US3279532A - Heat exchanger tube-joint sealing arrangement - Google Patents
Heat exchanger tube-joint sealing arrangement Download PDFInfo
- Publication number
- US3279532A US3279532A US370906A US37090664A US3279532A US 3279532 A US3279532 A US 3279532A US 370906 A US370906 A US 370906A US 37090664 A US37090664 A US 37090664A US 3279532 A US3279532 A US 3279532A
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- US
- United States
- Prior art keywords
- tube
- ring
- counterbore
- tubes
- heat exchanger
- 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
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Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F28—HEAT EXCHANGE IN GENERAL
- F28F—DETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
- F28F9/00—Casings; Header boxes; Auxiliary supports for elements; Auxiliary members within casings
- F28F9/02—Header boxes; End plates
- F28F9/04—Arrangements for sealing elements into header boxes or end plates
- F28F9/06—Arrangements for sealing elements into header boxes or end plates by dismountable joints
- F28F9/14—Arrangements for sealing elements into header boxes or end plates by dismountable joints by force-joining
-
- Y—GENERAL 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
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10S165/00—Heat exchange
- Y10S165/051—Heat exchange having expansion and contraction relieving or absorbing means
- Y10S165/052—Heat exchange having expansion and contraction relieving or absorbing means for cylindrical heat exchanger
- Y10S165/067—Cylindrical heat exchanger rectilinearly slidable relative to its support
- Y10S165/068—Cylindrical heat exchanger rectilinearly slidable relative to its support including fluid seal
Definitions
- the tube plate is provided with a plurality of openings extending therethrough and into each of t-he openings, a tube is extended and attached to the tube plate in such a manner as to provide a leak-proof assembly permitting Huid at one temperature to ow through the tubes to provide heat exchange with a uid at another temperature flowing about the tubes, as well understood in this art.
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- 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
Oct. 18, 1966 A, H, PFElL, JR 3,279,532
TUB JOIN Filed May 28, 1964 WITNEssE INVENTOR MM Adolph H. Pfeil ,Jr
Wl@ y.
United States Patent O 3,279,532 HEAT EXCHANGER TUBE-JOINT SEALING ARRANGEMENT Adolph H. Pfeil, Jr., Springfield, Pa., assigner to Westinghouse Electric Corporation, Pittsburgh, Pa., a corporation of Pennsylvania Filed May 28, 1964, Ser. No. 370,906 1 Claim. (Cl. 165-81) This invention relates to heat exchangers, such as vapor condensers and the like, more particularly to arrangements for maintaining tubes in duid-tight relation with a tube plate of a surface heat exchanger, and has for an object to provide a simple, inexpensive, yet highly effective and reliable tube-joint assembly of this type.
Briey, in accordance with the invention, there is provided an improved arrangement for maintaining the tubes in duid-tight rel-ation with a tube plate of a heat exchange-r of the surface type, While permitting relative movement therebetween to occur parallel t-o the tube axes, due to relative thermal elongation and/or contraction of the tubes and the heat exchanger shell structure.
The tube plate is provided with a plurality of openings extending therethrough and into each of t-he openings, a tube is extended and attached to the tube plate in such a manner as to provide a leak-proof assembly permitting Huid at one temperature to ow through the tubes to provide heat exchange with a uid at another temperature flowing about the tubes, as well understood in this art.
Considering one of the tube-joints, one of the openings in the tube plate is provided with a cylindrical walled counterbore and the tube associated therewith extends freely through the opening is loosely received therein so that, jointly with the wall of the counterbore, an annular space is defined therebetween. A sealing ring member of resilient material, for example an O-ring of synthetic rubber, is compressed in the space in encompassing sealing abutment with the tube and in encompassed abutment with the wall of the counterbore to complete the seal.
