GB2251299A - Heat exchanger - Google Patents
Heat exchanger Download PDFInfo
- Publication number
- GB2251299A GB2251299A GB9124898A GB9124898A GB2251299A GB 2251299 A GB2251299 A GB 2251299A GB 9124898 A GB9124898 A GB 9124898A GB 9124898 A GB9124898 A GB 9124898A GB 2251299 A GB2251299 A GB 2251299A
- Authority
- GB
- United Kingdom
- Prior art keywords
- heat exchanger
- plates
- passages
- vessel
- fluid
- 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.)
- Granted
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F28—HEAT EXCHANGE IN GENERAL
- F28D—HEAT-EXCHANGE APPARATUS, NOT PROVIDED FOR IN ANOTHER SUBCLASS, IN WHICH THE HEAT-EXCHANGE MEDIA DO NOT COME INTO DIRECT CONTACT
- F28D9/00—Heat-exchange apparatus having stationary plate-like or laminated conduit assemblies for both heat-exchange media, the media being in contact with different sides of a conduit wall
- F28D9/0006—Heat-exchange apparatus having stationary plate-like or laminated conduit assemblies for both heat-exchange media, the media being in contact with different sides of a conduit wall the plate-like or laminated conduits being enclosed within a pressure vessel
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F28—HEAT EXCHANGE IN GENERAL
- F28D—HEAT-EXCHANGE APPARATUS, NOT PROVIDED FOR IN ANOTHER SUBCLASS, IN WHICH THE HEAT-EXCHANGE MEDIA DO NOT COME INTO DIRECT CONTACT
- F28D9/00—Heat-exchange apparatus having stationary plate-like or laminated conduit assemblies for both heat-exchange media, the media being in contact with different sides of a conduit wall
- F28D9/0012—Heat-exchange apparatus having stationary plate-like or laminated conduit assemblies for both heat-exchange media, the media being in contact with different sides of a conduit wall the apparatus having an annular form
- F28D9/0018—Heat-exchange apparatus having stationary plate-like or laminated conduit assemblies for both heat-exchange media, the media being in contact with different sides of a conduit wall the apparatus having an annular form without any annular circulation of the heat exchange media
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F28—HEAT EXCHANGE IN GENERAL
- F28D—HEAT-EXCHANGE APPARATUS, NOT PROVIDED FOR IN ANOTHER SUBCLASS, IN WHICH THE HEAT-EXCHANGE MEDIA DO NOT COME INTO DIRECT CONTACT
- F28D9/00—Heat-exchange apparatus having stationary plate-like or laminated conduit assemblies for both heat-exchange media, the media being in contact with different sides of a conduit wall
- F28D9/0025—Heat-exchange apparatus having stationary plate-like or laminated conduit assemblies for both heat-exchange media, the media being in contact with different sides of a conduit wall the conduits being formed by zig-zag bend plates
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F28—HEAT EXCHANGE IN GENERAL
- F28D—HEAT-EXCHANGE APPARATUS, NOT PROVIDED FOR IN ANOTHER SUBCLASS, IN WHICH THE HEAT-EXCHANGE MEDIA DO NOT COME INTO DIRECT CONTACT
- F28D9/00—Heat-exchange apparatus having stationary plate-like or laminated conduit assemblies for both heat-exchange media, the media being in contact with different sides of a conduit wall
- F28D9/0093—Multi-circuit heat-exchangers, e.g. integrating different heat exchange sections in the same unit or heat-exchangers for more than two fluids
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F28—HEAT EXCHANGE IN GENERAL
- F28F—DETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
- F28F2250/00—Arrangements for modifying the flow of the heat exchange media, e.g. flow guiding means; Particular flow patterns
- F28F2250/10—Particular pattern of flow of the heat exchange media
- F28F2250/102—Particular pattern of flow of the heat exchange media with change of flow direction
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
Heat Exchanger 22-,12,1 P This invention relates to a plate-type heat
exchanger, and particularly, but not exclusively to a heat exchanger suitable for use where one fluid is at a high pressure.
