US2595822A - Spring seal for tube and shell heat exchangers - Google Patents

Spring seal for tube and shell heat exchangers Download PDF

Info

Publication number
US2595822A
US2595822A US123400A US12340049A US2595822A US 2595822 A US2595822 A US 2595822A US 123400 A US123400 A US 123400A US 12340049 A US12340049 A US 12340049A US 2595822 A US2595822 A US 2595822A
Authority
US
United States
Prior art keywords
shell
tube
disk
truncated
tubes
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
US123400A
Inventor
Uggerby William
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.)
Young Radiator Co
Original Assignee
Young Radiator 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.)
Filing date
Publication date
Application filed by Young Radiator Co filed Critical Young Radiator Co
Priority to US123400A priority Critical patent/US2595822A/en
Application granted granted Critical
Publication of US2595822A publication Critical patent/US2595822A/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
    • F28F9/00Casings; Header boxes; Auxiliary supports for elements; Auxiliary members within casings
    • F28F9/22Arrangements for directing heat-exchange media into successive compartments, e.g. arrangements of guide 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
    • 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
    • F28D7/16Heat-exchange apparatus having stationary tubular conduit assemblies for both heat-exchange media, the media being in contact with different sides of a conduit wall the conduits being arranged in parallel spaced relation
    • F28D7/1607Heat-exchange apparatus having stationary tubular conduit assemblies for both heat-exchange media, the media being in contact with different sides of a conduit wall the conduits being arranged in parallel spaced relation with particular pattern of flow of the heat exchange media, e.g. change of flow direction
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F28HEAT EXCHANGE IN GENERAL
    • F28FDETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
    • F28F9/00Casings; Header boxes; Auxiliary supports for elements; Auxiliary members within casings
    • F28F9/02Header boxes; End plates
    • F28F9/0219Arrangements for sealing end plates into casing or header box; Header box sub-elements
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F28HEAT EXCHANGE IN GENERAL
    • F28FDETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
    • F28F2230/00Sealing means
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F28HEAT EXCHANGE IN GENERAL
    • F28FDETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
    • F28F2275/00Fastening; Joining
    • F28F2275/20Fastening; Joining with threaded elements
    • 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
    • Y10S165/42Segmented plate

