fin II may be set at an angle of from to 90 with the plane of the disks.
  • the bafiies are set at an angle of at least 85 with the plane of the disk.
  • the cuts 34 and 35 have a slight curvature at their ends but straight cuts are frequent y employed.
  • 24 and 38 are shown as perfectlv flat members attached to their respective disks at their ends. However, these vanes are usually not perfectly flat since they have volutes at their ends produced when the vanes are twisted out of the plane of the disks.
  • An economy of material may be effected by producing the disks I I form ng the fin for the interior of tube I0 and the disks 29 forming the fin for the exterior of the t be from the Same sheet of copper or other foil-like material of high heat conducting prop rties, the disks II being I formed from the material req ir d to produce the circular opening 30 in the disks 29.
  • a multiplicitv of disks 29 are assembled on the exterior of tube I0 so that the flange 3
  • the disks II may be readily dispo ed in the interior of the tube I0 by simply stacking them within the tube, it being only neces ary to drop stantially the same as the external diameter of tube 1 ll. Since the disks are of foil-like metal of high heat conductivity, preferably copper, the
  • the flange of the disk or 'plate-' like fin which contacts the walls of the tubular member may be incised to permit contraction of interior fins or expansion of exterior fins.
  • disk ll such a cut would be made between any two baffies 2
  • a tubular unit is shown forming one unit of a cold exchanger of the type disclosed in the aforesaid Keith application.
  • This unit comprises a pair oi concentric tubes 39 and 40.
  • Inner tube 39 has the ein a cold exchange fin 4
  • Outer tube 40 has on the exterior thereof a fin 42 produced in the same manner as the fin 29 on the exterior of tube in, i. e., by stacking disks 42 on tube 40 with the iiange of one disk abutting the face of a contiguous disk.
  • a fin 43 Disposed in the annular space between tubes 39 and 40 is a fin 43 formed, for example, by folding, for each section of tube length, a strip of foil-like copper into the shape shown in Fig. 7 to provide alternate portions in contact with the inner wall of tube 40 and the outer wall of tube 39 connected by inclined portions, thereby forming two sets of substantially triangular longitudinally extending channels 44 and 45.
  • Each strip of foil-like copper so folded may be approximately 2" wide and adjacent sections of folded strips 43 are preferably separated by narrow spaces or slots 46 to induce turbulence of the gas flowing through the longitudinally extending channels 44 and 45.
  • the exchanger units of Figs. 5 and 6 are assembled with other like units in a stack or bundle in a shell 47 (Fig. 9) provided with headers, as more fully disclosed in the aforesaid Scheibel copending application.
  • the individual units within the shell 41 are in metal-to-metal contact with one another since the peripheries of the fins on the exterior thereof are disposed with metal-to-metal contact.
  • the spaces between the units and the interior wall of the shell may be filled with packing 48, e. g., crumpled aluminum foil or wood blocks.
  • the shell if desired, may be made closefitting, relative to the tube bundle, thereby eliminating such packing.
  • the exchanger units of Figs. 7 and 8 are assembled with other like units in a stack or bundle in a shell 41 (Fig. 10) provided with headers, as more fully disclosed in the aforesaid Keith copending application as shown in Fig. 13.
  • the individual units in the bundle of Figs. 10 and 13 have a small clearance between the peripheries of the fins on the exterior thereof, or may be in metal-tmmetal contact.
  • flanges are flexible, i. e., have a certain amount of 6
  • the annular fin 43 of folded strips of foil-like metal may be replaced by fins of the disk type where the annular space between the concentric tubes is appreciable, say over about one-half inch.
  • Such construction is shown in Figs. 11 and 12 in which 58 indicates an interior tube of high heat conductivity of smaller diameter than tube 39 of Figs. 7 and 8 thereby providing a larger annular space between inner tube and exterior tube 49.
  • Stacked on the exterior of tube 40, as in the case of Figs. 7 and 8, are a multiplicity of disks 42 with the flange of one disk abutting the face of a contiguous disk.
  • a multiplicity ofdisks 54 each having flanges 52, 53 along the a two edges thereof, flange 52 of each disk being bonded, if desired, to the exterior of tube 59 and flange 53 to the interior wall of tube 40.
  • Disks 54 are each provided with a series of radially disposed passages defined by vanes 5
  • Stacked within the interior of tube 50 is a multiplicity of disks 55 with the flange of one disk in substantially abutting relation with the face of a contiguous disk as hereinabove more fully described in connection with the constructions of Figs. 5 to 8, inclusive. 7
  • Fig. 13 shows a preferred header and associated port arrangement for the exchanger units of .Figs. 7 and 8.
  • the shell 41 is provided at each end with (1) an oxygen header 56 communicating with through ports 51 with a manifold 58 which is provided with a port 59, (2) a header 50 communicating with the channels formed on the exterior of tubes 40 by disks 42 and through ports 6
  • headers 60, 64, respectively take place through headers 60, 64, respectively, and upon reversal during the subsequent cycle of operation the flows of air and nitrogen, as indicated by the dotted line arrows, take place through the headers 54 and 50, respectively. Oxygen flows continuously through headers 55.
  • the longitudinally extending passages produced by the disks when assembled within and without the tubes provide a symmetrical path for cold exchange between the air, the oxygen and nitrogen products of rectification flowing through each exchanger since, with the flns of this invention, these longitudinally extending passages are all disposed substantially radially relative to the tubes with which they are associated. This results in such greatly improved cold transfer between the gaseous media that it is not neces-' sary to use copper tubes, but less expensive nickel steel tubes may be used and still obtain satisfacwry cold exchange.
  • the use of nickel steel tubes in an exchanger having a nickel steel shell eliminates the necessity of providing such shell with expansion joints.
  • the disk fin II may be made with a singleceptionally high surface area of heat transfer surface per unit of volume of exchanger space may be made with the fins of this invention.
  • the exchanger may have from 300 to 500 square feet of exchanger surface per cubic foot of exchanger volume.
  • the exchanger is, therefore, of exceptionally high cold transfer efiiciency. This makes it possible to have the volumetric space through which nitrogen on the one hand and air on the other flows relatively small, thereby minimizing reversal losses. Moreover, the flow through the interior of the tubes and in the channels defined by the fins on the exterior of the tubes takes place in a general longitudinal direction; hence, minimum pressure drop of fluid flowing therethrough occurs.