Heat exchangers enable heat transfer to take place between two fluids by causing them to flow in adjacent ducts. In plate-type heat exchangers ducts are defined between parallel spaced-apart plates, and adjacent plates may be spaced apart for example by fins integral with one or other plate, or by a corrugated spacer. Where one or both fluids may be at a high pressure (e. g. between 10 and 300 atm.) the plates may be exposed to large forces; they may be held together by metallurgically bonding adjacent plates together so as to minimi ze the unsupported areas, for example by brazing the ends of the fins on one plate onto the adjacent plate, or they may be held together by bolts extending between thick end plates. Where corrosion is encountered it can be worsened by electrochemical differences between the metal of the braze and the plate, while the use of bolts puts the end plates under very large stresses if the fluid pressures are high.
According to the present invention there is provided a heat exchanger suitable for heat exchange between two fluids at least one of which is at a high pressure above 10 atmospheres comprising a hollow cylindrical pressure vessel through which a high pressure fluid may flow, an assembly comprising a plurality of spaced apart plates within the vessel defining passages between the plates for both the fluids, and ducts for flow of the lower pressure fluid to and from the assembly of plates, pairs of adjacent plates defining between them passages for the lower pressure fluid extending in respective substantially radial, angularlyspaced, planes within an annular region coaxial with the - 2 pressure vessel, and pairs of adjacent plates being defined by a folded sheet.
The plates may be flat and held apart by separators, or may be ridged to define fins, or may be corrugated. The separators, fins, or corrugations may be arranged to constrain the fluid flow into particular desired paths, for example to ensure two fluid flows on opposite sides of a plate are in countercurrent. The plates may be of any material which conducts heat sufficiently well, for example of metals such as titanium, or non-metals such as ceramics or plastics material. The material must be chosen in accordance with the pressures and temperature differences to which it will be subjected in use, and to the required heat flux.
Desirably a plurality of the plates, and more desirably all the plates, are defined by a single long sheet folded into a zig-zag. By using folded sheets the length of welded edges is reduced, and such a zig-zag sheet leads-to a still greater reduction. The use of a circular geometry for the plates enables better use to be made of the volume of the pressure vessel compared to a conventional rectangular geometry. Preferably the radial planes defined by the passages between pairs of adjacent plates are at equally spaced angles around the longitudinal axis of the vessel.
The present invention provides a heat exchanger in which the pressure forces are primarily taken by the cylindrical pressure vessel, which may form a part of a high pressure pipeline, and nay be the same diameter as the pipeline. It enables a simple compact heat exchanger to be made of corrosion-resistant materials such as titanium and its alloys, and enables wastage of such material during construction to be minimized. The heat exchanger can provide more than 100 m2/m3 of heat transfer surfaces, preferably more than 200 m2/m3, for example 250 m2/m3.
Such a compact heat exchanger would be suitable for use for example on a production platform in an off-shore gas-field, where the fluids would be high pressure natural gas (principally methane, along with carbon dioxide and water vapour) at a temperature between about 1501 and 2501C, and low pressure sea-water or fresh water/glycol mixture.
Since the heat exchanger is smaller and lighter than heat exchangers used hitherto it enables consequential space and weight reductions to be made in other aspects of the platform.
The pressure vessel might be of diameter between about is 0.1m and 1.5m, a diameter of about 1.Om being suitable for the off- shore use mentioned above. The annular region occupied by the plates is preferably of inner diameter about half that of the pressure vessel, and may be of outer diameter just less than that of the vessel. The plates might be of length between about half and about five times the diameter of the pressure vessel; for the off-shore use described, the plates might be between about lm and 4m or even 5m long, the preferred length being about 3m. The folded sheet might be of stainless steel or of titanium alloy, and of thickness between about 0.3 and 1.2rim, preferably about 0. 5mm. The gap between the pairs of adjacent plates, which define a passage for the low pressure fluid, might be between 2mm and 1Omm, preferably between 2mm and 6mm, most preferably about 3mn.
