[go: up one dir, main page]

US3294159A - Heat exchanger with spring biased support - Google Patents

Heat exchanger with spring biased support Download PDF

Info

Publication number
US3294159A
US3294159A US409860A US40986064A US3294159A US 3294159 A US3294159 A US 3294159A US 409860 A US409860 A US 409860A US 40986064 A US40986064 A US 40986064A US 3294159 A US3294159 A US 3294159A
Authority
US
United States
Prior art keywords
floating
shell
heat exchanger
tube
cover
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
US409860A
Inventor
Albert E Kovalik
Samuel H S Raub
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.)
Union Carbide Corp
Original Assignee
Union Carbide Corp
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 Union Carbide Corp filed Critical Union Carbide Corp
Priority to US409860A priority Critical patent/US3294159A/en
Application granted granted Critical
Publication of US3294159A publication Critical patent/US3294159A/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
    • F28F21/00Constructions of heat-exchange apparatus characterised by the selection of particular materials
    • F28F21/02Constructions of heat-exchange apparatus characterised by the selection of particular materials of carbon, e.g. graphite
    • 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
    • Y10S165/051Heat exchange having expansion and contraction relieving or absorbing means
    • Y10S165/052Heat exchange having expansion and contraction relieving or absorbing means for cylindrical heat exchanger
    • Y10S165/053Flexible or movable header or header element
    • Y10S165/054Movable header, e.g. floating header
    • Y10S165/055Movable header, e.g. floating header including guiding means for movable header
    • Y10S165/056Fluid sealing means between movable header and enclosure

