US1683236A - Heat-exchanging apparatus - Google Patents

Heat-exchanging apparatus Download PDF

Info

Publication number
US1683236A
US1683236A US132694A US13269426A US1683236A US 1683236 A US1683236 A US 1683236A US 132694 A US132694 A US 132694A US 13269426 A US13269426 A US 13269426A US 1683236 A US1683236 A US 1683236A
Authority
US
United States
Prior art keywords
fluid
compartment
shell
tubes
dome
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
US132694A
Inventor
Carl F Braun
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.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Priority to US132694A priority Critical patent/US1683236A/en
Application granted granted Critical
Publication of US1683236A publication Critical patent/US1683236A/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
    • F28BSTEAM OR VAPOUR CONDENSERS
    • F28B1/00Condensers in which the steam or vapour is separate from the cooling medium by walls, e.g. surface condenser
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10STECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10S165/00Heat exchange
    • Y10S165/355Heat exchange having separate flow passage for two distinct fluids
    • Y10S165/40Shell enclosed conduit assembly
    • Y10S165/401Shell enclosed conduit assembly including tube support or shell-side flow director
    • Y10S165/405Extending in a longitudinal direction
    • Y10S165/413Extending in a longitudinal direction for directing flow along the length of tube

Definitions

  • This invention relates to heat exchanging apparatus and particularl pertains to counterpassing condensers, ractionating condensers, coolers and the like.
  • heat exchangers with an. outer shell, through which a flow of fluid to be cooled is maintained and within which shella-tube nest is positioned to provide a plurality of circulating passageways for a cooling fluid, a heat exchange takin place between the fluid outside of the tu es and the fluid inside the tubes.
  • the apparatus may become impracticable and uneconomical on account of size and cost.
  • the object of the present invention is to provide an arrangement whereby a plurality of passes's'through the apparatus is combined with counterflow of the fluids in a multipass heat exchanger.
  • the present invention contemplates the use of an enclosing shell through which a fluid may flow, and within which shell is disposed a set oftubes through which another fluid flows, said shell and tubes being so arranged that a counterflow of the two fluids will be effected through a length of counterflow passagewaysi
  • the invention is illustrated b I way of example in the accompanying rawings, in which:
  • Fig. 1 is a view in longitudinal'central section showing one form of the present invention.
  • Fig. 2 is a view in transverse vertical section as seen on line 2-2 of Fig. 1.
  • Fig. 3 is a view showing another form of the present invention as seen on its central longitudinal section line.
  • Fig. 4 is a view in transverse section through the form of the invention shown in Fig. 3, as. seen on the line 44 of Fig. 3.
  • Fig. 5 is a view in transverse section through the opposite end of the exchanger as seen on line 5-5 of Fig. 3.
  • Fig. 6 is a diagrammatical-view showin the flow of the two fluids through the-shell and the groups of tubes.
  • a shell 10 is provided having an induction port ,11 and an eduction port 12.
  • a fluid flows longitudmally through the shell from the induction port 11 to the eduction port 12.
  • the opposite ends of the shell are closed by a dome 13 at one end and a cap 14 at the oppo s te and.
  • the dome 13 is substantially cylindrieal inv shape and is formed with an outer cylindrical .wall 15- having a-transverse web or partition member lfi. This member does not divide the interior of the dome into equal parts, but is so arranged as,
  • the outer end of the dome is closed by a cover plate 17, while the inner end of the dome is closed by a tube sheet 18 of a tube nest 19.
  • the tube nest comprises a plurality of parallel longitudinally extending tubes 20 connected to tube sheet. 18 at one end and a tube sheet 21 at the opposite end.
  • The. dome member 15 is formed with an induction port 22 and an eduction port 23 communicating with the compartments 24 and 25, into which the domes divided by the partition walls 16.
  • the compartment 24 as seen in Fig.2 is of relatively small sectional area and communicates with a small number of tubes 20, as compared with the aggregate number of tubes in the tube nest.
  • the compartment 25 communicates with the remaining tubes. All of the tubes terminatin in the tube sheet 21 are in communication y a cap 26 which is secured over the end of'the tube sheet 21 and diverts the fluid passing through the tube sheets in communication with compartment 24 to the tubes communicating with the enlarged compartment 25.