  • a heat exchanger fin comprising a platelike member of foil-like thickness of high heat conducting material having a central opening defined by an integral flange, a second integral flange on the periphery thereof and having in the face thereof a multiplicity of closely-spaced passages formed by cutting the plate-like member along closely spaced lines disposed substantially radially of said central opening and defleeting the material between contiguous lines to provide vanes defining the side walls of said passages, each of said vanes extending substantially equidistantly above and below the original plane of said plate-like member and having the opposite terminal ends thereof integral with the said flanges, substantially the entire surface of the face of said plate-like member being thus deflected without waste to roduce said vanes and being thus utilized as a heat exchange surface, said member adapted to be stacked with at least one of said flanges of each member except one terminal member in substantially abutting relationship with the face of a contiguous member to provide a relatively large mass of high heat conducting material per
  • a heat exchanger fin comprising a disk from .005" to .020" thick of high heat conducting material, said disk having a central opening adapted to flt over a tube, an integral flange on the periphery thereof, a second integral flange defining said central opening and having in the face thereof a series of closely spaced passages disposed radially relative to said central opening, said passages being formed by cutting said disk along closely spaced lines disposed substantially radially of said central opening and deflecting the material between contiguous lines to provide vanes defining the sidewalls of said passages, each of said vanes extending substantially equidistantly above and below the original plane of said disk and having the opposite terminal ends thereof integral with said flanges, substantially the entire surface of the face of said disk being thus deflected without waste to produce said vanesand being thus utilized as a heat exchange surface, said disk adapted to be stacked with at least one of said flanges of each disk except one terminal disk in substantially abutting relationship with the
  • a heat exchanger fin comprising a plate of foil-like thickness of high heat conducting material having a periphery of hexagonal outline and a central opening adapted to fit over a tube, an integral flange about said central opening, a second integral flange defining said periphery of hexagonal outline, the face of said plate having a multiplicity of closely spaced passages formed by cutting the material of said plate along closely spaced lines disposed substantially radially of said central opening and deflecting the material between contiguous lines to provide vanes defining the side walls of said passages, each of said vanes extending substantially equidistantly above and below the original plane of said plate and having the opposite terminal ends thereof integral with i said flanges, substantially the entire surface of the face of said plate in which said closely spaced lines are out being thus deflected without waste to produce said vanes and being thus utilized as a heat exchange surface, said plate adapted to be placed with at least one of said flanges of each plate except one terminal plate in substantially abutting relationship with
  • a heat exchanger unit comprising a tubular member having thereon a multiplicity of disks of foil-like thickness of high heat conducting material, each disk having a central opening defined by an integral flange through which said tubular member passes and an integral flange on the periphery thereof, at least one of said flanges of each disk except one terminal disk being in substantially abutting relationship with the face of a contiguous disk and each disk having in the face thereof a series of closely spaced passages disposed substantially radially of said central open ing, said passages being formed by cutting the disk along closely spaced lines disposed substantially radially of said central opening and deflecting the material between contiguous lines to provide vanes defining the side walls of said passages, each of said vanes extending substantially equi-- distantly above and below the original plane of said disk and having the opposite terminalends thereof integral with the said flanges, substantially the entire face of said disk being thus deflected without waste to produce said vanes and being thus utilized as a heat exchange surface, the
  • a heat exchanger unit comprising a tubular member having thereon a multiplicity of platelike members, each of foil-like thickness and of high heat conducting material, each such member having a central opening deflned by an integral flange through which said tubular member passes, a periphery of polygonal shape and an integral flange on said polygonal periphery, said members? being arranged on the tubular member so that at least one of said flanges of each member except one terminal member is in substantially abutting relationship with the face of a.
  • each member having a multiplicity of closely spaced passages separated by vanes, each of said vanes being formed by'cutting the plate-like member along closely spaced lines disposed substantially radially of said central opening and deflecting the material between contiguous lines, each of said vanes extending substantially equidistantly above and below the original plane of said plate-like member and having the terminal ends thereof integral with said flanges, substantially the entire surface of the portion of said plate-like member in which said closely spaced lines are cut being thus deflected without waste to produce said vanes and being thus utilized as a heat exchange surface, the vanes of each member having the edges thereof positioned close to the edges of the vanes of the plate-hke members on the opposite sides thereof, thereby providing a relatively large mass of said high heat conducting material per unit of exchanger volume.
  • a heat exchanger comprising a shell, a multiplicity of individual units insaid shell for flow of three fluid streams therethrough, the individual units each having anouter polygonal outline and being disposed in said shell in nested relation of disks of foil-like thickness of high heat conducting material, each disk having an integral flange on the periphery thereof, the disks being so arranged that the flange of each disk except one terminal disk is in substantially abutting relationship with the face of'a-contiguous disk, is in contact with'the inner wall of the inner tube, and each disk having in the face thereof a multiplicity of closely spaced passages formed bycutting the disk along closely spacedlines disposed substantially radially of the periphery of said disk and deflecting the material between contiguous lines to providevanes defining the side walls or said passages, each'of said vanes extending substantially equidistantly above and below the oflginal plane of said disk,substantially the entire surface-of the face of said disk being thusdeflected
  • a heat exchanger comprising a shell, a multiplicity of individual units in said shell for flow of three fluid streams therethrough, the individual units each having an outer hexagonal outline and being disposed in said shell in nested relation with the outer surfaces of interior units disposed close to and in alignment with the outer surfaces of contiguous units, each unit comprising a pair of concentric tubes in spaced relation, the inner tube of each unit having a multiplicity of circular metallic disks thereon each having a thickness of from .005" to .020, each disk having an integral flange on the periphery thereof, the disks being so arranged that the flange of each disk except one terminal disk is in substantially abutting relationship with the face of a contiguous disk and is in contact with the inner wall of the inner tube and each disk having in the face thereof a multiplicity of closely spaced passages formed by cutting the disk along closely spaced lines disposed substantially radially of the periphery of said disk and deflecting the material between contiguous lines to provide vanes defining the side walls of