Definitions

  • the present invention relates, in general to improvements in heat exchangers and, in particular, to heat exchangers of the shell and tube type, and more particularly to totally enclosed tube bundle heat exchangers of the character containing non-metallic tubes of carbon or graphite construction for conducting corrosive fluid media.
  • the particular improvement advanced by this invention is directed to a novel floating head arrangement.
  • the principal object of the invention is to provide a floating head arrangement including a tube sheet and closure therefor, wherein the gaskets between the end cover domes and the tube sheets on both ends of the enclosed tube bundle, and the gaskets between the fixed end plate and the inner dome are sealed by spring pressure on the floating end.
  • the use of springs in this application is unique in that they maintain the above-noted gaskets leak tight under all operating conditions of temperature and pressure.
  • the tube bundle comprising a plurality of tubes is conventionally stayed by balfles spaced on normal centers along the tube length.
  • FIGURE 1 is a side elevational view, partly in section showing the preferred form of the invention
  • FIGURE 2 is a greatly enlarged fragmentary view, largely in section showing the details of the spring loading means applied to the dome of the heat exchanger i1- lustrated in FIGURE 1;
  • FIGURE 3 is another side elevational view, partly in section showing another form of the invention.
  • FIG- URES 1 and 2 there is shown a singlepass heat exchanger of the shell and tube type generally indicated by the numeral 10.
  • An inlet end casting 12 and an outlet end casting 14 are conventionally welded to the longitudinal metallic shell 16.
  • the baflles 20 are secured to and generally spaced along the tie rods 21 which pass through the baflles 20.
  • a fixed tube sheet 22 of carbon or graphite enclosed within the shell 16 and supporting the tubes 18 is disposed adjacent to and connects with a single pass fixed outlet dome or cover 24 of carbon or graphite.
  • a floating tube sheet 28 of carbon or graphite which likewise supports the tubes 18 and is connected to a single pass floating inlet dome or cover 3,294,159 Patented Dec. 27, 1966 30 also of carbon or graphite.
  • the tubes 18 as is done in the art are conventionally cemented into open-ended sockets in the tube sheets 22 and 28.
  • An end plate 34 is clamped and gasketed to flange 32, which is suitably secured preferably by welding to the shell 16 adjacent the floating end 26 of the heat exchanger 10.
  • the improved feature of the heat exchanger 10 centers around the floating end members which permit the tube bundle (tube sheets, tube battles and tie rods) to be under continuous compressive loading and seals the gaskets 36 and 38 between the covers 30 and 24 andtube sheets 22 and 28, and the gasket 40 between the fixed cover 24 and end plate 42.
  • Gasket 41 provides the seal between the end plate 42 and the flange 43.
  • the tubes are in tension.
  • a plurality of compression springs 44 aligned about studs 46 are positioned about the periphery of the floating cover 30.
  • a cup-shaped member 47 maintains the springs 44 in place about the studs 46 should the end plate 34 be removed by loosening the nuts 48 from the bolts 50 which clamp together the end plate 34, gasket 52 and flange 32.
  • the springs 44 bear against the floating outlet cover 30 which is seated against the floating tube sheet 28.
  • the floating tube sheet 28 in turn bears toward the fixed tube sheet 22, thus loading the tubes 18 in compression.
  • the tubes 18 when loaded in compression hunt their way through the baflies 20 and brace against them and thus tube cutting caused by vibration of taut and lightly supported tubes is minimized and may even be eliminated entirely.- Since carbon and graphite is much stronger in compression than in tension, it is highly advantageous to utilize the invention for such shell and tube type heat exchangers employing a tube bundle assembly. Moreover, continuous spring loading follows the-gasket material under all conditions of cold flow, maintains pressure over full range of differential thermal expansion, and eliminates complete relaxation of bolt loading which occurs when the .bolt heads rust against their bearing surfaces or when the nuts vibrate loose. Further, the spring loading under these conditions control the gasket loading as opposed to the excessive and variable bolt loading necessary when standard bolts are used to seal the gaskets.
  • passage means such as clearance 54 between the shell wall 16 and the floating dome 30 and tube sheet 28 permits hydraulic pressure to be impressed against the dome 30 in the direction of the spring loading thereby increasing the effectiveness of the gasket sealing.
  • the operating pressures in the shell are generally equal to or greater than the pressure in the tubes which are of carbon or graphite. It should be realized that in such an armored construction all of the carbonaceous members of the heat exchanger are totally enclosed within the shell.
  • FIGURE 3 there is shown a variation of the structure for effecting the improvement hereinbefore described for such shell and tube type heat exchangers.
  • This struc ture accomplishes the objects of the invention in a four pass shell and tube heat exchanger.