Definitions

  • a gap between a baflle and the shell or a distortion or displacement of the baffle might result in a failure to have the desired fluid-tight contact of the baffle with the shell throughout its entire periphery.
  • the main objects of this invention are to provide an improved form of baflle construction for use with tube and shell heat-exchangers; to provide an improved peripheral formation of baflles of this kind which facilitates the insertion of the tube and baffle assembly, with its header supports, into the shell so as to secure a practically fluid-tight seal between the 'bafiles and the shell; to provide an improved, yielding, peripheral seal for baifies in structures of this kind which can be placed on the bafiies either before or after assembly with the tubes, and which will yield sufliciently to allow the tube and bafile as sembly to slide into the shell with the application of very little pressure and be completely free from the danger of distorting or displacing any of the bafiles, or leaving gaps between the baflies and shell; and to provide a yielding peripheral seal of this kind which is economical to manufacture and assemble and which eliminates practically all possibility of by-pass leaks around the bafiles.
  • Fig. 1 is a side elevation of a tube and shell heat-exchanger of the type wherewith baflles constructed in accordance with this invention are particularly adapted for use;
  • Fig. 2 is an enlarged, fragmentary, cross-sectional, elevation of one end of a tube and shell heat-exchanger equipped with bailles embodying this invention and showing the manner of mounting one end of the tube and bafile assembly on the shell;
  • Fig. 3 is an exploded perspective view of one of the disks and spring seal which constitute this improved form of baflle;
  • Fig. 4 is an enlarged view of the same showing the spring seal in place on the disk.
  • a tube and shell heat-exchanger 5 Wherewith spring-sealed bafiies 6 embodying this invention are adapted for use, comprises a core unit I telescoped into a shell 8 to provide for the exchange of heat between two fluids of diiiering temperatures flowing through and around the core unit 7.
  • lhe core unit 7 comprises a bundle of tubes 9 arranged in parallel, radially-spaced relationship and bonded at their ends to header-plates it, thereby forming a labyrinth Hv around the tubes 8 intermediate the header-plates l0 and Within the shell 8.
  • the shell 8 is a cylindrical casting provided with a fluid inlet l2 and a fluid outlet I3 communicating with the core-labyrinth II and having the open ends of the shell closed with end plates I4 wherein are formed ports [5 communicating with the tubes 9.
  • Yielding support for one end of the core unit 7 within the shell is provided to allow for the expansion and contraction of the core unit 7.
  • this involves a diaphragm l6 clamped between a pair of rings l1 and i8, and between a shell-flange I9 and the ported plate Hi.
  • the rings H and I8 are secured together by suitable bolts and nuts 20, with the inner ring ii bonded to the adjacent header-plate I 0 by a sleeve 21.
  • the ported plate [4 is secured to the shell flange 9 by suitable bolts and nuts 22.
  • a spring-sealed baffle 6, constructed in accordance with this invention, comprises a truncated, apertured disk or plate 24 and a truncated ring 25 of channel-shaped cross-section embracing the peripheral portion of said disk 24.
  • the truncated rin 25 is formed with one end of each of the parallel sections extended beyond the other to provide shoulders 27. After the disk 24 and ring 25 are assembled, these shoulders are struck down, as shown in Fig. 4, to insure the retention of the truncated ring 25 on the truncated disk i i.
  • a plurality of such baffies 6 are assembled on the bundle of tubes a, being spaced apart axially so that when in the shell 8 they divide the labyrinth H into a plurality of compartments communicating through the spaces 25 between the cut-off part of each disk 24 and the shell 8.
  • Adjacent baflies are oppositely disposed so as to direct a normal fluid flow axially through said shell in a constantly-reversing radial direction.
  • the truncated ring 25 is formed of spring material with the internal diameter of the channel slightly greater than the diameter of the disk 24, and the channel so formed that it fits the disk 24 snugly and forms a practically fluid-tight contact therewith. (See Fig. 2.)
  • the truncated rings 25 compress slightly to accommodate the external circumference of the ring 24 to that of the interior wall of the shell 8, and provide a practically fluid-tight seal around the peripheral part of the ring 25.