Since the tubes are relatively long with relation to their cross sectional area, and since the heat exchanger shell must be of even greater length to accommodate the tubes, during operation either the tubes and/ or the shell undergo a certain degree of thermal expansion or contraction. Accordingly, the axial length of the counterbore wall is at least of suicient length to accommodate the relative movement between the tube and the tube plate dur-ing operation. In normal operation, the tube slides relative to the seal ring so that the axial length of the counterbore is not vital to reliability of the seal. However, in the event that for any reason the seal ring should adhere to the tube instead of the wall of the counterbore, disengagement of the ring from the counterbore is prevented.
The above and other objects are effected by the invention Ias will be apparent from the foregoing description and claim taken in connection with the accompanying drawings, forming a part of this application, in which:
FIGURE 1 is a longitudinal sectional view of a typical vapor condenser having t-he invention incorporated there- 1n;
FIG. 2 is .a greatly enlarged sectional view taken along line II'II of FIG. 1; and
FIG. 3 is a sectional View taken along line III- III of FIG. 2.
Referring to the drawing in detail, in FIG. 1 there is shown a vapor condenser 10 of the well-known surface type including a tubular shell structure 11, a pair of tube plates 12 and 13 disposed in closing relation at opposite ends of the shell structure 11, waterboxes 14 and 15 disposed in abutment with the tube plates 12 and 13, respectively, and a plurality of tubes 16 supported in the tube plates 12 and 13 and communicating with the Waterboxes 14 and 15. The waterbox 15 is of the divided type provided wit-h a duid inlet 17 and a uid outlet 18 and the shell structure 11 is provided with a vapor inlet 19 and a condensate outlet 20.
In operation, as well known in this art, vapor to be condensed is directed into the shell structure 11 through the inlet 19, and, during its flow through the shell structure 11, ows around the tubes 16. At the same time coolant lluid, such as water, is admitted through the inlet 17 of the water box 1-5 and thence transverse the tubes 16 in the lower portion to the water box 14, wherein its direction of ilow is reversed and it tlows in opposite direction through the tubes 16 in the upper portion to the water box 15 and thence through the outlet 18. Since the iluid flowing through the tube 16 is at a lower temperature than t-he vapor flowing thereabout, the vapor is condensed and falls to the bottom of the shell structure 11 and is then withdrawn through the outlet 20.
From the above it will be seen that to prevent contamination of the vapor being condensed in the shell 11 by the uid owing in the tubes 16 and the w-ater boxes 14 and 1-5, it is important to provide a leakproof joint between the tubes 16 and the plates 12 and 13. Heretof-ore, the tube joints have been attained by various expedients, all with varying degrees of success. For example, it is known to weld, solder or swage the tubes in the tube plates 12 and 13, thereby forming a rigid structure. In addition thereto, metal packing has even been proposed to provide a fluid-tight joint between the tubes and the tube plates. All of the above schemes are relatively expensive and time consuming in manufacture and, invariably, some of such joints will eventually break down in service and incur incipient leakage of fluid requiring repair. Such repair in service is even more laborious and costly than during initial manufacture.
In accordance with the invention, the tube plates 12 and 13 are provided with a plurality of openings 21 and 22, respectively, and the terminal ends of the tubes 16 are received therein and attached thereto in a manner now to be described in detail. However, only one of the joints, generally indicated 24, will be described.
Referring now to FIGS. 2 and 3, the tube-joint assembly 24 is provided by forming a cylindrical smooth walled counterbore 25 in an opening 22 and extending into the surface 26 of the tube plate 13. Hence, a ring-shaped shoulder 27 is provided in the tube plate 13 intermedi-ate the surface 26 and the opposite surface 28 of the tube plate 13. The surface 26 is exposed to the iiuid pressure of the coolant tluid in the waterbox 15, while the surface 28 is exposed to the tluid pressure of the vapor within the shell structure 11. The tube 16 is of slightly smaller diameter than the diameter of the opening 22 and of considerably smaller diameter than the diameter of the counterbore 25. Accordingly, as thus far described, the tube 16 freely extends through the tube plate 13 with its terminal portion 29 extending to a small degree beyond the face 26 of the tube plate 13.