Landscapes

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

Description

Dec. 5, 1950 H. F. BUSCHOW HEAT EXCHANGE UNIT 4 Sheets-Sheet 1 Filed June 21, 1946 l NI 'EN'II'OR. ffarman Z'jwrfiwa ATTORNEY Dec. 5, 1950 H. F. BUSCHOW 2,532,233
HEAT EXCHANGE UNIT Filed June 21, 1946 4 Sheets-Sheet 2 INVENTOR Herman J'T'flaac/imu BY. Z I
ATTORNEY Dec. 5, 1950 uscubw 2,532,288
HEAT CHANGE UNIT Filed June 21, 1946 4 Sheets-Sheet 3 JNVENTOR.
Dec. 5, 1950 H. F. BUSCHOW 2,532,288
HEAT EXCHANGE UNIT 4 Sheets-Sheet 4 57 55 59 55 flennan Ffiasdw/o JTI'ORNE Y Patented Dec. 1950 near EXCHANGE UNIT Herman F. Buschow, North Arlington, N. 1., as-
signor to Hydrocarbon Research, Inc., New York, N. Y., a corporation ofNew Jersey Application June 21, Bid, Serial No. 678,464
The present invention relates to an improved exchanger for recovering the cold content of the outgoing oxygen and nitrogen products of rectiflcation, which may be at a temperature of about 280 F., in the production of oxygen by the liquefaction and rectification of air, and more particularly to the construction and design of the cold exchangesurface areas providing for high cold transfer emclency between the oxygen and nitrogen products of rectification on the one hand and the air on the other.
Cold accumulators or regenerators (hereinafter referred to as cold exchangers) of large cold-absorbing capacity are well known. In these cold exchangers, the relatively warm incoming air and the relatively cold outgoing oxygen and nitrogen products of rectification are alternately passed with periodically reversed opi eration. so that streams of warm air are flowed through the same packing-filled spaces as, the
cold oxygen and nitrogen traversed during'the preceding step in the process, the high-boiling impurities deposited in these spaces during the passage of the air therethrough being removed therein a large number of tubes each provided with an interior accordion fin of foil-like metal and high heat conductivity disposed to form channels extending longitudinally through the tube and a somewhat similaraccordion fin on the exterior thereof. These fins are usually made by folding thin sheets of copper into shape to produce the desired channels, and then bonding them to the interior and exterior walls of the tubes by coating these walls with soldering metal,
placing the fin sections folded in the desired shape in contact with the solder coating, then placing the assembly in an oven and heating it to a temperature so that the solder on the tube walls wets the fins and later cooling, thereby obtaining a bond between the tube walls and the portions of the fins in flat contact therewith. This operation is arduous and time-consuming and greatly increases the cost of the exchanger.
Among the objects of this invention is to provide a cold exchanger having an exceptionally high area of cold exchanger surface per unit of volume and which can more readily be fabricated and assembled than heretofore known exchangers.
Another object is to provide a fin member 7 Claims. (Cl. 257-228) 2 r i which canreadily be produced, for example, by a simple stamping operation, and this without waste of heat-conducting metal, and which can readily be assembled within a tubular unit to produce longitudinally extending channels for turbulent flow of gaseous media.
Still another object is to provide such exchanger which is more efficient in operation in that the cold transfer rate is considerably greater than in prior known exchangers.
Other objects and advantages of this inven tion will be apparent from the following detailed description thereof.
In the accompanying drawings forming part of this specification and showing for purposes of exempliilcation preferred forms of this invention without limiting the claimed invention to such illustrative instance:
Fig. 1 is a fragmentary (one-quarter) plan view of a preferred form of disk which may be arranged with other like disks to produce a fin for the interior of a tubular unit of a coldexchanger embodying this invention;
Fig. 2 is an enlarged section taken in a plane normal to the disk fin and passing through line 2-2 ofFig.1;
Fig. 3 is a fragmentary (one-quarter) plan view of a preferred form of disk which may be arranged with other like disks to. produce a fin on the exterior of atubular exchanger unit embodying this invention; r
Fig. 3A is a fragmentary plan view of the disk of Fig. 3 showing the disk' as it appears after being cut from a foil-like sheet of metal and prior to the bending of the flanges and twisting of the vanes; i
Fig. 4 is an enlarged section taken. in a plane normal to thefin and passing through line H of Fig. 3; r l
Fig. 5 is a diagrammatic section through a preferred form of exchanger unit embodying this invention;
Fig. 6 is a fragmentary and diagrammatic vertical section through the exchanger unit of Fig. 5 taken through line 6-6 of Fig. 5;
Fig. 7 is a diagrammatic section through a modified form of exchanger unit embodying this invention;
Fig. 8 is a fragmentary and diagrammatic vertical section taken through line 8-8 of Fig. 7; Fig. 9 is a diagrammatic sectionthrough a cold exchanger embodying this invention, involving a bundle or stack of the units of Figs/5 and 6;
Fig. 10 is a diagrammatic section through a cold exchanger embodying this invention, in-
3 vvolving a bundle or stack of the units of Figs. '7 and 8;
Fig. 11 is a diagrammatic section through still another modified form of exchanger unit embodying this invention;
Fig. 12 is a fragmentary and diagrammatic vertical section through the exchanger unit of Fig. 11 taken through line I2--I2 cf Fig. 11; and
Fig. 13 is a composite view of a cold exchanger embodying this invention, the lower half being a vertical section through the exchanger and the upper half a front elevation.
The cold exchange fin embodying this invention may be formed on the interior or exterior, or both the interior and exterior, of a tube such as the oxygen, nitrogen or air tubes of a cold exchanger of the type disclosed and claimed in the Scheibel application Serial No. 641,276, filed January 15, 1946. Also such fins may be employed in the unit of the cold exchanger disclosed more fully in copending application of Keith, Serial No. 676,142, which unit involves two concentric tubes each provided with longitudinally extending channels for flow of gaseous media.
In accordance with this invention, such fins are made by assembling a multiplicity of platelike members or disks by simply stacking them in desired relation on the interior or exterior of the tube, as hereinafter more fully described. Each plate-like member or disk may be made by stamping or otherwise shaping a foil-like sheet,
say of a thickness of from .005" to .020", preferably about .008 to .010", of a material of high heat conductivity, preferably copper. For the "fin adapted to be disposed within the interior of a tube such as tube I 0, Figs. and 6, which corresponds to an oxygen, nitrogen or air tube of the, exchanger shown in the aforesaid Scheibel application, disks I I of the type disclosed in Figs. 1 and 2 are employed.
between deflected to form the series of radially disposed passages I5 and I6 and baiiles 2I and 24 while concurrently producing the integral flanges I2 and '26. Further, it is important to note the production of these exchanger disks involves no waste of relatively expensive copper or other metal, all of the material being utilized, the portion deflected to form the battles and to produce the passages functioning in the operation of the exchanger, as hereinafter described, to provide an exceptionally high surface area of heat exchanger metal per unit of volume.