  • truncated rings 25 To assemble a truncated ring 25 on a truncated disk 24 they are placed in parallel axial alinement and the ring is sprung sufliciently to allow the sidewise insertion of the disk into the ring.
  • the truncated rings 25 may be assembled on the truncated disks 24 before or after the disks have been assembled on the tubes I I.
  • a secondary advantage of this form of springseal bafile is that the core unit 7 may be easily removed for repair or cleaning.
  • a battle for tube and shell heat-exchangers comprising, a plate apertured for assembly on a bundle of parallel radially-spaced tubes bonded to headers and thereafter insertable into a shell whereby said plate divides the interior of said shell around said tubes into separate compartments on opposite sides of said plate, and an arcuate-shaped spring metal element embracing a major peripheral portion of said plate and circumferentially contractible in the plane of said plate to permit the sliding insertion of said tubesupported plate into said shell and thereby form a practically fluid-tight seal between said compartments around said major peripheral portion of said plate but allowing communication between said compartments around that peripheral portion of the plate not embraced by said element.
  • a barier for tube and shell heat-exchangers comprising, a truncated disk apertured for assembly on a bundle of parallel radially-spaced tubes bonded to supporting headers and thereafter insertable into a shell whereby said disk divides the interior of said shell around said tubes into separate compartments on opposite sides of said disk, a truncated spring metal ring of channel-shaped cross-section embracing the circumferential peripheral portion of said disk and contractible in the plane of said disk to permit the sliding insertion of said tube-supported disk into said shell to form a practically fluid-tight seal between said compartments around said peripheral portion of said disk.
  • a heat-exchanger core of the class described for assembly with a supporting shell comprising, a bundle of parallel radially-spaced tubes spanning and bonded at their ends to header plates, a plurality of apertured truncated disks assembled on said tubes in axially-spaced relationship with the truncated portions of adjacent disks oppositely disposed to form bafiles dividing said shell into communicating compartments and directing a fluid flow axially through said shell in a constantly-reversing radial direction, and an armate-shaped spring metal element of channelshaped cross-section embracing the circumferential peripheral portions of each of the respective disks and each independently circumferentially contractible in the plane of the respective disks to permit a sliding insertion of said core into a shell, whereby said yielding elements form a practically fluid-tight seal between said compartments and said shell and the peripheral portions of said disks.
  • a heat-exchanger core unit comprising a bundle of parallel radially-spaced tubes spanning and bonded at their ends to header plates, a plurality of apertured truncated disks assembled on said tubes in axiallyspaced relationship with the truncated portions of adjacent disks oppositely disposed to form bafiies dividing said shell into communicating compartments and directing a fluid flow axially through said shell in constantly-reversing radial direction, and a truncated spring metal ring of channel-shaped cross-section embracing the peripheral portion of each of said disks and ex pansible and contractible in the plane of the respective disks to insure contacting of the periphcry of each ring the interior of said shell to form a practically fluid-tight seal between said compartment around said shell and the peripheral portions of said disks.
  • a barier for tube and shell heat-exchangers comprising, a truncated disk apertured for assembly on a bundle of parallel radially-spaced tubes bonded to supporting headers and thereafter insertable into a shell whereby said disk divides the interior of said shell around said tubes into separate compartments on opposite sides of said disk, an arcuate-shaped spring metal element of channel-shaped cross-section with an inside diameter of the channel normally slightly greater than the diameter of said disk to permit a yielding embracing of said element around the circumferential periphery of said disk and circumferentially contractible in the plane of said disk to permit the sliding insertion of said tube-supported disk into said shell and form a practically fluid-tight seal between said compartments around said disk, and shouldersformed at the ends of said arcuate-shaped element adapted to engage the edge of the subtended periphery of said truncated disk for removably holding said element in place on said disk.