  • the entire volume of fluid circulating through the shell passes from induction 'open through the induction opening 22 of the dome passes at high velocity throughthe tubes in communication with the compartment 24 and, of course, in the same direction, as the direction of flow of the fluid in the shell.
  • a fluid induction port 38 communicates with the segmental passageway 34 and a fluid eduction port 39 communicates with the segmental compartment 37 'of the dome.
  • the compartments 34 and 37 are sectors of the circle, each being measured by substantially onesixth of the circumference of the circle and separated by a partition wall 40 which also separates the induction port 38 and the eduction port 39.
  • the compartments 35 and 36 are sectors of the circle, each including sub-. stantially one-third of the circumference of' the circle and divided by a partition wall 41 extending diametrically opposite from the partition wall 40.
  • the compartments 34 and 35 are separated by radially extending partition wall 42 and the compartments 36 and 37 are separated by radially extending partition wall 43.
  • the opposite end of the shell 27 from the end upon which the cylindrical dome 32 is mounted' isclosed by a tube sheet 44, on the outside of. which isa cap 45.
  • cap 45 is divided into three compartments of sector shape, as indicated at 46, 47 and 48. These compartments are separated by radially extending walls. Such a wall 49 separates compartments 46.a nd 47, and wall 50 separates compartments 47 and 48, and a wall ,51 separates compartments 46 and 48.
  • wall'40 in the dome 32 is in the same plane and in longitudinal alignment with wall 51 oflthe cap 45, and that walls 49 and 50 in the cap .45 are 'spaced at one hundred twenty degrees to wall 51, so that viewed collectively the radial 'walls in the dome 32 and the cap are arranged at sixty degrees to each other, which divides the set of tubes into six sets indicated by the reference characters A, B, C, D, E and F, each set being defined by a sector representing approximately one-sixth of the sectional area of the shell.
  • a fluid to be cooled may pass into the shell 27 through induction port 29 and then flow lengthwise of the shell along the passageway of the semi-circular section, as defined by the shell wall, and the longitudinal partition member 28.
  • the fluid When the fluid has reached the opposite end of the partition member from its induction end, it will pass around the end of the partition member 28 and between this end and the tube sheet 44 through a passageway '52. 'The fluid will then return along the lower passageway of semicircular section to the eduction port 30.
  • Cooling fluid is delivered to the dome 32 through induction port 38 and into compartment 34 defined b the radial walls 40 and 42.
  • the cooling fli iid will then flov; lengthwise of the set of tubes indicate! by the character A.
  • This fluid will pass out of this set of tubes A and into compartment 46 formed in the cap 45 at the opposite end of the shell.
  • the compartment 46 is represented by a sector of twice the arcuate length of compartment 34 and soarranged that the compartment 46 will overlap the compartment 34 by. substantially one-half its arcuate length. This will cause the fluid which flowed through the pipes A in exclusive communication with compartment 34 to be diverted into pipes B exclusively communicating with the compartment 46 at the cap end.
  • the fluid which has now assed to compartment 35 in the dome by owing through tubes B will be diverted from compartment 35 to tubes C which communicate with the other half of compartment 35 and extend to the opposite end of the shell where they communicate with compartment 47 of the cap.
  • the fluid will then flow through compartment 47 of the cap.
  • the fluid will then find its way into the set of tubes D in communication with the compartment 47 at one end and the compartment 36 in the dome.
  • the fluid in compartment 36 will be diverted from the set of tubes D to the set of tubes E and will again flow throughout the length of the shell to compartment 48 in the cap.
  • the fluid will pass from pipes E into compartment 48. and then into tu es F which communicate with this compartment and also cor'nmunlcate at the opposite end with compartment 37 of the dome.
  • the fluid passes from the exchanger through education port 38.
  • cooling medium and the medium to be cooled may each flow either through shell or tubes.
  • a shell through which a'fluid flows longitudinally from end to end of the shell and returns in a single pass in each direction, a tube nest extending longitudinally of the .shell and through which a cooling medium flows, means at the opposite ends of the tube nest for dividing the tubes into three times as many groups as there are longitudinal passes of the fluid in the shell and creating a circulation of a cooling medium through said tubes in a manner to establish a countercurrent flow of the two fluids in a ratio of one portion parallel current to two portions countercurrent.