The disks II, as shown in Fig. 6, are disposed within tube In so that flange I2 on one disk substantially abuts the face of a contiguous disk within the tube III. The two series I3 and I4 of openings I5 and I6, respectively, in effect, form longitudinally extending channels radially disposed within tube IO, flow through which is interrupted at closely-spaced intervals, i. e., between each pair of contiguous disks 'II.
Fin 29 on the exterior of tube In is shown in detail in Figs. 3, 3A and 4. It is formed preferably of copper of foil-like thickness, say from .005 to .020" thick, and produced by a simple stamping operation. Each disk 29 has an interior circular outline 30 ada ted to conform to the shape of the tube III on which it is mounted, the interior edge 30 having an integral flange 3|. The opposite edge 32 of the disk is preferably of polygonal shape, e. g., a hexagonal shape as shown in Figs. 3 and 5. Edge 32 is provided with an integral flange 33. The face of the disk is out along pairs of closely spaced lines 34 and 35, and the material between these lines deflected or twisted about points 38 and 31, as pivots, to produce bafiies 38 which, as shown in Fig. 3, are at right angles to the plane of the disk fin 29.
I However, baffles 38 as well as baffles 2I and 24 Each disk II has an integral flange I2 on the periphery thereof and has in the face thereof two series I3 and I4 of radially-disposed closelyspaced passages I5 and I6. The two series of passa es I5 and I6 are se arated bv a flat area or portion ll of the disk of substantially circular outline. as indicated in Fig. 1. The passages I5 are each formed by cutting the disk along pairs of substantially radially disposed lines I8 and I9, and then deflecting or twisting the material between each pair of lines so as to move this material out of the plane of the disk about points 2n as nivots. therebv producing a vane or bafiie 2I guiding the gaseous flow through each passage I5 forming the series I3. In like manner, the passages I6 are formed by deflecting the material between each pair of radial cuts 22 and 23 to form the baffles 24, one of which is provided for each passage I6 of the series I4. The central portion 25 of each disk is preferably shaped to provide a circ lar flange 26 defining a central relatively small circular opening 27 the cross sectional area of which is substantiallv less than that of the passages I5. The flange 26 defining this opening 21 increases the metal surface over which the gas sweeps and im roves the heat transfer between the gas passing through the tube in which the disks are disposed and that passing outside of the tube of each unit forming the heat exchanger of this invention.
It will be noted each of the disks I I may easily be fabricated by a simple stamping and cutting operation in which the radial cuts IB, I9, 22 and 23 are first produced, thenthe material thereof disk fin II may be set at an angle of from to 90 with the plane of the disks. Preferably, the bafiies are set at an angle of at least 85 with the plane of the disk. As shown in Fig. 3A, the cuts 34 and 35 have a slight curvature at their ends but straight cuts are frequent y employed.
For simplicity of exemplification, the baflies or vanes 2| 24 and 38 are shown as perfectlv flat members attached to their respective disks at their ends. However, these vanes are usually not perfectly flat since they have volutes at their ends produced when the vanes are twisted out of the plane of the disks.
An economy of material may be effected by producing the disks I I form ng the fin for the interior of tube I0 and the disks 29 forming the fin for the exterior of the t be from the Same sheet of copper or other foil-like material of high heat conducting prop rties, the disks II being I formed from the material req ir d to produce the circular opening 30 in the disks 29.
As shown in Figs. 5 and 6, a multiplicitv of disks 29 are assembled on the exterior of tube I0 so that the flange 3| of one disk substantial y abuts the face of a contiguous disk, thus producing a multi licity of lon tudinally extending channels formed by baffles 38.
The disks II may be readily dispo ed in the interior of the tube I0 by simply stacking them within the tube, it being only neces ary to drop stantially the same as the external diameter of tube 1 ll. Since the disks are of foil-like metal of high heat conductivity, preferably copper, the
tubular member, the flange of the disk or 'plate-' like fin which contacts the walls of the tubular member may be incised to permit contraction of interior fins or expansion of exterior fins. With disk ll, such a cut would be made between any two baffies 2| through flange l2 as indicated by He on Fig. 1, while with plate-like fin 29, such a cut would be made between any two baflles 38 through flange 3i as indicated by 29112 on Fig. 3.
in the modification of Figs. 7 and 8, a tubular unit is shown forming one unit of a cold exchanger of the type disclosed in the aforesaid Keith application. This unit comprises a pair oi concentric tubes 39 and 40. Inner tube 39 has the ein a cold exchange fin 4| made by stacking within the tube a sufllcient number of disks like disk I 1 shown in Figs. 1 and 2. Outer tube 40 has on the exterior thereof a fin 42 produced in the same manner as the fin 29 on the exterior of tube in, i. e., by stacking disks 42 on tube 40 with the iiange of one disk abutting the face of a contiguous disk. Disposed in the annular space between tubes 39 and 40 is a fin 43 formed, for example, by folding, for each section of tube length, a strip of foil-like copper into the shape shown in Fig. 7 to provide alternate portions in contact with the inner wall of tube 40 and the outer wall of tube 39 connected by inclined portions, thereby forming two sets of substantially triangular longitudinally extending channels 44 and 45. Each strip of foil-like copper so folded may be approximately 2" wide and adjacent sections of folded strips 43 are preferably separated by narrow spaces or slots 46 to induce turbulence of the gas flowing through the longitudinally extending channels 44 and 45.
The exchanger units of Figs. 5 and 6 are assembled with other like units in a stack or bundle in a shell 47 (Fig. 9) provided with headers, as more fully disclosed in the aforesaid Scheibel copending application. The individual units within the shell 41 are in metal-to-metal contact with one another since the peripheries of the fins on the exterior thereof are disposed with metal-to-metal contact. The spaces between the units and the interior wall of the shell may be filled with packing 48, e. g., crumpled aluminum foil or wood blocks. The shell, if desired, may be made closefitting, relative to the tube bundle, thereby eliminating such packing.
Similarly, the exchanger units of Figs. 7 and 8 are assembled with other like units in a stack or bundle in a shell 41 (Fig. 10) provided with headers, as more fully disclosed in the aforesaid Keith copending application as shown in Fig. 13. The individual units in the bundle of Figs. 10 and 13 have a small clearance between the peripheries of the fins on the exterior thereof, or may be in metal-tmmetal contact.