Landscapes

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

Description

y 6, 1952 w. UGGERBY 2,595,822
SPRING SEAL FOR TUBE AND SHELL. HEAT EXCHANGERS Filed on. 25, 1949 IN V EN TOR.
BY @A.
ATmEWW Patented May 6, 1952 SPRING SEAL FOR TUBE AND SHELL HEAT EXCHANGERS William Uggerby, Racine, Wis., assignor to Young Radiator Company, Racine, Wis., a corporation of Wisconsin Application October 25, 1949, Serial No. 123,400
In the manufacture of tube and shell heatexchangers, of the type wherewith this invention is adaptable, as they have heretofore been constructed, one of the problems has been to insure a satisfactory fluid-tight contact of the bafiies of the tube assembly with the shell. Obviously, this is essential in order to preclude the fluid by-passing its normal flow around the cutoff section of the baffie, and thereby reduce the efiieiency of the heat-exchanger. The core unit of tubes, headers, and baflles, is first assembled and then slid into the shell. Of necessity this must be a press-fit operation for the bafiles. If, perchance, a baflie is slightly over-size, or undersize, and/or not truly concentric with the shell axis, a gap between a baflle and the shell or a distortion or displacement of the baffle might result in a failure to have the desired fluid-tight contact of the baffle with the shell throughout its entire periphery.
The main objects of this invention, therefore, are to provide an improved form of baflle construction for use with tube and shell heat-exchangers; to provide an improved peripheral formation of baflles of this kind which facilitates the insertion of the tube and baffle assembly, with its header supports, into the shell so as to secure a practically fluid-tight seal between the 'bafiles and the shell; to provide an improved, yielding, peripheral seal for baifies in structures of this kind which can be placed on the bafiies either before or after assembly with the tubes, and which will yield sufliciently to allow the tube and bafile as sembly to slide into the shell with the application of very little pressure and be completely free from the danger of distorting or displacing any of the bafiles, or leaving gaps between the baflies and shell; and to provide a yielding peripheral seal of this kind which is economical to manufacture and assemble and which eliminates practically all possibility of by-pass leaks around the bafiles.
In the accompanying drawings:
' Fig. 1 is a side elevation of a tube and shell heat-exchanger of the type wherewith baflles constructed in accordance with this invention are particularly adapted for use;
Fig. 2 is an enlarged, fragmentary, cross-sectional, elevation of one end of a tube and shell heat-exchanger equipped with bailles embodying this invention and showing the manner of mounting one end of the tube and bafile assembly on the shell;
Fig. 3 is an exploded perspective view of one of the disks and spring seal which constitute this improved form of baflle; and
5 Claims. (Cl. 257-236) Fig. 4 is an enlarged view of the same showing the spring seal in place on the disk.
A tube and shell heat-exchanger 5, Wherewith spring-sealed bafiies 6 embodying this invention are adapted for use, comprises a core unit I telescoped into a shell 8 to provide for the exchange of heat between two fluids of diiiering temperatures flowing through and around the core unit 7.
lhe core unit 7 comprises a bundle of tubes 9 arranged in parallel, radially-spaced relationship and bonded at their ends to header-plates it, thereby forming a labyrinth Hv around the tubes 8 intermediate the header-plates l0 and Within the shell 8.
The shell 8 is a cylindrical casting provided with a fluid inlet l2 and a fluid outlet I3 communicating with the core-labyrinth II and having the open ends of the shell closed with end plates I4 wherein are formed ports [5 communicating with the tubes 9.
Yielding support for one end of the core unit 7 within the shell is provided to allow for the expansion and contraction of the core unit 7. In the present embodiment this involves a diaphragm l6 clamped between a pair of rings l1 and i8, and between a shell-flange I9 and the ported plate Hi. As clearly shown in Fig. 2, the rings H and I8 are secured together by suitable bolts and nuts 20, with the inner ring ii bonded to the adjacent header-plate I 0 by a sleeve 21. The ported plate [4 is secured to the shell flange 9 by suitable bolts and nuts 22.
A spring-sealed baffle 6, constructed in accordance with this invention, comprises a truncated, apertured disk or plate 24 and a truncated ring 25 of channel-shaped cross-section embracing the peripheral portion of said disk 24.
As will be noted from Fig. 3, the truncated rin 25 is formed with one end of each of the parallel sections extended beyond the other to provide shoulders 27. After the disk 24 and ring 25 are assembled, these shoulders are struck down, as shown in Fig. 4, to insure the retention of the truncated ring 25 on the truncated disk i i.
A plurality of such baffies 6 are assembled on the bundle of tubes a, being spaced apart axially so that when in the shell 8 they divide the labyrinth H into a plurality of compartments communicating through the spaces 25 between the cut-off part of each disk 24 and the shell 8. Adjacent baflies are oppositely disposed so as to direct a normal fluid flow axially through said shell in a constantly-reversing radial direction.
The truncated ring 25 is formed of spring material with the internal diameter of the channel slightly greater than the diameter of the disk 24, and the channel so formed that it fits the disk 24 snugly and forms a practically fluid-tight contact therewith. (See Fig. 2.) Thus, when the truncated rings 25 are inplace on the disks 24, as shown in Figs. 2 and 4, and the core unit I is slid into the shell 8, the truncated rings 25 compress slightly to accommodate the external circumference of the ring 24 to that of the interior wall of the shell 8, and provide a practically fluid-tight seal around the peripheral part of the ring 25.