Landscapes

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

Description

Sept. 4, 1928.
C. F. BRAUN HEAT EXCHANGING APPARATUS Filed Aug. 31, 1926 INVENTOR.
ATTORNEYS.
Patented Sept. 4, 1928.
UNITED STATES CARL F. B'BAUN, OF PASADENA, CALIFORNIA.
HEAT-EXOKANGING APPARATUS.
Application filed August a1, 1926. Serial No. 132,694.
This invention relates to heat exchanging apparatus and particularl pertains to counterpassing condensers, ractionating condensers, coolers and the like.
It is common practice to construct heat exchangers with an. outer shell, through which a flow of fluid to be cooled is maintained and within which shella-tube nest is positioned to provide a plurality of circulating passageways for a cooling fluid, a heat exchange takin place between the fluid outside of the tu es and the fluid inside the tubes.
, Practice has demonstrated that in most cases counterflow of the two fluids is desirable.
If the two fluids pass through the apparatus in a single pass each, the apparatus may become impracticable and uneconomical on account of size and cost.
In some heat exchangers, a 'multipass arrangement has been made whereby the fluids between which heat exchange takes place, make a plurality of passes back and forth throughout the length of exchanger; this construction has the advantage of compactness, but frequently at the expense of the counterflow principle.
The object of the present invention is to provide an arrangement whereby a plurality of passe's'through the apparatus is combined with counterflow of the fluids in a multipass heat exchanger.
The present invention contemplates the use of an enclosing shell through which a fluid may flow, and within which shell is disposed a set oftubes through which another fluid flows, said shell and tubes being so arranged that a counterflow of the two fluids will be effected through a length of counterflow passagewaysi The invention is illustrated b I way of example in the accompanying rawings, in which:
Fig. 1 is a view in longitudinal'central section showing one form of the present invention.
Fig. 2 is a view in transverse vertical section as seen on line 2-2 of Fig. 1.
Fig. 3 is a view showing another form of the present invention as seen on its central longitudinal section line.
Fig. 4 is a view in transverse section through the form of the invention shown in Fig. 3, as. seen on the line 44 of Fig. 3.
Fig. 5 is a view in transverse section through the opposite end of the exchanger as seen on line 5-5 of Fig. 3. v
Fig. 6 is a diagrammatical-view showin the flow of the two fluids through the-shell and the groups of tubes.
Referring more particularly to Figs. 1 and 2 ot the. drawings, it will be seen that a shell 10 is provided having an induction port ,11 and an eduction port 12. A fluid flows longitudmally through the shell from the induction port 11 to the eduction port 12. The opposite ends of the shell are closed by a dome 13 at one end and a cap 14 at the oppo s te and. 'The dome 13 is substantially cylindrieal inv shape and is formed with an outer cylindrical .wall 15- having a-transverse web or partition member lfi. This member does not divide the interior of the dome into equal parts, but is so arranged as,
to form two compartments of-predetermined unequal cross sectional area, as more clearly shown in Fig. 2 of the drawings.
The outer end of the dome is closed by a cover plate 17, while the inner end of the dome is closed by a tube sheet 18 of a tube nest 19. The tube nest comprises a plurality of parallel longitudinally extending tubes 20 connected to tube sheet. 18 at one end and a tube sheet 21 at the opposite end. The. dome member 15 is formed with an induction port 22 and an eduction port 23 communicating with the compartments 24 and 25, into which the domes divided by the partition walls 16.