flanges are flexible, i. e., have a certain amount of 6 In the heat exchanger unit of Figs. '7 and 8, the annular fin 43 of folded strips of foil-like metal may be replaced by fins of the disk type where the annular space between the concentric tubes is appreciable, say over about one-half inch. Such construction is shown in Figs. 11 and 12 in which 58 indicates an interior tube of high heat conductivity of smaller diameter than tube 39 of Figs. 7 and 8 thereby providing a larger annular space between inner tube and exterior tube 49. Stacked on the exterior of tube 40, as in the case of Figs. 7 and 8, are a multiplicity of disks 42 with the flange of one disk abutting the face of a contiguous disk. Stacked within the annular space between tubes" and 50 are a multiplicity ofdisks 54 each having flanges 52, 53 along the a two edges thereof, flange 52 of each disk being bonded, if desired, to the exterior of tube 59 and flange 53 to the interior wall of tube 40. Disks 54 are each provided with a series of radially disposed passages defined by vanes 5| in the same manner as the passages l5 are defined by the vanes 2| of the disk ll hereinabove described. Stacked within the interior of tube 50 is a multiplicity of disks 55 with the flange of one disk in substantially abutting relation with the face of a contiguous disk as hereinabove more fully described in connection with the constructions of Figs. 5 to 8, inclusive. 7
Fig. 13 shows a preferred header and associated port arrangement for the exchanger units of .Figs. 7 and 8. In the construction of this flgure the shell 41 is provided at each end with (1) an oxygen header 56 communicating with through ports 51 with a manifold 58 which is provided with a port 59, (2) a header 50 communicating with the channels formed on the exterior of tubes 40 by disks 42 and through ports 6| with a manifold 62 provided with a. port 63, and (3) a header 64 communicating with the interior of tubes 39 and provided with a port 55. The flows of air and nitrogenduring one cycle of the operation indicated by full line arrows in Fig. 13 take place through headers 60, 64, respectively, and upon reversal during the subsequent cycle of operation the flows of air and nitrogen, as indicated by the dotted line arrows, take place through the headers 54 and 50, respectively. Oxygen flows continuously through headers 55.
In the operation of the exchanger of Fig. 13, the flow of oxygen, as shown by the fullline arrows, takes place through bottom port 59 into the manifold 58, thence through the ports 51 into the bottom header 5!; through all of the tubes 49 in the assembly of units in the shell 41 into and through the top header 56, top ports 51 and manifold 58, the oxygen leaving through the top port 59. This flow is continuous throughout the operation of the exchanger, 1. e., no reversal of oxygen flow takes place. operation, the nitrogen, as shown by the full line arrows on Fig. 13, enters through bottom port into the header 64, flows through the interior of all of the tubes 39 and exits through top header the dotted line arrows, air flows through top port During one period of into and through the top header. [4,, then through all of the tubes 39, exiting through the bottom header 64 and bottom port 65. During this reversal period nitrogen fiows through bottom port 63, bottom manifold 62, bottom ports 6 I bottom header 60, the channels formed by the disks 42 on the exterior of all of the tubes 40 and exits through top header 60, ports 5|, manifold 52 and top port 83. As in theprevious cycle of operation, air flows countercurrent to both the nitrogen and oxygen streams.
Exchangers made in accordance with this in-' I vention have been found to have a heat transfer rate of about 42 B. t. u.s per square foot per hour, as compared to about 17 B. t. u.s per square foot per hour of heat exchangers made with fins of the same metal (copper) but of I the type employed prior to this invention.
The longitudinally extending passages produced by the disks when assembled within and without the tubes provide a symmetrical path for cold exchange between the air, the oxygen and nitrogen products of rectification flowing through each exchanger since, with the flns of this invention, these longitudinally extending passages are all disposed substantially radially relative to the tubes with which they are associated. This results in such greatly improved cold transfer between the gaseous media that it is not neces-' sary to use copper tubes, but less expensive nickel steel tubes may be used and still obtain satisfacwry cold exchange. The use of nickel steel tubes in an exchanger having a nickel steel shell, eliminates the necessity of providing such shell with expansion joints.
Where the disk fin II is required for tubes of small diameter, it may be made with a singleceptionally high surface area of heat transfer surface per unit of volume of exchanger space may be made with the fins of this invention. With these fins, employing tubes of from 1 to 4" outside diameter, preferably about 2%" outside diameter, having a wall thickness of .035" to .125", preferably about .065", the exchanger may have from 300 to 500 square feet of exchanger surface per cubic foot of exchanger volume. The thorough contact between the flanges of the fins and the walls of the tubes results in high fin efficiency. The turbulent flow, caused by the interruptions in the passages at closely spaced intervals; 1. e., between each pair of contiguous disks or plate-like fins, further improves the cold transfer efficiency of the exchanger. The exchanger is, therefore, of exceptionally high cold transfer efiiciency. This makes it possible to have the volumetric space through which nitrogen on the one hand and air on the other flows relatively small, thereby minimizing reversal losses. Moreover, the flow through the interior of the tubes and in the channels defined by the fins on the exterior of the tubes takes place in a general longitudinal direction; hence, minimum pressure drop of fluid flowing therethrough occurs.
It will be noted that exchangers with an ex- In Figs. 5 and '7, the fins of this invention are shown associated with cylindrical tubes which are generally preferred. However, fins of this type may be made for use with hexagonal, square or other shaped tubes; hence, the terms tube" and tubular member" are" used in a broad sense and are intended to include all such polygonal tubular members. Similarly, the external fins shown in Figs. 5 and '7 may assume any desired polygonal exterior outline other than the described hexagonal outline.
Since different embodiments of the invention can be made without departing from the scope of this invention, it is intended that all matter contained in the above description or shown in the accompanying drawings shall be interpreted as illustrative and not in a limiting sense.
What is claimed is:
