US2268386A - Heat exchanger apparatus - Google Patents

Heat exchanger apparatus Download PDF

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Publication number
US2268386A
US2268386A US311453A US31145339A US2268386A US 2268386 A US2268386 A US 2268386A US 311453 A US311453 A US 311453A US 31145339 A US31145339 A US 31145339A US 2268386 A US2268386 A US 2268386A
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United States
Prior art keywords
heat exchanger
conduit
chamber
manifold
exchanger apparatus
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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
US311453A
Inventor
Harold W Fisher
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Standard Oil Development Co
Original Assignee
Standard Oil Development Co
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.)
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Publication date
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Priority to US311453A priority Critical patent/US2268386A/en
Application granted granted Critical
Publication of US2268386A publication Critical patent/US2268386A/en
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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01NGAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR MACHINES OR ENGINES IN GENERAL; GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR INTERNAL COMBUSTION ENGINES
    • F01N5/00Exhaust or silencing apparatus combined or associated with devices profiting by exhaust energy
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F28HEAT EXCHANGE IN GENERAL
    • F28DHEAT-EXCHANGE APPARATUS, NOT PROVIDED FOR IN ANOTHER SUBCLASS, IN WHICH THE HEAT-EXCHANGE MEDIA DO NOT COME INTO DIRECT CONTACT
    • F28D21/00Heat-exchange apparatus not covered by any of the groups F28D1/00 - F28D20/00
    • F28D21/0001Recuperative heat exchangers
    • F28D21/0003Recuperative heat exchangers the heat being recuperated from exhaust gases
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F28HEAT EXCHANGE IN GENERAL
    • F28DHEAT-EXCHANGE APPARATUS, NOT PROVIDED FOR IN ANOTHER SUBCLASS, IN WHICH THE HEAT-EXCHANGE MEDIA DO NOT COME INTO DIRECT CONTACT
    • F28D7/00Heat-exchange apparatus having stationary tubular conduit assemblies for both heat-exchange media, the media being in contact with different sides of a conduit wall
    • F28D7/02Heat-exchange apparatus having stationary tubular conduit assemblies for both heat-exchange media, the media being in contact with different sides of a conduit wall the conduits being helically coiled
    • F28D7/024Heat-exchange apparatus having stationary tubular conduit assemblies for both heat-exchange media, the media being in contact with different sides of a conduit wall the conduits being helically coiled the conduits of only one medium being helically coiled tubes, the coils having a cylindrical configuration
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F28HEAT EXCHANGE IN GENERAL
    • F28FDETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
    • F28F9/00Casings; Header boxes; Auxiliary supports for elements; Auxiliary members within casings
    • F28F9/24Arrangements for promoting turbulent flow of heat-exchange media, e.g. by plates
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F28HEAT EXCHANGE IN GENERAL
    • F28DHEAT-EXCHANGE APPARATUS, NOT PROVIDED FOR IN ANOTHER SUBCLASS, IN WHICH THE HEAT-EXCHANGE MEDIA DO NOT COME INTO DIRECT CONTACT
    • F28D21/00Heat-exchange apparatus not covered by any of the groups F28D1/00 - F28D20/00
    • F28D2021/0019Other heat exchangers for particular applications; Heat exchange systems not otherwise provided for
    • F28D2021/008Other heat exchangers for particular applications; Heat exchange systems not otherwise provided for for vehicles
    • 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T10/00Road transport of goods or passengers
    • Y02T10/10Internal combustion engine [ICE] based vehicles
    • Y02T10/12Improving ICE efficiencies
    • 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
    • Y10S165/416Extending transverse of shell, e.g. fin, baffle
    • Y10S165/417Extending transverse of shell, e.g. fin, baffle including spacer or support for transverse tube support or shell-side flow director