The tube 16 and the counterbore 25 jointly define an annular space 30 and within this space there is disposed a sealing ring member 31 formed of any suitable resilient material. For example, the sealing ring 31 may be of the type known as an O-ring formed of any suitable resilient material such as natural rubber or `synthetic rubbers including silicones. The preferred cross sectional shape of the ring 31 is circular, in the relaxed state before assembly, hence the ring member 31 may be termed a torus.
In considering the O-ring 31 in its relaxed state before assembly, with relation to the external diameter of the 3` tube 16 and the internal diameter of the counterbore 25, the internal diameter of the O-ring 31 is slightly smaller (about 2%) than the external diameter of the tube 16 so that to assemble the ring 31 on the tube 16 it must be stretched to a slight degree to encompass the tube 16. Further, the radial thickness of the O-ring is slightly larger (about 20%) than the radial width of the space 30 l so that the O-ring must also be compressed to permit insertion into the counterbore 25.; Hence,.by referring to FIG. 2, it will be seen that when the O-ring is in place it isdistorted from the true circular cross sectional aspect to that of an ellipse with opposed attened surfaces 32 and 33. Further, the O-ring is in a state of radial compression but axial equilibrium and is substantially free to expand in a direction parallel to its central axis.
During operation, the tube 16 and the shell 11 become heated to different operating temperatures and since the tubes and shell are of considerable length, relative movement between the two occurs due to varying thermal elongation. With the arrangement shown, the tube 16 is slidable relative to the O-ring and the O-ring is maintained substantially in tixed abutment with the annular shoulder 27 in the tube plate 13. However, to assure the utmost reliability ofthe Huid-tight joint in operation, the preferred axial length of the counterbore 25 is at least as long as the expected diierence in thermal elongation between the shell 11 and the tube 16 in operation. O-ring 31 for any reason-adhere to the tube 16 and slide therewith as a unit relative to the counterbore 25, disengagement of the O-ring from the counterbore is prevented.
To further insure against disengagement of the O-ring 31 from the counterbore 25 during operation, the inlet end portion 29 of the `tube 16 is preferably ared outwardly toa small degree yas indicated at 34 and `the .diametrical extent of the flared portion is slightly less than the diametrical extent of the counterbore 25, so that the tube is free to move to the left as viewed in FIG. 2 without interference between the flared portion 34 and the tube plate 13.
The opening 22 is of slightly larger diametrical extent than the external diameter of the tube 16 so that jointly therewith an yannular space 35 is formed. However, the pressure of the condensing vapor in the shell structure 11 is insufficient to dislodge or move the O-ring 31 towards the right as viewed in FIG. 2, since the cross sectional area of the annular space 30 is considerably, larger than the area of the cross sectional area of the space 35, and the pressure of the uid in the waterbox is more than sufcient to maintain the seal ring 31 in abutment with the shoulder 27.'
Hence, should the It will now be seen that the invention provides a simple yet hightly eifective and inexpensive fluid-tight joint for joining a tube to the plate of a condenser or similar heat exchange apparatus, while permitting relative movement between the rtubes and the tube plates due to unequal thermal expansion and/or contractionof-the tubes and the shell structure.
Although only Vone embodiment of the invention has been shown, it will be obvious to those skilled in the art that it is not so limited, but is susceptible of various other changes and modifications without departing from the spirit thereof. Y
I claim as my invention:
A uid-tight tube-joint assembly for a heat exchanger comprising:
a tube plate having `a plurality of circular openings extending therethrough, at least one of said openings being partly defined by a cylindrical walled counterbore and a cylindrical Wall portion of reduced crosssectional area,
an elongated tube extending freely through said one opening,
said tube having a terminal portion subject, to axial movement when the tube undergoesthermal elongzv tion in operation,
said terminal portion and said counterbore jointly delining an annular space, and
a resilient rubb'er sealing ring member disposed in said space and in a state of radial compression but axial equilibrium,
said tube being of substantially constant diameter but the terminal portion being flared,
said counterbore being at least as long in axial extent as the thermal elongation of said tube, and
said sealing ring being restrained against movement in one axial direction by said reduced wall portion and in the opposite axial direction by said llarediportion.