The lower pressure fluid ducts may provide support for the assembly of the plates within the vessel. Strains due to thermal expansion and contraction of the heat exchanger have to be withstood by these ducts, one or both of which may incorporate for example strain-accommodating bends. The ducts may be connected to opposite ends of the plate assembly, or alternatively may both be connected to the is same end of the assembly (for example with the ducts being coaxial). If the cylindrical pressure vessel is vertical the latter arrangement of the ducts enables the plate assembly to be withdrawn easily from the pressure vessel, for example for cleaning.
The invention will now be further and more particularly described, by way of example only, and with reference to the accompanying drawings in which:
Figure 1 shows a transverse sectional view of a heat exchanger (on the line I-I of Figure 2); Figure 2 shows a longitudina 1 sectional view of the heat exchanger of Figure 1, on the line II-II of Figure 1, but to a smaller scale; Figure 3 shows to a larger scale than Figure 1, a transverse sectional view partly broken away of a modification to the heat exchanger of Figure 1; - Figure 4 shows a longitudinal sectional view of an alternative heat exchanger; Figure 5 shows a transverse sectional view partly broken away of another alternative heat exchanger; and Figure 6 shows a longitudinal sectional view of another modification to the heat exchanger of Figure 1.
Referring to Figure 1 there is shown a transverse sectional view of a compact heat exchanger 10 for use on an off-shore gas production platform, for bringing about heat transfer between a stream of natural gas at a pressure of 200 atmospheres and a temperature usually about 1501C (but which may be as high as 250IC), and a stream of coolant water. The heat exchanger 10 incorporates a cylindrical tubular titanium alloy pressure vessel 12 of external diameter 0.50m, which is installed as part of a pipeline of the same diameter which carries the gas stream.
A cylindrical_forne.r 14, of external diameter 0.25m, is supported coaxially within the vessel 12, so an annular space 16 is defined between the former 14 and the vessel 12. Within the space 16 passages 18 and 20 are defined, for the gas and for the water respectively, by a long rectangular sheet 22 of O.Smm thick titanium alloy folded into a zig-zag to form almost four hundred flat plates, the ends of the sheet 22 being welded together; this zig-zag extends throughout the space 16 as indicated by the chain-dotted line, each plate of the zig-zag extending from the former 14 to within lmm of the inner surface of the vessel 12.
Each passage 18 is of triangular cross-section tapering towards zero width nearest the former 14, and of width 4mm at its radially outermost part. Each passage 20 is of uniform width 3mn and lies in a respective radial plane, and the plates on either side of a passage 20 are held apart by a rectangular sheet of coarse woven wire nesh 24 (two wire mesh sheets 24 are indicated diagrammatically in Figure 1). The sheet 22 is thus folded into a sharp fold adjacent to the former 14, and a rounded fold enclosing the mesh 24 remote from the former 14.
Referring now to Figure 2, the former 14 is closed at each end and is supported by coaxial perforated tubes 26, one at each end, which extend from the mouths of tubes 28; 6 - the tubes 28 are of the same diameter as, and coaxial with, the former 14. There is a gap 30 of width 0.1m bridged by the perforated tube 26 at each end between the mouth of' the L tube 28 and the former 14. The zig-zag plates defined by the sheet 22 extend beyond the former 14 at each end and are welded to the outer surface of the tube 28, and the ends of the plates on either side of each passage 20 are bent towards each other and welded together, so as to seal the ends of each passage 20. The tubes 28 support the assembly of the former 14 and the zig-ga.g^sheet 22 within the pressure vessel 12, each tube 28 tapering to a diameter of 0.15m and turning through a right angle to protrude through the wall of the pressure vessel 12, to which it is welded; one of the tubes 28 is bent to form an S-bend 32, in order-to accommodate any thermal strains.
In use coolant water is caused to flow to and from, the heat exchanger 10 through the tubes 28F as the hot high pressure gas flows along the pipeline and along the pressure vessel 12. The gas flows through the passages 18, while the water flows through one gap 30 into and along the passages 20 to emerge through the other gap 30. The pressure of the gas is contained by the vessel 12, and the mesh sheets 24 prevent the passages 20 from being crushed.