To assemble a truncated ring 25 on a truncated disk 24 they are placed in parallel axial alinement and the ring is sprung sufliciently to allow the sidewise insertion of the disk into the ring. The truncated rings 25 may be assembled on the truncated disks 24 before or after the disks have been assembled on the tubes I I.
A secondary advantage of this form of springseal bafile is that the core unit 7 may be easily removed for repair or cleaning.
Although but one specific embodiment of this invention has been herein shown and described, it will be understood that details of the construction shown may be altered without departing 'from the spirit of the invention as defined by the following claims.
I claim:
1. A battle for tube and shell heat-exchangers comprising, a plate apertured for assembly on a bundle of parallel radially-spaced tubes bonded to headers and thereafter insertable into a shell whereby said plate divides the interior of said shell around said tubes into separate compartments on opposite sides of said plate, and an arcuate-shaped spring metal element embracing a major peripheral portion of said plate and circumferentially contractible in the plane of said plate to permit the sliding insertion of said tubesupported plate into said shell and thereby form a practically fluid-tight seal between said compartments around said major peripheral portion of said plate but allowing communication between said compartments around that peripheral portion of the plate not embraced by said element.
2. A baiile for tube and shell heat-exchangers comprising, a truncated disk apertured for assembly on a bundle of parallel radially-spaced tubes bonded to supporting headers and thereafter insertable into a shell whereby said disk divides the interior of said shell around said tubes into separate compartments on opposite sides of said disk, a truncated spring metal ring of channel-shaped cross-section embracing the circumferential peripheral portion of said disk and contractible in the plane of said disk to permit the sliding insertion of said tube-supported disk into said shell to form a practically fluid-tight seal between said compartments around said peripheral portion of said disk.
3. A heat-exchanger core of the class described for assembly with a supporting shell comprising, a bundle of parallel radially-spaced tubes spanning and bonded at their ends to header plates, a plurality of apertured truncated disks assembled on said tubes in axially-spaced relationship with the truncated portions of adjacent disks oppositely disposed to form bafiles dividing said shell into communicating compartments and directing a fluid flow axially through said shell in a constantly-reversing radial direction, and an armate-shaped spring metal element of channelshaped cross-section embracing the circumferential peripheral portions of each of the respective disks and each independently circumferentially contractible in the plane of the respective disks to permit a sliding insertion of said core into a shell, whereby said yielding elements form a practically fluid-tight seal between said compartments and said shell and the peripheral portions of said disks.
4. In a tube and shell heat-exchanger, the combination of a shell, a heat-exchanger core unit comprising a bundle of parallel radially-spaced tubes spanning and bonded at their ends to header plates, a plurality of apertured truncated disks assembled on said tubes in axiallyspaced relationship with the truncated portions of adjacent disks oppositely disposed to form bafiies dividing said shell into communicating compartments and directing a fluid flow axially through said shell in constantly-reversing radial direction, and a truncated spring metal ring of channel-shaped cross-section embracing the peripheral portion of each of said disks and ex pansible and contractible in the plane of the respective disks to insure contacting of the periphcry of each ring the interior of said shell to form a practically fluid-tight seal between said compartment around said shell and the peripheral portions of said disks.
5. A baiile for tube and shell heat-exchangers comprising, a truncated disk apertured for assembly on a bundle of parallel radially-spaced tubes bonded to supporting headers and thereafter insertable into a shell whereby said disk divides the interior of said shell around said tubes into separate compartments on opposite sides of said disk, an arcuate-shaped spring metal element of channel-shaped cross-section with an inside diameter of the channel normally slightly greater than the diameter of said disk to permit a yielding embracing of said element around the circumferential periphery of said disk and circumferentially contractible in the plane of said disk to permit the sliding insertion of said tube-supported disk into said shell and form a practically fluid-tight seal between said compartments around said disk, and shouldersformed at the ends of said arcuate-shaped element adapted to engage the edge of the subtended periphery of said truncated disk for removably holding said element in place on said disk.
WILLIAM UGGERBY.
REFERENCES CITED The following references are of record in the file of this patent:
UNITED STATES PATENTS Number Name Date 1,689,910 Brocklebank Oct. 30, 1928 1,822,698 How Sept. 8, 1931 2,024,209 Doyle et a1 Dec. 17, 1935 2,376,505 Rathbun et a1 May 22, 1945 2,469,785 Alcock May 10, 1949 FOREIGN PATENTS Number Country Date 530,357 Great Britain Dec. 10, 1940
US123400A 1949-10-25 1949-10-25 Spring seal for tube and shell heat exchangers Expired - Lifetime US2595822A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US123400A US2595822A (en) 1949-10-25 1949-10-25 Spring seal for tube and shell heat exchangers