1. A heat exchanger fin comprising a platelike member of foil-like thickness of high heat conducting material having a central opening defined by an integral flange, a second integral flange on the periphery thereof and having in the face thereof a multiplicity of closely-spaced passages formed by cutting the plate-like member along closely spaced lines disposed substantially radially of said central opening and defleeting the material between contiguous lines to provide vanes defining the side walls of said passages, each of said vanes extending substantially equidistantly above and below the original plane of said plate-like member and having the opposite terminal ends thereof integral with the said flanges, substantially the entire surface of the face of said plate-like member being thus deflected without waste to roduce said vanes and being thus utilized as a heat exchange surface, said member adapted to be stacked with at least one of said flanges of each member except one terminal member in substantially abutting relationship with the face of a contiguous member to provide a relatively large mass of high heat conducting material per unit of heat exchanger volume permeated by a multiplicity of said passages for flow of a fluid medium therethrough in surface contact with said vanes.
2. A heat exchanger fin comprising a disk from .005" to .020" thick of high heat conducting material, said disk having a central opening adapted to flt over a tube, an integral flange on the periphery thereof, a second integral flange defining said central opening and having in the face thereof a series of closely spaced passages disposed radially relative to said central opening, said passages being formed by cutting said disk along closely spaced lines disposed substantially radially of said central opening and deflecting the material between contiguous lines to provide vanes defining the sidewalls of said passages, each of said vanes extending substantially equidistantly above and below the original plane of said disk and having the opposite terminal ends thereof integral with said flanges, substantially the entire surface of the face of said disk being thus deflected without waste to produce said vanesand being thus utilized as a heat exchange surface, said disk adapted to be stacked with at least one of said flanges of each disk except one terminal disk in substantially abutting relationship with the face of a contiguous disk to provide a relatively large mass of high heat conducting material per unit of heat exchanger volume permeated by a multiplicity of said passages for flow of a fluid medium therethrough in surface contact with said vanes.
3. A heat exchanger fin comprising a plate of foil-like thickness of high heat conducting material having a periphery of hexagonal outline and a central opening adapted to fit over a tube, an integral flange about said central opening, a second integral flange defining said periphery of hexagonal outline, the face of said plate having a multiplicity of closely spaced passages formed by cutting the material of said plate along closely spaced lines disposed substantially radially of said central opening and deflecting the material between contiguous lines to provide vanes defining the side walls of said passages, each of said vanes extending substantially equidistantly above and below the original plane of said plate and having the opposite terminal ends thereof integral with i said flanges, substantially the entire surface of the face of said plate in which said closely spaced lines are out being thus deflected without waste to produce said vanes and being thus utilized as a heat exchange surface, said plate adapted to be placed with at least one of said flanges of each plate except one terminal plate in substantially abutting relationship with the face of a contiguous plate to provide a-relatlvely large mass of high heat conducting material per unit of heat exchanger volume permeated by a multiplicity of said passages for flow of a fluid medium therethrough in surface contact with said vanes,
4. A heat exchanger unit comprising a tubular member having thereon a multiplicity of disks of foil-like thickness of high heat conducting material, each disk having a central opening defined by an integral flange through which said tubular member passes and an integral flange on the periphery thereof, at least one of said flanges of each disk except one terminal disk being in substantially abutting relationship with the face of a contiguous disk and each disk having in the face thereof a series of closely spaced passages disposed substantially radially of said central open ing, said passages being formed by cutting the disk along closely spaced lines disposed substantially radially of said central opening and deflecting the material between contiguous lines to provide vanes defining the side walls of said passages, each of said vanes extending substantially equi-- distantly above and below the original plane of said disk and having the opposite terminalends thereof integral with the said flanges, substantially the entire face of said disk being thus deflected without waste to produce said vanes and being thus utilized as a heat exchange surface, the vanes of each disk having the edges thereof positioned close to the edges of the vanes. of the disks on opposite sides thereof, thereby providing a relatively large mass of said high heat conducting material per unit of exchanger volume.
5. A heat exchanger unit comprising a tubular member having thereon a multiplicity of platelike members, each of foil-like thickness and of high heat conducting material, each such member having a central opening deflned by an integral flange through which said tubular member passes, a periphery of polygonal shape and an integral flange on said polygonal periphery, said members? being arranged on the tubular member so that at least one of said flanges of each member except one terminal member is in substantially abutting relationship with the face of a. contiguous member, the face of each member having a multiplicity of closely spaced passages separated by vanes, each of said vanes being formed by'cutting the plate-like member along closely spaced lines disposed substantially radially of said central opening and deflecting the material between contiguous lines, each of said vanes extending substantially equidistantly above and below the original plane of said plate-like member and having the terminal ends thereof integral with said flanges, substantially the entire surface of the portion of said plate-like member in which said closely spaced lines are cut being thus deflected without waste to produce said vanes and being thus utilized as a heat exchange surface, the vanes of each member having the edges thereof positioned close to the edges of the vanes of the plate-hke members on the opposite sides thereof, thereby providing a relatively large mass of said high heat conducting material per unit of exchanger volume.