The former 14 helps to support the zig-zag sheet 22 against the radial inward forces due to gas pressure. The heat about 250 exchanger 10 provides a heat exchange area ol m2/m3 , and so inay be referred to as compact.
The heat exchanger 10 may be modified in a variety of ways. For example each passage 20 might contain, instead of a inesh sheet 24, a corrugated titanium plate (not shown), the orientation of the corrugations being arranged to ensure the low pressure fluid follows a particular route through the passage 20, and ensuring adequate fluid flow at all parts of the passage. Such a corrugated plate might be 7 - slitted with the corrugations oriented approximately transverse to each slit, but with the peaks on one side aligning with the troughs on the other side of that slit, so the fluid may flow alternately on one side and then the other of the corrugated plate. In another modification the ends of the passages 20 might be sealed by welding the adjacent plate edges to a titanium strip (not shown), the strip either occupying the entire thickness (3mm) of the gap between the plates, or being thinner in which case some bending of the ends of the plates would again be necessary. Furthermore such strips might extend radially inwards beyond the inside of the zig- zag sheet 22 and be welded to each other to define a ring to which the mouth of the tube 28 is connected.
Referring to Figure 3, two modifications to the heat exchanger 10 are illustrated. To ensure the passages 20 remain in their radial planes and so to ensure the passages 18 are not distorted, one or more spacer wires 36 or strips may be provided in each passage 18 extending parallel to the 1(?ngitudinal axis of the assembly from one end of the passage 18 to the other. At the ends of the assembly all the spacer wires 36 at a particular radius from the axis micht be fixed to a ring (not shown) or be welded to one or other of the adjacent plates to ensure they cannot be displaced during operation. Alternatively or additionally the radially outermost parts 38 of the sheet 22 might be bent over so as to touch the adjacent plate on the opposite side of the passage 18.
Referring now to Figure 4 there is shown an alternative heat exchanger 40 with most of its features in common with the heat exchanger 10, identical components being referred to by the same reference numbers. The water flow tubes 28 and flow passages 20 are substantially the same as in the heat exchanger 10. However the ends of the plates defined by the zig-zag sheet 22, at each end of the assembly, are all welded to an annular end plate 42, so this plate 42 seals the ends of the passages 20. There is a radial gap 43 of width 50mm between the radially outermost folds of the zig-zag sheet 22 and the inner surface of the pressure vessel 12, so althouqh the ends of the gas passages 18 are closed by the end plates 42 the gas can flow into the passages 18 via the radial gap 43 between the outer edge of the end plate 42 and the vessel 12. Flow 1()- -along the gap 43 is prev.ented by a tubular member 44 fixed to the inner surface of the vessel 12, which extends along the entire length of the assembly apart from O.lm at each end. The gas flow is hence as indicated by the broken line arrow. It will be appreciated that the heat exchanger 40 may have the modifications to the gas flow passage 18 shown in Figure 3 (spacer wires 36 and bent over outer parts 38) but that these features must not extend to the ends of the passages 18, and if provided preferably terminate at least O.lm from each end.
Referring now to Figure 5 there is shown another alternative heat exchanger 50, for heat exchange amongst three fluids. Many of its features are substantially identical to those of heat exchanger 10, identical components being referred to by the same reference numbers. Between a cylindrical former 14 and a concentric cylindrical pressure vessel 12 a first long titanium sheet 52 is folded into a zig-zag to define passages 54 of constant width 4mm for a first low-pressure fluid (for example coolant water), each passage 54 enclosing a coarse mesh sheet 24 as a separator. Each passage 54 lies in a respective radial plane, and between one and the next the sheet 52 is folded round a 5mm wide spacer bar 56. A second long titanium sheet 58 is folded into a zig-zag to define passages 60 of constant width 3mm for a second low-pressure fluid (for example a second, low pressure - 9 gas or water), each passage 60 also enclosing a coarse mesh sheet 24 as a separator. Each passage 60 lies in a respective radial plane midway between planes in which adjacent passages 54 lie and between one passage 60 and the next the sheet 58 defines an arcuate portion 62 which lies on the inner surface of the pressure vessel 12. The high pressure gas can flow along the gaps 64 between the interleaved zig-zag sheets 52 and 58.