  • the fixed end 56 of the heat exchanger 58 is open at the fixed tube sheet 60 so that any suitable dome or cover 62 can be readily secured by bolts to ring 64 which is in turn secured in a like manner to flange 63.
  • Cover 62 is provided with three chambers 66, 68, and which permit the t) fluid A to be routed through the tubes 18 four times (see reference arrows).
  • a plurality of compression springs 44 bear against a two compartment floating dome or cover- 74 via plate 73 which in turn bears against the floating tube sheet 76.
  • End plate 71 which provides a suitable end bearing wall for the springs 44, is secured to flange 75 which is generally welded to the shell wall 78.
  • clearance 77 between the shell wall 78 and the floating dome 74 and'the tube sheet 76 also permits hydraulic pressure to be impressed against the dome 74 in the direction of the spring loading thereby increasing the effectiveness of the gasket sealing.
  • the path of the second fluid B is also illustrated by reference arrows. I
  • the improved heat exchanger of the invention provides compressive spring loading of the tube bundle which control the gasket loading as opposed to the excessive and variable bolt loading necessary when standard bolts are used to seal the gaskets in heretofore totally enclosed tube bundle heat exchangers.
  • the advantages of the heat exchangers in summary are that such apparatus provides spring loading of the gaskets under all conditions of cold flow, maintains pressure over full range of differential thermal expansion and eliminates relaxation of bolt loading which occurs when the bolt heads rust against their bearing surfaces or when the nuts vibrate loose.
  • a heat exchanger comprising a shell, a tube bundle therein, a floating tube sheet for slidably supporting one end of said tube bundle within said shell, a flange on said shell at the floating tube sheet end thereof, a floating cover abutting said floating tube sheet, an end plate for the floating end of said heat exchanger, means for securing said end plate to said flange, resilient loading means disposed between said end plate and said floating cover and passage means for enabling the shell side fluid to impress against said floating cover in the direction of said resilient loading means whereby the tubes of said tube bundle are compressively loaded.
  • a heat exchanger comprising a shell, a tube bundle therein, a fixed tube sheet for supporting one end of said tube bundle within said shell, a fixed cover and a gasket between said fixed tube sheet and said fixed cover, a floating tube sheet for slidably supporting the opposite end of said tube bundle within said shell, a flange on said shell at the floating tube sheet end thereof, a floating cover and a second gasket between said floating tube sheet and said floating cover, an end plate for the floating end of said heat exchanger, means for securing said end plate to said flange, resilient loading means disposed between said end plate and said floating cover and passage means for enabling the shell side fluid to impress against said floating cover in the direction of said resilient loading means whereby said gaskets are compressively loaded.
  • a heat exchanger comprising a shell, a tube bundle therein, a fixed tube sheet for supporting one end of said tube bundle within said shell, a fixed cover and a gasket between said fixed tube sheet and said fixed cover, an end plate for the fixed end of said heat exchanger and a second gasket between said fixed cover and said end plate, a
  • a heat exchanger comprising a shell, a tube bundle therein, an impervious carbonaceous tube sheet fixed to one end of said shell for supporting one end of said tube bundle within said shell, an impervious carbonaceous fixed cover and a gasket between said fixed tube sheet and said fixed cover, an impervious carbonaceous floating tube sheet for slidably supporting the opposite end of said tube bundle within said shell, a flange on said shell at the floating tube sheet end thereof, an impervious carbonaceous floating cover and a second gasket between said floating tube sheet and said floating cover, an end plate for the floating end of said heat exchanger, means for securing said end plate to said flange, resilient loading means disposed between said end plate and said floating cover and passage means for enabling the shell side fluid to impress against said floating cover in the direction of said resilient loading means whereby said gaskets and the tubes of said tube bundle are compressively loaded.
  • a heat exchanger comprising a shell, an impervious carbonaceous tube sheet fixed to one end of said shell, an impervious carbonaceous floating tube sheet at the opposite end of said shell, a bundle of substantially parallel impervious carbonaceous tubes extending between said tube sheets and communicating with corresponding openended sockets in said tube sheets, a flange on said shell at the floating tube sheet end thereof, an impervious carbonaceous floating cover abutting said floating tube sheet, an end plate for the floating end of said seat exchanger, means for securing said end plate to said flange, resilient loading means disposed between said end plate and said floating cover and passage means for enabling the shell side fluid to impress against said floating cover in the direction of said resilient loading means whereby said tubes are compressively loaded between said tube sheets.