References Cited by the Examiner UNITED` STATES PATENTS 911,156 2/1909 Poli-rz 16s- 173x 2,488,807 11/1949 Currie 16s-82X FOREIGN PATENTS 418,770 12/1910 France.
897,785 11/ 1953 Germany.
ROBERT A. OLEARY, Primary Examiner,
A. W. DAVIS,-A.ssstant Examiner.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US370906A US3279532A (en) | 1964-05-28 | 1964-05-28 | Heat exchanger tube-joint sealing arrangement |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US370906A US3279532A (en) | 1964-05-28 | 1964-05-28 | Heat exchanger tube-joint sealing arrangement |
Publications (1)
Publication Number | Publication Date |
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US3279532A true US3279532A (en) | 1966-10-18 |
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Family Applications (1)
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US370906A Expired - Lifetime US3279532A (en) | 1964-05-28 | 1964-05-28 | Heat exchanger tube-joint sealing arrangement |
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Cited By (17)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3380516A (en) * | 1966-06-17 | 1968-04-30 | Raypak Company Inc | Heat exchanger including tube expansion means |
US3517734A (en) * | 1967-03-16 | 1970-06-30 | Kvarner Brugs Kjoleavdeling As | Heat exchangers |
US3922768A (en) * | 1973-06-26 | 1975-12-02 | Kiyotelu Takayasu | Method of manufacturing a heat exchanger |
US4171832A (en) * | 1976-11-16 | 1979-10-23 | International Harvester Company | Relaxing joints |
US4257788A (en) * | 1979-04-16 | 1981-03-24 | Nicholas Nassir | Power recovery hot gas separator |
US4564504A (en) * | 1983-11-29 | 1986-01-14 | Sorco Corporation | Apparatus for producing an acid compound |
DE3502116A1 (en) * | 1985-01-23 | 1986-07-24 | Halberg Maschinenbau GmbH, 6700 Ludwigshafen | Shell-and-tube heat exchanger with expansion compensation for heat exchange of gases |
US4730669A (en) * | 1986-02-03 | 1988-03-15 | Long Manufacturing Ltd. | Heat exchanger core construction utilizing a diamond-shaped tube-to-header joint configuration |
US4759405A (en) * | 1987-03-18 | 1988-07-26 | Metzger Frederick W | Air conditioner condenser manifold |
US4905766A (en) * | 1987-04-28 | 1990-03-06 | R&G Sloane Mfg. Co., Inc. | Adapter for plastic pipe |
US5064223A (en) * | 1989-10-06 | 1991-11-12 | Ford Motor Company | Throttle modulator assemblies and thermoplastic fluid direction tubes for insertion therein |
US5538261A (en) * | 1994-08-02 | 1996-07-23 | Columbian Chemicals Company | Mechanical heat-exchange tube sealing system |
US20160273838A1 (en) * | 2015-03-18 | 2016-09-22 | Mahle International Gmbh | Exhaust gas heat transfer device |
WO2018044813A1 (en) * | 2016-08-31 | 2018-03-08 | Nlight, Inc. | Laser cooling system |
US10447004B2 (en) | 2015-11-19 | 2019-10-15 | Nlight, Inc. | Laser fault tolerance and self-calibration system |
US10574020B2 (en) | 2016-12-15 | 2020-02-25 | Nlight, Inc. | Fiber laser packaging |
US10784645B2 (en) | 2018-03-12 | 2020-09-22 | Nlight, Inc. | Fiber laser having variably wound optical fiber |
Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US911156A (en) * | 1907-06-29 | 1909-02-02 | Gustav Politz | Tube-joint. |
FR418770A (en) * | 1909-09-06 | 1910-12-19 | Joseph Weishaeupl | Gasket for condenser tubes by surface |