The compartment 24 as seen in Fig.2 is of relatively small sectional area and communicates with a small number of tubes 20, as compared with the aggregate number of tubes in the tube nest. The compartment 25 communicates with the remaining tubes. All of the tubes terminatin in the tube sheet 21 are in communication y a cap 26 which is secured over the end of'the tube sheet 21 and diverts the fluid passing through the tube sheets in communication with compartment 24 to the tubes communicating with the enlarged compartment 25.
The entire volume of fluid circulating through the shell passes from induction 'open through the induction opening 22 of the dome passes at high velocity throughthe tubes in communication with the compartment 24 and, of course, in the same direction, as the direction of flow of the fluid in the shell.
.ing 11 to eduction opening 12 in the direction of the arrow a,. The fluid delivered When passing through the ends of the tubes in the tube nest 21 the fluid from compartment 24 will return in counterflow through the tubes which communicate with compartment 25 and in the direction of the arrow an eduction port are provided upon opposite sides of the partition wall 28. The end of the shell adjacent the ports is closed by a tube sheet 31 on the outside of which is a cylindrical dome 32. The dome is provided with a cover plate 33 and is divided into passageways 34, 35, 36 and 37. These passageways are formed by radially extending'partition walls, as indicated more particularly in section in Fig. 4 ofthe drawings. v
A fluid induction port 38 communicates with the segmental passageway 34 and a fluid eduction port 39 communicates with the segmental compartment 37 'of the dome.' The compartments 34 and 37 are sectors of the circle, each being measured by substantially onesixth of the circumference of the circle and separated by a partition wall 40 which also separates the induction port 38 and the eduction port 39. The compartments 35 and 36 are sectors of the circle, each including sub-. stantially one-third of the circumference of' the circle and divided by a partition wall 41 extending diametrically opposite from the partition wall 40. The compartments 34 and 35 are separated by radially extending partition wall 42 and the compartments 36 and 37 are separated by radially extending partition wall 43. The opposite end of the shell 27 from the end upon which the cylindrical dome 32 is mounted'isclosed by a tube sheet 44, on the outside of. which isa cap 45. The
cap 45 is divided into three compartments of sector shape, as indicated at 46, 47 and 48. These compartments are separated by radially extending walls. Such a wall 49 separates compartments 46.a nd 47, and wall 50 separates compartments 47 and 48, and a wall ,51 separates compartments 46 and 48.
By comparing Figs. 4 and 5 of the drawings, it willbe seen that wall'40 in the dome 32 is in the same plane and in longitudinal alignment with wall 51 oflthe cap 45, and that walls 49 and 50 in the cap .45 are 'spaced at one hundred twenty degrees to wall 51, so that viewed collectively the radial 'walls in the dome 32 and the cap are arranged at sixty degrees to each other, which divides the set of tubes into six sets indicated by the reference characters A, B, C, D, E and F, each set being defined by a sector representing approximately one-sixth of the sectional area of the shell.
In operation of the apparatus shown in. Figs. 3 to 5 inclusive, a fluid to be cooled may pass into the shell 27 through induction port 29 and then flow lengthwise of the shell along the passageway of the semi-circular section, as defined by the shell wall, and the longitudinal partition member 28. When the fluid has reached the opposite end of the partition member from its induction end, it will pass around the end of the partition member 28 and between this end and the tube sheet 44 through a passageway '52. 'The fluid will then return along the lower passageway of semicircular section to the eduction port 30.