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

Dec. 27, 1966 A. E. KOVALIK ETAL 3,294,159
HEAT EXCHANGER WITH SPRING BIASED SUPPORT 2 Sheets-Sheet 1 Filed Nov. 9, 1964 K m 0 T R N EKS WEH I E mu mm AS A T TORNE'V Dec. 27, 1966 A. E. KOVALIK ETAL 3,
HEAT EXCHANGER WITH SPRING BIASED SUPPORT Filed Nov. 9, 1964 2 Sheets-Sheet 2 INVENTORS ALBERT E. KOVALIK SAMUEL H. S. RAUB United States Patent 3,294,159 HEAT EXCHANGER WITH SPRING BIASEDSUPPORT Albert E. Kovalik, Cleveland, and Samuel H. S. Raub,
Bay Village, Ohio, assiguors to Union Carbide Corporation, a corporation of New York Filed Nov.'9, 1964, Ser. No. 409,860 9 Claims. (Cl. 165-81) The present invention relates, in general to improvements in heat exchangers and, in particular, to heat exchangers of the shell and tube type, and more particularly to totally enclosed tube bundle heat exchangers of the character containing non-metallic tubes of carbon or graphite construction for conducting corrosive fluid media.
The particular improvement advanced by this invention is directed to a novel floating head arrangement.
The principal object of the invention is to provide a floating head arrangement including a tube sheet and closure therefor, wherein the gaskets between the end cover domes and the tube sheets on both ends of the enclosed tube bundle, and the gaskets between the fixed end plate and the inner dome are sealed by spring pressure on the floating end. The use of springs in this application is unique in that they maintain the above-noted gaskets leak tight under all operating conditions of temperature and pressure. The tube bundle comprising a plurality of tubes is conventionally stayed by balfles spaced on normal centers along the tube length.
Since the invention is primarily concerned with a floating head structure arrangement to be used with the more or less conventional forms of totally enclosed tube bundle heat exchangers, the other portions of'such exchanger including the shell and the fixed end of the tube bundle although shown in the accompanying drawings will not be described in great detail since such heat exchangers are well known and understood by those skilled in the art.
The main object and other objects and advantages of the invention will be readily understood from the following detailed description when read in conjunction with the accompanying drawing, which illustrates the preferred forms of the device, and in which like characters of reference designate like parts throughout the several views, and in which:
FIGURE 1 is a side elevational view, partly in section showing the preferred form of the invention;
FIGURE 2 is a greatly enlarged fragmentary view, largely in section showing the details of the spring loading means applied to the dome of the heat exchanger i1- lustrated in FIGURE 1; and
FIGURE 3 is another side elevational view, partly in section showing another form of the invention.
Referring to the drawings, and particularly to FIG- URES 1 and 2, there is shown a singlepass heat exchanger of the shell and tube type generally indicated by the numeral 10. An inlet end casting 12 and an outlet end casting 14 are conventionally welded to the longitudinal metallic shell 16. Inside the shell 16 is mounted a bundle of uniformly disposed impervious carbon or graphite tubes 18, which pass through correspondingly spaced holes (not shown) in baflles 20. The baflles 20 are secured to and generally spaced along the tie rods 21 which pass through the baflles 20. A fixed tube sheet 22 of carbon or graphite enclosed within the shell 16 and supporting the tubes 18 is disposed adjacent to and connects with a single pass fixed outlet dome or cover 24 of carbon or graphite. At the floating end 26 of the heat exchanger is a floating tube sheet 28 of carbon or graphite which likewise supports the tubes 18 and is connected to a single pass floating inlet dome or cover 3,294,159 Patented Dec. 27, 1966 30 also of carbon or graphite. The tubes 18 as is done in the art are conventionally cemented into open-ended sockets in the tube sheets 22 and 28.
An end plate 34 is clamped and gasketed to flange 32, which is suitably secured preferably by welding to the shell 16 adjacent the floating end 26 of the heat exchanger 10. Y
The improved feature of the heat exchanger 10 centers around the floating end members which permit the tube bundle (tube sheets, tube battles and tie rods) to be under continuous compressive loading and seals the gaskets 36 and 38 between the covers 30 and 24 andtube sheets 22 and 28, and the gasket 40 between the fixed cover 24 and end plate 42. Gasket 41 provides the seal between the end plate 42 and the flange 43. In contrast to the above-described construction, it should be noted that in conventional heat exchanger designs the tubes are in tension.
A plurality of compression springs 44 aligned about studs 46 are positioned about the periphery of the floating cover 30. A cup-shaped member 47 maintains the springs 44 in place about the studs 46 should the end plate 34 be removed by loosening the nuts 48 from the bolts 50 which clamp together the end plate 34, gasket 52 and flange 32. The springs 44 bear against the floating outlet cover 30 which is seated against the floating tube sheet 28. The floating tube sheet 28 in turn bears toward the fixed tube sheet 22, thus loading the tubes 18 in compression. The tubes 18 when loaded in compression hunt their way through the baflies 20 and brace against them and thus tube cutting caused by vibration of taut and lightly supported tubes is minimized and may even be eliminated entirely.- Since carbon and graphite is much stronger in compression than in tension, it is highly advantageous to utilize the invention for such shell and tube type heat exchangers employing a tube bundle assembly. Moreover, continuous spring loading follows the-gasket material under all conditions of cold flow, maintains pressure over full range of differential thermal expansion, and eliminates complete relaxation of bolt loading which occurs when the .bolt heads rust against their bearing surfaces or when the nuts vibrate loose. Further, the spring loading under these conditions control the gasket loading as opposed to the excessive and variable bolt loading necessary when standard bolts are used to seal the gaskets. In addition, passage means such as clearance 54 between the shell wall 16 and the floating dome 30 and tube sheet 28 permits hydraulic pressure to be impressed against the dome 30 in the direction of the spring loading thereby increasing the effectiveness of the gasket sealing. For reasons of safety, the operating pressures in the shell are generally equal to or greater than the pressure in the tubes which are of carbon or graphite. It should be realized that in such an armored construction all of the carbonaceous members of the heat exchanger are totally enclosed within the shell.
It should also be noted at this time that the longitudinal force on the tubes can always be maintained in compression by proper proportioning of the area of the inner side of the tube sheet-to the area of the outer end surface of the dome which is under hydraulic shell pressure.