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US123400A US2595822A (en) 1949-10-25 1949-10-25 Spring seal for tube and shell heat exchangers

Publications (1)

Publication Number Publication Date
US2595822A true US2595822A (en) 1952-05-06

Family

ID=22408472

Family Applications (1)

Application Number Title Priority Date Filing Date
US123400A Expired - Lifetime US2595822A (en) 1949-10-25 1949-10-25 Spring seal for tube and shell heat exchangers

Country Status (1)

Country Link
US (1) US2595822A (en)

Cited By (20)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2715516A (en) * 1951-10-25 1955-08-16 Standard Oil Co Heat exchanger design
US2761668A (en) * 1950-12-13 1956-09-04 Smidth & Co As F L Apparatus and method for exchanging heat between solid materials and a fluid medium
US2811337A (en) * 1951-07-20 1957-10-29 Garrett Corp Heat exchanger
US2873098A (en) * 1955-10-03 1959-02-10 Yates American Machine Co Heat exchange apparatus
US2902830A (en) * 1955-07-02 1959-09-08 Lenz William Steam power plants
US3201949A (en) * 1963-08-22 1965-08-24 Vilter Manufacturing Corp Refrigerating apparatus with oil separator means
DE1246776B (en) * 1963-05-15 1967-08-10 Christian Steeb Heat exchanger
DE1258003B (en) * 1963-02-18 1968-01-04 California Research Corp Reactor for hydrocarbon conversions
US4190398A (en) * 1977-06-03 1980-02-26 General Electric Company Gas turbine engine and means for cooling same
US4197907A (en) * 1978-04-05 1980-04-15 Exxon Research & Engineering Co. Floating head support system for shell and tube heat exchanger
US4559996A (en) * 1983-06-03 1985-12-24 Societe Anonyme Dite-Delas-Weir Modular bundle of tubes for a steam condenser, and a steam condenser using such modular bundles
US4660631A (en) * 1980-04-28 1987-04-28 Phillips Petroleum Company Baffle
US4733722A (en) * 1981-11-20 1988-03-29 Serck Industries Limited Shell- and tube-type heat exchangers and their production
US5447195A (en) * 1993-06-11 1995-09-05 Atlas Copco Airpower, Naamloze Vennootschap Heat exchanger
WO2003016813A1 (en) * 2001-08-14 2003-02-27 H2Gen Innovations, Inc. Heat exchange reactor having integral housing assembly
US20040226701A1 (en) * 2003-05-13 2004-11-18 H2Gen Innovations, Inc. Heat exchanger housing and seals
US20080202724A1 (en) * 2003-03-21 2008-08-28 Behr Gmbh & Co. Kg Exhaust Gas Heat Exchanger and Sealing Device for the Same
US20110067837A1 (en) * 2006-06-22 2011-03-24 Harald Schatz Heat exchanger
US20110186276A1 (en) * 2010-01-29 2011-08-04 Casterton Joel T Heat exchanger assembly and method
US10487723B2 (en) * 2015-06-10 2019-11-26 Wärtsilä Finland Oy Charge air cooler arrangement

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1689910A (en) * 1927-11-05 1928-10-30 Foster Wheeler Corp Heat exchanger
US1822698A (en) * 1930-09-04 1931-09-08 Struthers Wells Titusville Cor Baffle packing for heat exchangers
US2024209A (en) * 1934-10-08 1935-12-17 Baldwin Southwark Corp Machine cooling apparatus
GB530357A (en) * 1939-06-22 1940-12-10 Serck Radiators Ltd Improvements relating to coolers for oil and other viscous liquids
US2376505A (en) * 1943-06-30 1945-05-22 Westinghouse Electric & Mfg Co Heat exchange apparatus
US2469785A (en) * 1944-01-29 1949-05-10 Interval Instr Inc Frequency controlled transducer

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1689910A (en) * 1927-11-05 1928-10-30 Foster Wheeler Corp Heat exchanger
US1822698A (en) * 1930-09-04 1931-09-08 Struthers Wells Titusville Cor Baffle packing for heat exchangers
US2024209A (en) * 1934-10-08 1935-12-17 Baldwin Southwark Corp Machine cooling apparatus
GB530357A (en) * 1939-06-22 1940-12-10 Serck Radiators Ltd Improvements relating to coolers for oil and other viscous liquids
US2376505A (en) * 1943-06-30 1945-05-22 Westinghouse Electric & Mfg Co Heat exchange apparatus
US2469785A (en) * 1944-01-29 1949-05-10 Interval Instr Inc Frequency controlled transducer