Cooling fluid is delivered to the dome 32 through induction port 38 and into compartment 34 defined b the radial walls 40 and 42. The cooling fli iid will then flov; lengthwise of the set of tubes indicate! by the character A. This fluid will pass out of this set of tubes A and into compartment 46 formed in the cap 45 at the opposite end of the shell. The compartment 46 is represented by a sector of twice the arcuate length of compartment 34 and soarranged that the compartment 46 will overlap the compartment 34 by. substantially one-half its arcuate length. This will cause the fluid which flowed through the pipes A in exclusive communication with compartment 34 to be diverted into pipes B exclusively communicating with the compartment 46 at the cap end.
of the shell and the compartment 35, at the dome end of the shell.
The fluid which has now assed to compartment 35 in the dome by owing through tubes B will be diverted from compartment 35 to tubes C which communicate with the other half of compartment 35 and extend to the opposite end of the shell where they communicate with compartment 47 of the cap. The fluid will then flow through compartment 47 of the cap. The fluid will then find its way into the set of tubes D in communication with the compartment 47 at one end and the compartment 36 in the dome. The fluid in compartment 36 will be diverted from the set of tubes D to the set of tubes E and will again flow throughout the length of the shell to compartment 48 in the cap. Here the fluid will pass from pipes E into compartment 48. and then into tu es F which communicate with this compartment and also cor'nmunlcate at the opposite end with compartment 37 of the dome. When the fluid reaches this compartment it passes from the exchanger through education port 38.
By considering the apparatus, it will thus be evident that in. a shell of relativel small area and length it is possible to o tain a large area of heat exchan e surface distributed throughout length 0 fluid passageway while the fluid is flowing countercurrent. By further analysis it will be seen that in the upper half of the heat exchanger, fluid flows in the direction of the arrow --or- I claim and desire to secure by Letters Patand that in the lower passageway the fluid flows in the direction of the arrow 'b--. However, the cooling fluid which flows through the tubes makes six passes while the fluid in the shell makes two passes. Thus, the two fluids will be unidirectional in their flow while fluid passes through the groups of pipes B and E and will flow in counter direction in pipes A, C, D and F. This insures that the fluids will only have one-third of their flow unidirectional and that two-thirds of their flow will be in a counterdirection which is desirable for producing eflicient heat exchange in a multi-pass apparatus.
While I have shown the preferred form of my invention as now known to me, it is to be understood that various changes may be made in its construction without departing from the spirit of the invention as defined in the appended claim.
Equally it is to be understood that the cooling medium and the medium to be cooled may each flow either through shell or tubes.'
Having thus described my invention, what ent is:
In a device of the character described, a shell through which a'fluid flows longitudinally from end to end of the shell and returns in a single pass in each direction, a tube nest extending longitudinally of the .shell and through which a cooling medium flows, means at the opposite ends of the tube nest for dividing the tubes into three times as many groups as there are longitudinal passes of the fluid in the shell and creating a circulation of a cooling medium through said tubes in a manner to establish a countercurrent flow of the two fluids in a ratio of one portion parallel current to two portions countercurrent.
CARL F. BRA-UN.
US132694A 1926-08-31 1926-08-31 Heat-exchanging apparatus Expired - Lifetime US1683236A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US132694A US1683236A (en) 1926-08-31 1926-08-31 Heat-exchanging apparatus