6. A heat exchanger comprising a shell, a multiplicity of individual units insaid shell for flow of three fluid streams therethrough, the individual units each having anouter polygonal outline and being disposed in said shell in nested relation of disks of foil-like thickness of high heat conducting material, each disk having an integral flange on the periphery thereof, the disks being so arranged that the flange of each disk except one terminal disk is in substantially abutting relationship with the face of'a-contiguous disk, is in contact with'the inner wall of the inner tube, and each disk having in the face thereof a multiplicity of closely spaced passages formed bycutting the disk along closely spacedlines disposed substantially radially of the periphery of said disk and deflecting the material between contiguous lines to providevanes defining the side walls or said passages, each'of said vanes extending substantially equidistantly above and below the oflginal plane of said disk,substantially the entire surface-of the face of said disk being thusdeflected without waste to produce said vanes and being thus utilized as a heat exchange surface, the vanes of each disk having the edges thereof positioned close to the edges of the vanes of the disks on opposite sides thereof, thereby providing a relatively large mass of said high heat conducting material per unit volume of inner tube, each inner tube'of each unit having on the exterior thereof a multiplicity of disks of foil-like thickness of high heat conducting material, each such disk-having a, central opening defined by an integralflange through which the inner tube passes and an integral flange on the periphery thereof, the disksbeing so arranged that at least one flange of each disk except one terminal disk is in substantially abutting relationship with the face of a, contiguous disk and each disk having in the face thereof amultiplicity of closely spaced passages formed by cutting the disk along closely spaced lines substantially radially of its periphery and deflecting the material between contiguous lines to provide vanes deflningthe side walls of said passages, each of said vanes extending sub stantially equidistantly above and below the original plane of said disk and having the terminal ends thereof integral with said flanges, substantially the entire surface of the face of said disk being thus deflected without waste to produce 1 1 said vanes and being thus utilized as a heat exchange surface, the vanes of each member having the edges thereof positioned close to the edges of the vanes of the members on opposite sides thereof, and the outer tube of each unit having on the exterior wall thereof a multiplicity of plates of foil-like thickness of high heat conducting material, each plate having an outer polygonal outline defined by an integral flange and a central opening defined by an integral flange through which the outer tube passes, the plates being so arranged that at least one flange of each plate except one terminal plate is in substantially abutting relationship with the face of a contiguous plate and each plate having in the face thereof a multiplicity of closely spaced passages formed by cutting the plate along closely spaced lines substantially radially of the central opening therein and deflecting the material between contiguous lines to provide vanes defining the side walls of said passages, each of said vanes extending substantially equidistantly above and below the original plane of said plate and having the terminal ends thereof integral with said flanges, substantially the entire surface of the face of said plate being thus deflected without waste to produce said vanes and being thus utilized as a heat exchange surface, the vanes of each plate having the edges thereof positioned close to the edges of the vanes of the plates on opposite sides thereof.
7. A heat exchanger comprising a shell, a multiplicity of individual units in said shell for flow of three fluid streams therethrough, the individual units each having an outer hexagonal outline and being disposed in said shell in nested relation with the outer surfaces of interior units disposed close to and in alignment with the outer surfaces of contiguous units, each unit comprising a pair of concentric tubes in spaced relation, the inner tube of each unit having a multiplicity of circular metallic disks thereon each having a thickness of from .005" to .020, each disk having an integral flange on the periphery thereof, the disks being so arranged that the flange of each disk except one terminal disk is in substantially abutting relationship with the face of a contiguous disk and is in contact with the inner wall of the inner tube and each disk having in the face thereof a multiplicity of closely spaced passages formed by cutting the disk along closely spaced lines disposed substantially radially of the periphery of said disk and deflecting the material between contiguous lines to provide vanes defining the side walls of said passages, each of said vanes extending substantially equidistantly above and below the original plane of said disk, substantially the entire surface of the face of said disk being thus deflected without waste to produce said vanes and being thus utilized as a heat exchange surface, the vanes of each disk having the edges thereof positioned close to the edges of the vanes of the disks on opposite sides thereof; each inner tube of each unit having on the exterior wall thereof a multiplicity of circular metallic disks each havdisk having a central opening deflned by an integral flange through which the inner tube passes and an integral flange on the periphery thereof, the disks being so arranged that at least one flange of each disk except one terminal disk is in substantially abutting relationship with the face of a contiguous disk and each disk having in the face thereof a multiplicity of closely spaced passages formed by cutting the disk along closely spaced lines substantially radially of its periphery and deflecting the material between contiguous lines to provide vanes deflning the side walls of said passages, each of said vanes extending substantially equidistantly above and below the original plane of said disk and having the terminal ends thereof integral with said flanges, substantially the entire surface of the face of said disk being thus deflected without waste to produce said vanes and being thu utilized as a heat exchange surface, the vanes of each member having the edges thereof positioned close to the edges of the vanes of the members on opposite sides thereof; and the outer tube of each unit having on the exterior wall thereof a multiplicity of metallic plates of a thickness of from .005" to .020", each plate having an outer hexagonal outline deflned by an integral flange and a central opening deflned by a flange through which the outer tube passes, the plates being so arranged that at least one flange of each plate except one terminal plate is in substantially abutting relationship with the face of a contiguous plate and each plate having in the face thereof a multiplicity of closely spaced passages formed by cutting the plate along closely spaced lines substantially radially of said central opening and deflecting the material between contiguous lines to provide vanes defining the side walls of said passages, each of said vanes extending substantially equidistantly above and below the original plane of said plate and having the terminal ends thereof integral with said flanges, substantially the entire surface of the face of said plate being thus deflected without waste to produce said vanes and being thus utilized as a v heat exchange surface, the vanes of each member having the edges thereof positioned close to the edges of the vanes of the plates on opposite sides thereof.
HERMAN F. BUSCHOW.
REFERENCES CITED The following references are of record in the flle of this patent:
UNITED STATES PATENTS Number Name Date 1,148,865 Shipman Aug. 3, 1915 1,880,533 Thomas Oct. 4, 1932 1,912,644 Lenning June 6, 1933 2,016,164 Williams Oct. 1, 193 2,036,417 Laird Apr. 7, 1936 2,384,714 Villiger Sept. 11, 1945
US678464A 1946-06-21 1946-06-21 Heat exchange unit Expired - Lifetime US2532288A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US678464A US2532288A (en) 1946-06-21 1946-06-21 Heat exchange unit