In FIGURE 3, there is shown a variation of the structure for effecting the improvement hereinbefore described for such shell and tube type heat exchangers. This struc ture accomplishes the objects of the invention in a four pass shell and tube heat exchanger. In this embodiment, the fixed end 56 of the heat exchanger 58 is open at the fixed tube sheet 60 so that any suitable dome or cover 62 can be readily secured by bolts to ring 64 which is in turn secured in a like manner to flange 63. Cover 62 is provided with three chambers 66, 68, and which permit the t) fluid A to be routed through the tubes 18 four times (see reference arrows). At the floating end 72 of the heat exchanger 58 a plurality of compression springs 44 bear against a two compartment floating dome or cover- 74 via plate 73 which in turn bears against the floating tube sheet 76. End plate 71, which provides a suitable end bearing wall for the springs 44, is secured to flange 75 which is generally welded to the shell wall 78.
In this modification, clearance 77 between the shell wall 78 and the floating dome 74 and'the tube sheet 76 also permits hydraulic pressure to be impressed against the dome 74 in the direction of the spring loading thereby increasing the effectiveness of the gasket sealing. As shown in FIGS. 1 and 3, the path of the second fluid B is also illustrated by reference arrows. I
In essence then, the improved heat exchanger of the invention provides compressive spring loading of the tube bundle which control the gasket loading as opposed to the excessive and variable bolt loading necessary when standard bolts are used to seal the gaskets in heretofore totally enclosed tube bundle heat exchangers. The advantages of the heat exchangers in summary are that such apparatus provides spring loading of the gaskets under all conditions of cold flow, maintains pressure over full range of differential thermal expansion and eliminates relaxation of bolt loading which occurs when the bolt heads rust against their bearing surfaces or when the nuts vibrate loose.
What is claimed is:
' 1. A heat exchanger, comprising a shell, a tube bundle therein, a floating tube sheet for slidably supporting one end of said tube bundle within said shell, a flange on said shell at the floating tube sheet end thereof, a floating cover abutting said floating tube sheet, an end plate for the floating end of said heat exchanger, means for securing said end plate to said flange, resilient loading means disposed between said end plate and said floating cover and passage means for enabling the shell side fluid to impress against said floating cover in the direction of said resilient loading means whereby the tubes of said tube bundle are compressively loaded.
2. The heat exchanger of claim 1 wherein said resilient means disposed between said end plate and said floating cover comprise a plurality of compression springs.
23. The heat exchanger of claim 2 wherein said compression springs are positioned about a plurality of studs which maintain said compression springs in place against said end plate.
4. A heat exchanger, comprising a shell, a tube bundle therein, a fixed tube sheet for supporting one end of said tube bundle within said shell, a fixed cover and a gasket between said fixed tube sheet and said fixed cover, a floating tube sheet for slidably supporting the opposite end of said tube bundle within said shell, a flange on said shell at the floating tube sheet end thereof, a floating cover and a second gasket between said floating tube sheet and said floating cover, an end plate for the floating end of said heat exchanger, means for securing said end plate to said flange, resilient loading means disposed between said end plate and said floating cover and passage means for enabling the shell side fluid to impress against said floating cover in the direction of said resilient loading means whereby said gaskets are compressively loaded.
5. A heat exchanger, comprising a shell, a tube bundle therein, a fixed tube sheet for supporting one end of said tube bundle within said shell, a fixed cover and a gasket between said fixed tube sheet and said fixed cover, an end plate for the fixed end of said heat exchanger and a second gasket between said fixed cover and said end plate, a
4 floating tube sheet for slidably supporting the opposite end of said tube bundle within said shell, a flange on said shell at the floating tube sheet end thereof, a floating cover and a third gasket between said floating tube sheet and said floating cover, a second end plate for the floating end of said heat exchanger, means for securing said end plate to said flange, resilient loading means disposed between said second end plate and said floating cover and passage means for enabling the shell side fluid to impress against said floating cover in the direction of said resilient loading means whereby all of said gaskets are compressively loaded.
6. A heat exchanger, comprising a shell, a tube bundle therein, an impervious carbonaceous tube sheet fixed to one end of said shell for supporting one end of said tube bundle within said shell, an impervious carbonaceous fixed cover and a gasket between said fixed tube sheet and said fixed cover, an impervious carbonaceous floating tube sheet for slidably supporting the opposite end of said tube bundle within said shell, a flange on said shell at the floating tube sheet end thereof, an impervious carbonaceous floating cover and a second gasket between said floating tube sheet and said floating cover, an end plate for the floating end of said heat exchanger, means for securing said end plate to said flange, resilient loading means disposed between said end plate and said floating cover and passage means for enabling the shell side fluid to impress against said floating cover in the direction of said resilient loading means whereby said gaskets and the tubes of said tube bundle are compressively loaded.
7. A heat exchanger comprising a shell, an impervious carbonaceous tube sheet fixed to one end of said shell, an impervious carbonaceous floating tube sheet at the opposite end of said shell, a bundle of substantially parallel impervious carbonaceous tubes extending between said tube sheets and communicating with corresponding openended sockets in said tube sheets, a flange on said shell at the floating tube sheet end thereof, an impervious carbonaceous floating cover abutting said floating tube sheet, an end plate for the floating end of said seat exchanger, means for securing said end plate to said flange, resilient loading means disposed between said end plate and said floating cover and passage means for enabling the shell side fluid to impress against said floating cover in the direction of said resilient loading means whereby said tubes are compressively loaded between said tube sheets.
8. The heat exchanger of claim 7 wherein said resilient means disposed between said end plate and said floating cover comprise a plurality of compression springs.
9. The heat exchanger of claim 8 wherein said compression springs are positioned about a plurality of studs which maintain said compression springs in place against said end plate.
References Cited by the Examiner UNITED STATES PATENTS 464,159 12/1891 Link -82 826,966 7/1906 Schneible 165--82 1,591,174 7/1926 Mailey 165-81X 2,887,303 5/1959 Reys 16582 2,965,787 10/1960 Raub 16s 82 FOREIGN PATENTS 1,211,918 10/1959 France.
908,028 4/1954 Germany.
ROBERT A. OLEARY, Primary Examiner.
A. DAVIS, Assistant Examiner.