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US132694A US1683236A (en) 1926-08-31 1926-08-31 Heat-exchanging apparatus

Publications (1)

Publication Number Publication Date
US1683236A true US1683236A (en) 1928-09-04

Family

ID=22455171

Family Applications (1)

Application Number Title Priority Date Filing Date
US132694A Expired - Lifetime US1683236A (en) 1926-08-31 1926-08-31 Heat-exchanging apparatus

Country Status (1)

Country Link
US (1) US1683236A (en)

Cited By (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4147209A (en) * 1975-08-27 1979-04-03 Skf Industrial Trading And Development Company B.V. Corrosion resistant heat exchanger
US4694896A (en) * 1985-11-05 1987-09-22 Frank Navratil Heat exchanger
US4706646A (en) * 1986-03-27 1987-11-17 M.A.C., Inc. Total counterflow heat exchanger
US4858681A (en) * 1983-03-28 1989-08-22 Tui Industries Shell and tube heat exchanger
US4871014A (en) * 1983-03-28 1989-10-03 Tui Industries Shell and tube heat exchanger
US6012514A (en) * 1997-11-26 2000-01-11 Swain; Robert L. B. Tube-in tube heat exchanger
US6668914B2 (en) * 2000-03-29 2003-12-30 Sgl Acotec Gmbh Multiple tube bundle heat exchanger
US20050067153A1 (en) * 2003-09-30 2005-03-31 Wu Alan K. Tube bundle heat exchanger comprising tubes with expanded sections
US8495859B2 (en) 2006-11-15 2013-07-30 Modine Manufacturing Company Heat recovery system and method
US20140262162A1 (en) * 2013-03-15 2014-09-18 Caloris Engineering, LLC Liquid to liquid multi-pass countercurrent heat exchanger
US10295266B2 (en) 2015-07-14 2019-05-21 Holtec International Tubular heat exchanger having multiple shell-side and tube-side fluid passes

Cited By (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4147209A (en) * 1975-08-27 1979-04-03 Skf Industrial Trading And Development Company B.V. Corrosion resistant heat exchanger
US4858681A (en) * 1983-03-28 1989-08-22 Tui Industries Shell and tube heat exchanger
US4871014A (en) * 1983-03-28 1989-10-03 Tui Industries Shell and tube heat exchanger
US4694896A (en) * 1985-11-05 1987-09-22 Frank Navratil Heat exchanger
US4706646A (en) * 1986-03-27 1987-11-17 M.A.C., Inc. Total counterflow heat exchanger
US6012514A (en) * 1997-11-26 2000-01-11 Swain; Robert L. B. Tube-in tube heat exchanger
US6668914B2 (en) * 2000-03-29 2003-12-30 Sgl Acotec Gmbh Multiple tube bundle heat exchanger
US20050067153A1 (en) * 2003-09-30 2005-03-31 Wu Alan K. Tube bundle heat exchanger comprising tubes with expanded sections
WO2005031235A1 (en) 2003-09-30 2005-04-07 Dana Canada Corporation Tube bundle heat exchanger comprising tubes with expanded sections
US7240723B2 (en) 2003-09-30 2007-07-10 Dana Canada Corporation Tube bundle heat exchanger comprising tubes with expanded sections
US8495859B2 (en) 2006-11-15 2013-07-30 Modine Manufacturing Company Heat recovery system and method
US20140262162A1 (en) * 2013-03-15 2014-09-18 Caloris Engineering, LLC Liquid to liquid multi-pass countercurrent heat exchanger
US9885523B2 (en) * 2013-03-15 2018-02-06 Caloris Engineering, LLC Liquid to liquid multi-pass countercurrent heat exchanger
US10295266B2 (en) 2015-07-14 2019-05-21 Holtec International Tubular heat exchanger having multiple shell-side and tube-side fluid passes

Similar Documents

Publication Publication Date Title
US1893484A (en) Heat exchanger
US1683236A (en) Heat-exchanging apparatus
US2870997A (en) Heat exchanger
US2730337A (en) Heat exchanger
US2372079A (en) Heat exchanger
US2188975A (en) Multiple heat exchange unit
US2418191A (en) Heat exchanger
US2703701A (en) Heat exchanger
US1916768A (en) Heat exchanger
US1578830A (en) Heat exchanger
US3006612A (en) Heat exchangers
US1338479A (en) Heat-transfer apparatus
US1990251A (en) Heat exchange apparatus
US3731733A (en) Tube-group heat exchangers
US2715516A (en) Heat exchanger design
US1692391A (en) Heat-transfer apparatus
US1325637A (en) harrison
US2155666A (en) Heat exchange unit
US2467741A (en) Heat exchange apparatus
US1509566A (en) Air cooler
US2022173A (en) Heat transfer apparatus
US1505429A (en) Heat-exchange apparatus
GB200463A (en) Improvements in and relating to heat-exchanging elements for use in radiators, condensers and like heating and cooling apparatus
US1602287A (en) Heat exchanger
US1615658A (en) Heat exchanger