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US678464A US2532288A (en) 1946-06-21 1946-06-21 Heat exchange unit

Publications (1)

Publication Number Publication Date
US2532288A true US2532288A (en) 1950-12-05

Family

ID=24722896

Family Applications (1)

Application Number Title Priority Date Filing Date
US678464A Expired - Lifetime US2532288A (en) 1946-06-21 1946-06-21 Heat exchange unit

Country Status (1)

Country Link
US (1) US2532288A (en)

Cited By (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2703225A (en) * 1951-05-31 1955-03-01 Holly Sugar Corp Heat transfer apparatus for granular material
US2703701A (en) * 1946-05-20 1955-03-08 Modine Mfg Co Heat exchanger
US2903246A (en) * 1957-12-20 1959-09-08 Richard W Kritzer Baseboard radiators
US2918265A (en) * 1955-07-22 1959-12-22 Mississippi River Fuel Corp Rectification apparatus
US2990163A (en) * 1958-06-09 1961-06-27 Borg Warner Turbulizer
US2999364A (en) * 1957-07-26 1961-09-12 Philips Corp Method and devices for separating components from a gas- and/or vapour mixture
US3396784A (en) * 1965-04-17 1968-08-13 Sulzer Ag Honeycomed restricted tube heat exchanger
FR2552216A1 (en) * 1983-09-21 1985-03-22 Onera (Off Nat Aerospatiale) Improvements made to heat exchanger pipes and to exchangers made with such pipes
EP0138677A3 (en) * 1983-09-21 1985-05-22 Office National d'Etudes et de Recherches Aérospatiales (O.N.E.R.A.) Heat-exchanger tubes, heat-exchangers provided therewith and gas-turbine plants comprising such a heat-exchanger
US4858683A (en) * 1988-04-04 1989-08-22 Heil-Quaker Corporation Stamped discharge grille including two louvred sections

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1148865A (en) * 1912-12-07 1915-08-03 Bennet Carroll Shipman Heat-transferring apparatus.
US1880533A (en) * 1932-02-03 1932-10-04 Servel Sales Inc Heat exchanger
US1912644A (en) * 1929-02-18 1933-06-06 Electrolux Servel Corp Refrigeration
US2016164A (en) * 1934-06-12 1935-10-01 Harry D Williams Fin radiator
US2036417A (en) * 1932-12-08 1936-04-07 Wilbur G Laird Method of making fin radiators
US2384714A (en) * 1943-04-12 1945-09-11 Tech Studien Ag Tubular heat exchanger

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1148865A (en) * 1912-12-07 1915-08-03 Bennet Carroll Shipman Heat-transferring apparatus.
US1912644A (en) * 1929-02-18 1933-06-06 Electrolux Servel Corp Refrigeration
US1880533A (en) * 1932-02-03 1932-10-04 Servel Sales Inc Heat exchanger
US2036417A (en) * 1932-12-08 1936-04-07 Wilbur G Laird Method of making fin radiators
US2016164A (en) * 1934-06-12 1935-10-01 Harry D Williams Fin radiator
US2384714A (en) * 1943-04-12 1945-09-11 Tech Studien Ag Tubular heat exchanger

Cited By (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2703701A (en) * 1946-05-20 1955-03-08 Modine Mfg Co Heat exchanger
US2703225A (en) * 1951-05-31 1955-03-01 Holly Sugar Corp Heat transfer apparatus for granular material
US2918265A (en) * 1955-07-22 1959-12-22 Mississippi River Fuel Corp Rectification apparatus
US2999364A (en) * 1957-07-26 1961-09-12 Philips Corp Method and devices for separating components from a gas- and/or vapour mixture
US2903246A (en) * 1957-12-20 1959-09-08 Richard W Kritzer Baseboard radiators
US2990163A (en) * 1958-06-09 1961-06-27 Borg Warner Turbulizer
US3396784A (en) * 1965-04-17 1968-08-13 Sulzer Ag Honeycomed restricted tube heat exchanger
FR2552216A1 (en) * 1983-09-21 1985-03-22 Onera (Off Nat Aerospatiale) Improvements made to heat exchanger pipes and to exchangers made with such pipes
EP0138677A3 (en) * 1983-09-21 1985-05-22 Office National d'Etudes et de Recherches Aérospatiales (O.N.E.R.A.) Heat-exchanger tubes, heat-exchangers provided therewith and gas-turbine plants comprising such a heat-exchanger
US4858683A (en) * 1988-04-04 1989-08-22 Heil-Quaker Corporation Stamped discharge grille including two louvred sections

Similar Documents

Publication Publication Date Title
JP2862213B2 (en) Heat exchanger
US2804284A (en) Heat exchanger
CN101526324B (en) Fin, heat exchanger with fin and heat exchanger device
US7334631B2 (en) Heat exchanger
JP4231610B2 (en) Manufacturing method of heat exchanger fins
US2532288A (en) Heat exchange unit
JP2002062085A (en) Heat-exchange fin for brazed-plate heat exchanger, and heat exchanger
US3528496A (en) Plate-fin heat exchanger
CN110822942B (en) Three-dimensional cobweb laminated tube type heat exchanger based on bionics
JPH10185478A (en) Metal cooling fin for heat exchanger
US2585912A (en) Regenerator for the recovery of the cold content of gases
US2045657A (en) Heat exchange apparatus
US12510299B2 (en) Spiral heat exchanger and heat exchange device
US2662749A (en) Annular flow heat exchanger
US3403727A (en) Crossflow countercurrent heat exchanger with inner and outer-tube sections made up of closely packed coaxially nested layers of helicoidally wound tubes
CN104390499A (en) Sawtooth porous corrugated fin type plate-fin heat exchanger
US2803440A (en) Finned tube construction
CN204301586U (en) Porous ripple fin-type plate-fin heat exchanger
JPS6334466A (en) Condenser
US2589262A (en) Heat exchanger
US3756310A (en) Regenerator
CN106440886A (en) Plate-fin heat exchanger
CN210051186U (en) Three-medium heat exchanger
CN204286172U (en) Zigzag porous ripple fin-type plate-fin heat exchanger
JPS63210595A (en) Plate fin type heat exchanger