Cited By (27)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2761668A (en) * 1950-12-13 1956-09-04 Smidth & Co As F L Apparatus and method for exchanging heat between solid materials and a fluid medium
US2811337A (en) * 1951-07-20 1957-10-29 Garrett Corp Heat exchanger
US2715516A (en) * 1951-10-25 1955-08-16 Standard Oil Co Heat exchanger design
US2902830A (en) * 1955-07-02 1959-09-08 Lenz William Steam power plants
US2873098A (en) * 1955-10-03 1959-02-10 Yates American Machine Co Heat exchange apparatus
DE1258003B (en) * 1963-02-18 1968-01-04 California Research Corp Reactor for hydrocarbon conversions
DE1246776B (en) * 1963-05-15 1967-08-10 Christian Steeb Heat exchanger
US3201949A (en) * 1963-08-22 1965-08-24 Vilter Manufacturing Corp Refrigerating apparatus with oil separator means
US4190398A (en) * 1977-06-03 1980-02-26 General Electric Company Gas turbine engine and means for cooling same
US4197907A (en) * 1978-04-05 1980-04-15 Exxon Research & Engineering Co. Floating head support system for shell and tube heat exchanger
US4660631A (en) * 1980-04-28 1987-04-28 Phillips Petroleum Company Baffle
US4733722A (en) * 1981-11-20 1988-03-29 Serck Industries Limited Shell- and tube-type heat exchangers and their production
US4559996A (en) * 1983-06-03 1985-12-24 Societe Anonyme Dite-Delas-Weir Modular bundle of tubes for a steam condenser, and a steam condenser using such modular bundles
US5447195A (en) * 1993-06-11 1995-09-05 Atlas Copco Airpower, Naamloze Vennootschap Heat exchanger
WO2003016813A1 (en) * 2001-08-14 2003-02-27 H2Gen Innovations, Inc. Heat exchange reactor having integral housing assembly
US6896041B2 (en) * 2001-08-14 2005-05-24 H2Gen Innovations, Inc. Heat exchange reactor having integral housing assembly
US9279395B2 (en) * 2003-03-21 2016-03-08 Mahle International Gmbh Exhaust gas heat exchanger and sealing device for the same
US10358958B2 (en) 2003-03-21 2019-07-23 Mahle International Gmbh Exhaust gas heat exchanger and sealing device for the same
US20080202724A1 (en) * 2003-03-21 2008-08-28 Behr Gmbh & Co. Kg Exhaust Gas Heat Exchanger and Sealing Device for the Same
US20040226701A1 (en) * 2003-05-13 2004-11-18 H2Gen Innovations, Inc. Heat exchanger housing and seals
US6957695B2 (en) 2003-05-13 2005-10-25 H2Gen Innovations, Inc. Heat exchanger housing and seals
US8978740B2 (en) * 2006-06-22 2015-03-17 Modine Manufacturing Company Heat exchanger
US20110067837A1 (en) * 2006-06-22 2011-03-24 Harald Schatz Heat exchanger
US9933216B2 (en) 2006-06-22 2018-04-03 Modine Manufacturing Company Heat exchanger
US20110186276A1 (en) * 2010-01-29 2011-08-04 Casterton Joel T Heat exchanger assembly and method
US9403204B2 (en) 2010-01-29 2016-08-02 Modine Manufacturing Company Heat exchanger assembly and method
US10487723B2 (en) * 2015-06-10 2019-11-26 Wärtsilä Finland Oy Charge air cooler arrangement

Similar Documents

Publication Publication Date Title
US2595822A (en) Spring seal for tube and shell heat exchangers
US2488807A (en) Sealing end plates of heat exchangers
US2873098A (en) Heat exchange apparatus
US2752128A (en) Heat exchange structure
US3494414A (en) Heat exchanger having improved seal for the floating tube sheet
US3267562A (en) Rotor assembly
JPS6243115B2 (en)
US2811337A (en) Heat exchanger
US3785435A (en) Thermal damper for plate type heat exchangers
US3134432A (en) Heat exchanger
US3385353A (en) Mounting and support for the stacked sheets of a heat exchanger
US2360094A (en) Heat exchanger
US3863713A (en) Heat exchanger
US3240267A (en) Heat exchanger
US3572429A (en) Heat exchanger
US4058157A (en) Bearing support of the heat-exchanger disk of regenerative heat-exchanger
US4019750A (en) Bearing support of the heat-exchanger disk of a regenerative heat-exchanger
US4405012A (en) Device to position components of shell and tube heat exchanger
US3311164A (en) Heat exchanger with expansible tube seal
US3010704A (en) Circumferential seal
GB1315055A (en) Plate heat exchanger
US1524595A (en) Heat exchanger
US1947109A (en) Heat exchange apparatus
US2272863A (en) Heat exchange tube protector
US1558139A (en) Heat-exchange apparatus