Definitions

  • the present invention relates to a heat exchange apparatus, and more particularly, it relates to a device in which provision is made for a high quantity of ow of a hot iluid with a minimum imposition of back pressure on the source of said fluid.
  • the apparatus provides for the heating of a cool or cold fluid material by means of hot exhaust gases, as from an internal combustion engine under the initial pressure of said gases.
  • Fig. 1 is a vertical section through a device of the character set forth;
  • Fig. 2 is a sectional view of the apparatus taken along the line II-II of Fig. 1.
  • the numeral I designates the shell of an enlarged chamber in an exhaust manifold line, or the like, connected in the line by means of the reducer portions 2.
  • a core member which as shown, is composed of a plurality of sections joined as a unit by a tie rod 3.
  • each section is composed of a rim element 4, having inwardly extending radial arms 5 and a hub portion 6.
  • Substantially triangular vanes 1 are disposed coextensively with an edge of each arm, with the apex portion adjacent the hub.
  • the vanes may be inclined slightly in a clockwise or counterclockwise direction, to impart a turbulent or pointed toward the walls, their apexes adjacent to those of the next section in such fashion as to provide a series of open receptacles disposed in augment along a helically curved path.
  • 'I'he l maximum diameter of yeach section or of the core is so adjusted as to provide for a space between the bottom of the grooves or receptacles 9 and the inner wall of the manifold I in which may be disposed a conduit I0 helically wound about the separator lns 8 of each core section.
  • the outer diameter of the core is such that when the conduit Ill is wound about the iin portions 8, the entire assembly may be snugly inserted within the manifold or chamber I, with the conduit in 'surface contact with the chamber walls. Suitable inlet and outlet connections with this conduit are provided in the manifold Wall as at II' and I2 respectively. An insulating cover I3 is provided for the manifold in order to reduce heat loss through the manifold.
  • a stream of exhaust gases may )be passed through:
  • a heat exchanger device of the character described comprising a tubular chamber in a iluid conduit system, and an exchanger assembly for said chamber consisting of a core of a. plu- Irality of substantially annular baille elements each having a rim, a hub, a plurality of spaced, vaned arms radially between the hub and rim, and a plurality of narrow, elongated fin elements disposed in right angular relation to the edge of said rim and spaced peripherally thereof, a tie rod extending centrally of said baille elements holding them in substantially rigid, spaced relation, the ends of the ns on one element abutting against those of the next adjacent elements, a
  • a heat-exchanger device of the character described comprising a tubular chamber in a uid conduit system, and an exchanger assembly i'or ⁇ said chamber consisting of a core of a pluralityy of substantially annular baille elements each having a rim, a hub, a plurality of spaced, vaned arms radially between the hub and rim, the vanes being inclined to impart turbulent motion to iluid moving through the chamber, and a plurality of narrow, elongated iin elements disposed in right angular relation to the edge ⁇ of said rim and spaced peripherally thereof, a

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Thermal Sciences (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Fluid Mechanics (AREA)
  • Heat-Exchange Devices With Radiators And Conduit Assemblies (AREA)

Description

Patented Dec. 30, 1941 HEAT EXCHANGER APPARATUS Harold W. Fisher, Cranford, N. J., assigner to Standard Oil Development Company, a corporation of Delaware Application December 29, 1939, Serial No. 311,453-
2 Claims.
The present invention relates to a heat exchange apparatus, and more particularly, it relates to a device in which provision is made for a high quantity of ow of a hot iluid with a minimum imposition of back pressure on the source of said fluid. Specically, the apparatus provides for the heating of a cool or cold fluid material by means of hot exhaust gases, as from an internal combustion engine under the initial pressure of said gases.
It is an object of the present invention to provide a means for boiling a liquid for use as in the generator of an absorption type refrigeration system. It is also an object of the invention to provide a combined heat exchanger device and exhaust muilier for use with internal combustion engines. 'I'hese and other objects of the invention may be fully understood from the following description, when it is read in conjunction 'with the accompanying drawing, in which Fig. 1 is a vertical section through a device of the character set forth; and
Fig. 2 is a sectional view of the apparatus taken along the line II-II of Fig. 1.
Referring to the drawing, the numeral I designates the shell of an enlarged chamber in an exhaust manifold line, or the like, connected in the line by means of the reducer portions 2. Within the chamber is disposed a core member, which as shown, is composed of a plurality of sections joined as a unit by a tie rod 3. As more clearly illustrated by Fig. 2, each section is composed of a rim element 4, having inwardly extending radial arms 5 and a hub portion 6. Substantially triangular vanes 1 are disposed coextensively with an edge of each arm, with the apex portion adjacent the hub. The vanes may be inclined slightly in a clockwise or counterclockwise direction, to impart a turbulent or pointed toward the walls, their apexes adjacent to those of the next section in such fashion as to provide a series of open receptacles disposed in augment along a helically curved path. 'I'he l maximum diameter of yeach section or of the core is so adjusted as to provide for a space between the bottom of the grooves or receptacles 9 and the inner wall of the manifold I in which may be disposed a conduit I0 helically wound about the separator lns 8 of each core section. As illustrated, the outer diameter of the core is such that when the conduit Ill is wound about the iin portions 8, the entire assembly may be snugly inserted within the manifold or chamber I, with the conduit in 'surface contact with the chamber walls. Suitable inlet and outlet connections with this conduit are provided in the manifold Wall as at II' and I2 respectively. An insulating cover I3 is provided for the manifold in order to reduce heat loss through the manifold.
In the apparatus as shown in Fig. 1, a stream of exhaust gases may )be passed through: the
.manifold I from left to right, while a stream of low boiling refrigerant liquid is led through the conduit I0 from right to left. The exhaust gases striking the vanes 'i are set into turbulent motion swirling outwardly against the fins 8 and with a wiping action over the conduit Ill, providing an intimate contact with all of the elements disposed in the manifold. The heat from the exhaust gases is indirectly transferred to the liquid not only by conduction through the direct contact of gases with the surface of the conduit,
but also indirectly through the core sections and fin members in contact with said conduit.
Although as described, emphasis has been placed on the utility of the device as'a heat exchanger, it should be apparent that by properly proportioning the size of the vanes'l and by suitable adjustment of the angle of their inclination, the structure set forth may function simultaneously as a muiiier for explosion motors of whatever type desired. Likewise, while described in connection with its possible .suitability for use in .conjunction with a refrigerating unit, it should be obvious that the structure is adaptable for use in any structural combination inwhich it is desired to utilize a uid heat exchanger in which it is desired that the flow of the heated medium be not too greatly restricted.
Obviously the apparatus and its utilization may be varied within wide limits without departing from the inventive concept disclosed, and it is not intended 'that the invention shall be limited by any disclosure set forth for the purpose of illustration, but only by the appen'ded claims.
Iciaim:
l. A heat exchanger device of the character described, comprising a tubular chamber in a iluid conduit system, and an exchanger assembly for said chamber consisting of a core of a. plu- Irality of substantially annular baille elements each having a rim, a hub, a plurality of spaced, vaned arms radially between the hub and rim, and a plurality of narrow, elongated fin elements disposed in right angular relation to the edge of said rim and spaced peripherally thereof, a tie rod extending centrally of said baille elements holding them in substantially rigid, spaced relation, the ends of the ns on one element abutting against those of the next adjacent elements, a
series of grooves in the edge portion of each iin element, and a helically wound conduit member disposed in said grooves in surface vcontact with said iins andthe chamber wall, said conduit having inlet and outlet connections through the chamber wall.
2. A heat-exchanger device of the character described, comprising a tubular chamber in a uid conduit system, and an exchanger assembly i'or `said chamber consisting of a core of a pluralityy of substantially annular baille elements each having a rim, a hub, a plurality of spaced, vaned arms radially between the hub and rim, the vanes being inclined to impart turbulent motion to iluid moving through the chamber, and a plurality of narrow, elongated iin elements disposed in right angular relation to the edge `of said rim and spaced peripherally thereof, a
ber wall.
US311453A 1939-12-29 1939-12-29 Heat exchanger apparatus Expired - Lifetime US2268386A (en)