US2488807A (en) * | 1946-10-26 | 1949-11-22 | Donald H Currie | Sealing end plates of heat exchangers |
DE897785C (en) * | 1939-01-27 | 1953-11-23 | Cie De Pont A Mousson | Socket connection of pipes or other pipe elements |
-
1964
- 1964-05-28 US US370906A patent/US3279532A/en not_active Expired - Lifetime
Patent Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US911156A (en) * | 1907-06-29 | 1909-02-02 | Gustav Politz | Tube-joint. |
FR418770A (en) * | 1909-09-06 | 1910-12-19 | Joseph Weishaeupl | Gasket for condenser tubes by surface |
DE897785C (en) * | 1939-01-27 | 1953-11-23 | Cie De Pont A Mousson | Socket connection of pipes or other pipe elements |
US2488807A (en) * | 1946-10-26 | 1949-11-22 | Donald H Currie | Sealing end plates of heat exchangers |
Cited By (21)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3380516A (en) * | 1966-06-17 | 1968-04-30 | Raypak Company Inc | Heat exchanger including tube expansion means |
US3517734A (en) * | 1967-03-16 | 1970-06-30 | Kvarner Brugs Kjoleavdeling As | Heat exchangers |
US3922768A (en) * | 1973-06-26 | 1975-12-02 | Kiyotelu Takayasu | Method of manufacturing a heat exchanger |
US4171832A (en) * | 1976-11-16 | 1979-10-23 | International Harvester Company | Relaxing joints |
US4257788A (en) * | 1979-04-16 | 1981-03-24 | Nicholas Nassir | Power recovery hot gas separator |
US4564504A (en) * | 1983-11-29 | 1986-01-14 | Sorco Corporation | Apparatus for producing an acid compound |
DE3502116A1 (en) * | 1985-01-23 | 1986-07-24 | Halberg Maschinenbau GmbH, 6700 Ludwigshafen | Shell-and-tube heat exchanger with expansion compensation for heat exchange of gases |
US4730669A (en) * | 1986-02-03 | 1988-03-15 | Long Manufacturing Ltd. | Heat exchanger core construction utilizing a diamond-shaped tube-to-header joint configuration |
US4759405A (en) * | 1987-03-18 | 1988-07-26 | Metzger Frederick W | Air conditioner condenser manifold |
US4905766A (en) * | 1987-04-28 | 1990-03-06 | R&G Sloane Mfg. Co., Inc. | Adapter for plastic pipe |
US5064223A (en) * | 1989-10-06 | 1991-11-12 | Ford Motor Company | Throttle modulator assemblies and thermoplastic fluid direction tubes for insertion therein |
US5538261A (en) * | 1994-08-02 | 1996-07-23 | Columbian Chemicals Company | Mechanical heat-exchange tube sealing system |
US20160273838A1 (en) * | 2015-03-18 | 2016-09-22 | Mahle International Gmbh | Exhaust gas heat transfer device |
US9927183B2 (en) * | 2015-03-18 | 2018-03-27 | Mahle International Gmbh | Exhaust gas heat transfer device |
US10447004B2 (en) | 2015-11-19 | 2019-10-15 | Nlight, Inc. | Laser fault tolerance and self-calibration system |
WO2018044813A1 (en) * | 2016-08-31 | 2018-03-08 | Nlight, Inc. | Laser cooling system |
CN109845052A (en) * | 2016-08-31 | 2019-06-04 | 恩耐公司 | Laser cooling system |
US11025034B2 (en) | 2016-08-31 | 2021-06-01 | Nlight, Inc. | Laser cooling system |
CN109845052B (en) * | 2016-08-31 | 2022-01-11 | 恩耐公司 | Laser cooling system |
US10574020B2 (en) | 2016-12-15 | 2020-02-25 | Nlight, Inc. | Fiber laser packaging |
US10784645B2 (en) | 2018-03-12 | 2020-09-22 | Nlight, Inc. | Fiber laser having variably wound optical fiber |
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