Claims (1)

1. A HEAT EXCHANGER, COMPRISING A SHELL, A TUBE BUNDLE THEREIN, A FLOATING TUBE SHEET FOR SLIDABLY SUPPORTING ONE END OF SAID TUBE BUNDLE WITHIN SAID SHELL, A FLANGE ON SAID SHELL AT THE FLOATING TUBE SHEET END THEREOF, A FLOATING COVER ABUTTING SAID FLOATING TUBE SHEET, AN END PLATE FOR THE FLOATING END OF SAID HEAT EXCHANGER, MEANS FOR SECURING SAID END PLATE TO SAID FLANGE, RESILIENT LOADING MEANS DISPOSED BETWEEN SAID END PLATE AND SAID FLOATING COVER AND PASSAGE MEANS FOR ENABLING THE SHELL SIDE FLUID TO IMPRESS AGAINST SAID FLOATING COVER IN THE DIRECTION OF SAID RESILIENT LOADING MEANS WHEREBY THE TUBES OF SAID TUBE BUNDLE ARE COMPRESSIVELY LOADED.
US409860A 1964-11-09 1964-11-09 Heat exchanger with spring biased support Expired - Lifetime US3294159A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US409860A US3294159A (en) 1964-11-09 1964-11-09 Heat exchanger with spring biased support