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Cited By (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3180245A (en) * 1962-03-12 1965-04-27 Jr Theodore A Erickson Air mixer for air streams
US3211215A (en) * 1961-02-01 1965-10-12 Gen Motors Corp Heat exchangers suitable for space use
US3235003A (en) * 1963-06-04 1966-02-15 Cloyd D Smith Spiral flow baffle system
US3736961A (en) * 1971-11-10 1973-06-05 R Walsh Heat exchanger for furnace pipes and the like
WO1980000368A1 (en) * 1978-07-28 1980-03-06 Fuelsaver Co Method and apparatus for improving heat transfer
US4364754A (en) * 1981-04-13 1982-12-21 Century 21 Pollution Control, Inc. Apparatus for separating foreign matter from a gas with a heat exchanger
US4382807A (en) * 1981-04-13 1983-05-10 Century 21 Pollution Control, Inc. Apparatus for separating foreign matter from a gas with a heat exchanger
US4493368A (en) * 1981-06-22 1985-01-15 Norsk Hydro A.S. Helical flow heat exchanger having individually adjustable baffles
US5375653A (en) * 1992-09-10 1994-12-27 The Procter & Gamble Company Heat exchanger system with turbulator for particle-in-liquid dispersion
US5727398A (en) * 1996-07-25 1998-03-17 Phillippe; Gary E. Refrigerant agitation apparatus
US20090025392A1 (en) * 2007-07-25 2009-01-29 Georg Wirth Flow guide device as well as exhaust system equipped therewith

Cited By (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3211215A (en) * 1961-02-01 1965-10-12 Gen Motors Corp Heat exchangers suitable for space use
US3180245A (en) * 1962-03-12 1965-04-27 Jr Theodore A Erickson Air mixer for air streams
US3235003A (en) * 1963-06-04 1966-02-15 Cloyd D Smith Spiral flow baffle system
US3736961A (en) * 1971-11-10 1973-06-05 R Walsh Heat exchanger for furnace pipes and the like
WO1980000368A1 (en) * 1978-07-28 1980-03-06 Fuelsaver Co Method and apparatus for improving heat transfer
US4364754A (en) * 1981-04-13 1982-12-21 Century 21 Pollution Control, Inc. Apparatus for separating foreign matter from a gas with a heat exchanger
US4382807A (en) * 1981-04-13 1983-05-10 Century 21 Pollution Control, Inc. Apparatus for separating foreign matter from a gas with a heat exchanger
US4493368A (en) * 1981-06-22 1985-01-15 Norsk Hydro A.S. Helical flow heat exchanger having individually adjustable baffles
US5375653A (en) * 1992-09-10 1994-12-27 The Procter & Gamble Company Heat exchanger system with turbulator for particle-in-liquid dispersion
US5727398A (en) * 1996-07-25 1998-03-17 Phillippe; Gary E. Refrigerant agitation apparatus
US20090025392A1 (en) * 2007-07-25 2009-01-29 Georg Wirth Flow guide device as well as exhaust system equipped therewith
US8572949B2 (en) * 2007-07-25 2013-11-05 Eberspächer Exhaust Technology GmbH & Co. KG Flow guide device as well as exhaust system equipped therewith

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