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US409860A US3294159A (en) 1964-11-09 1964-11-09 Heat exchanger with spring biased support

Publications (1)

Publication Number Publication Date
US3294159A true US3294159A (en) 1966-12-27

Family

ID=23622278

Family Applications (1)

Application Number Title Priority Date Filing Date
US409860A Expired - Lifetime US3294159A (en) 1964-11-09 1964-11-09 Heat exchanger with spring biased support

Country Status (1)

Country Link
US (1) US3294159A (en)

Cited By (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3669185A (en) * 1970-08-10 1972-06-13 Howard J Bare Modular heat exchanger construction
US3889744A (en) * 1972-04-20 1975-06-17 Owens Illinois Inc Recuperator structures and method of making same
US4119141A (en) * 1977-05-12 1978-10-10 Thut Bruno H Heat exchanger
FR2436955A1 (en) * 1978-09-19 1980-04-18 Nuclear Power Co Ltd HEAT EXCHANGER, PARTICULARLY FOR LIQUID COOLING METAL
US4215744A (en) * 1978-06-30 1980-08-05 Solartrap, Inc. Heat exchanger
US4244423A (en) * 1978-07-17 1981-01-13 Thut Bruno H Heat exchanger
US4328860A (en) * 1977-12-30 1982-05-11 Motoren- Und Turbinen-Union Munchen, Gmbh Recuperator for heat exchange between flow media of dissimilar temperatures
US4852644A (en) * 1986-11-29 1989-08-01 Man Gutehoffnungshuette Gmbh Tubular heat exchanger
US20040182546A1 (en) * 2002-02-05 2004-09-23 Hiroyuki Yoshida Heat exchanger with heat deformation absorbing mechanism
US20080229763A1 (en) * 2007-03-19 2008-09-25 Colmac Coil Manufacturing, Inc. Heat exchanger and method for defrosting a heat exchanger
WO2012106605A3 (en) * 2011-02-04 2013-03-21 Lockheed Martin Corporation Staged graphite foam heat exchangers
US9464847B2 (en) 2011-02-04 2016-10-11 Lockheed Martin Corporation Shell-and-tube heat exchangers with foam heat transfer units
US9513059B2 (en) 2011-02-04 2016-12-06 Lockheed Martin Corporation Radial-flow heat exchanger with foam heat exchange fins

Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US464159A (en) * 1891-12-01 Steam-heating radiator
US826966A (en) * 1905-05-04 1906-07-24 Joseph Schneible Cooler or condenser.
US1591174A (en) * 1923-12-07 1926-07-06 Cooper Hewitt Electric Co Jointure means
DE908028C (en) * 1948-11-03 1954-04-01 Hoechst Ag Process and column for material turnover and heat exchanger
US2887303A (en) * 1956-05-04 1959-05-19 Falls Ind Inc Heat exchanger
FR1211918A (en) * 1957-12-23 1960-03-18 Foster Wheeler Ltd advanced heat exchangers
US2965787A (en) * 1959-07-14 1960-12-20 Bomac Lab Inc Gaseous discharge device

Patent Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US464159A (en) * 1891-12-01 Steam-heating radiator
US826966A (en) * 1905-05-04 1906-07-24 Joseph Schneible Cooler or condenser.
US1591174A (en) * 1923-12-07 1926-07-06 Cooper Hewitt Electric Co Jointure means
DE908028C (en) * 1948-11-03 1954-04-01 Hoechst Ag Process and column for material turnover and heat exchanger
US2887303A (en) * 1956-05-04 1959-05-19 Falls Ind Inc Heat exchanger
FR1211918A (en) * 1957-12-23 1960-03-18 Foster Wheeler Ltd advanced heat exchangers
US2965787A (en) * 1959-07-14 1960-12-20 Bomac Lab Inc Gaseous discharge device

Cited By (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3669185A (en) * 1970-08-10 1972-06-13 Howard J Bare Modular heat exchanger construction
US3889744A (en) * 1972-04-20 1975-06-17 Owens Illinois Inc Recuperator structures and method of making same
US4119141A (en) * 1977-05-12 1978-10-10 Thut Bruno H Heat exchanger
US4328860A (en) * 1977-12-30 1982-05-11 Motoren- Und Turbinen-Union Munchen, Gmbh Recuperator for heat exchange between flow media of dissimilar temperatures
US4215744A (en) * 1978-06-30 1980-08-05 Solartrap, Inc. Heat exchanger
US4244423A (en) * 1978-07-17 1981-01-13 Thut Bruno H Heat exchanger
FR2436955A1 (en) * 1978-09-19 1980-04-18 Nuclear Power Co Ltd HEAT EXCHANGER, PARTICULARLY FOR LIQUID COOLING METAL
US4852644A (en) * 1986-11-29 1989-08-01 Man Gutehoffnungshuette Gmbh Tubular heat exchanger
US20040182546A1 (en) * 2002-02-05 2004-09-23 Hiroyuki Yoshida Heat exchanger with heat deformation absorbing mechanism
US7082988B2 (en) * 2002-02-05 2006-08-01 Nissan Motor Co., Ltd. Heat exchanger with heat deformation absorbing mechanism
US20080229763A1 (en) * 2007-03-19 2008-09-25 Colmac Coil Manufacturing, Inc. Heat exchanger and method for defrosting a heat exchanger
US7712327B2 (en) * 2007-03-19 2010-05-11 Colmac Coil Manufacturing, Inc. Heat exchanger and method for defrosting a heat exchanger
WO2012106605A3 (en) * 2011-02-04 2013-03-21 Lockheed Martin Corporation Staged graphite foam heat exchangers
US9464847B2 (en) 2011-02-04 2016-10-11 Lockheed Martin Corporation Shell-and-tube heat exchangers with foam heat transfer units
US9513059B2 (en) 2011-02-04 2016-12-06 Lockheed Martin Corporation Radial-flow heat exchanger with foam heat exchange fins
US9951997B2 (en) 2011-02-04 2018-04-24 Lockheed Martin Corporation Staged graphite foam heat exchangers

Similar Documents

Publication Publication Date Title
US3294159A (en) Heat exchanger with spring biased support
US3326279A (en) Heat exchanger
US2411097A (en) Heat exchanger
US6206086B1 (en) Multi-pass tube side heat exchanger with removable bundle
US2997435A (en) Pressure vessels
US3327777A (en) Heat interchanger
US4738310A (en) Heat exchanger
US3443548A (en) High temperature and high pressure steam generator
US2537276A (en) Heat exchanger
US5538261A (en) Mechanical heat-exchange tube sealing system
US3052452A (en) Leakage preventing welding connection
US3746083A (en) Heat-exchanger
GB2095389A (en) Shell and tube exchanger
US2766903A (en) Head closure construction for heat exchangers
US3721291A (en) End closure for a heat exchanger
US4623017A (en) Joint structure for a tube and a header
US4532771A (en) Cooler made of aluminum for stirling engines
GB1593675A (en) Tube and shell heat exchangers and composite tube plates therefor
US4331352A (en) Heat exchanger support system providing for thermal isolation and growth
US4458866A (en) Heat exchanger support system providing for thermal isolation and growth
NO160391B (en) EXPANSION DEVICE IN PRINTED LIQUID ACCUMULATOR.
US4109710A (en) Heat exchanger
GB2093537A (en) Seals
US4128126A (en) Apparatus for support of sheet-metal-type heat exchanger matrices for recuperative heat exchange
GB2132330A (en) Spiral heat exchanger