At the ends of the assembly the passage.s-54 and 60 are sealed, as described in relation to heat exchanger 10. The first low-pressurefluid is supplied to, and issues from, the passages 54 via tubes supporting the ends of the former 14, as described in relation to heat exchanger 10. The second low-pressure fluid is supplied to, and issues from, the passages 60, via respective headers (not shown) on the outside of the pressure vessel 12 and slots or perforations (not shown) through the wall of the pressure vessel 12, at each end of the asseribly.
In a modification (not shown), the pressure vessel 12 is provided with a sleeve spaced apart from its inner surface over a length slightly greater than that of the heat exchange assembly, the sleeve being welded to the vessel 12 around each end, and the central portion of the annular space between the sleeve and the vessel 12 being occupied by a tubular member. The arcuate portions 62 of the sheet 58 lie on the inner surface of the sleeve, and the ends of the passages 60 are sealed by welding adjacent plates to each other and to the sleeve. The unobstructed portions at each end of the annular space between the sleeve and the vessel 12 act as headers, to which a fluid may be supplied through ports in the vessel 12.
In a further modification (not shown) to the heat exchanger 50 there are half as many of the outer passages as of the inner passages 54, the arcuate portions 62 of the sheet 58 being long enough that a pair of adjacent passages 54 fit between one passage 60 and the next. Between each such pair of passages 54 the sheet 52 is folded into a sharp fold, the spacer bar 56 being omitted.
Referring now to Figure 6 there is shown a longitudinal sectional view of a modified version of the compact heat exchanger 10 of Figure 1, the same components being referred to by the same reference numerals. A heat exchanger 66 comprises a zig-zag sheet 22 defining passages for gas and for a liquid, as described previously, the sheet 22 occupying the annular space between the inner surface of a tubular pressure vessel 12 and a cylindrical former 68. The longitudinal axes of the vessel 12 and of the heat exchanger 66 are vertical. The former 68 is supported at both ends by coaxial perforated tubes 26. At the lower end the tube 26 bridges the gap between the former 68 and an end cap 70 of the same diameter as the former 68, while at the top end the tube 26 bridges the gap betyTeen the former 68 and a support tube 72. An outlet tube 74 communicates with the space between the lower end of the former 68 and the cap 70,-and extends upwardly through the former 68 and coaxially along the support tu;,_ 72.
Above the heat exchanger 66 the tubular pressure vessel 12 is closed by an end plate 75 secured to the vessel 12 by bolts 76 (only two are shown), below which a high pressure duct 78 branches off the vessel 12. The support tube 72 is fixed to the plate 75, through which it extends. Above the plate 75 the tube 72 is closed at its top end, and to it is fixed a lifting ring 80. A duct 82 branches off from the tube 72, and the tube 74 emerges through the wall of the tube 72. Hence in use a high pressure gas flows through the pressure vessel 12 and the 11 - high pressure duct 78, while a coolant liquid can be passed via the duct 82 and the tube 72 into and through the heat exchanger 66, to emerge through the coaxial tube 74. This arrangement enables the heat exchanger 66 to be removed from the vessel 12, for example for cleaning.
Claims (11)
1. A heat exchanger suitable for heat exchange between two fluids at least one of which is at a high pressure above 10 atmospheres comprising a hollow cylindrical pressure vessel through which a high pressure fluid may flow, an assembly comprising a plurality of spaced apart plates within the vessel defining passages between the plates for both the fluids, and ducts for flow of the lower pressure fluid to and from the assembly of plates, pairs of adjacent plates defining between then passages for the lower pressure fluid extending in respective substantially radial, angularly-spaced, planes within an annular region coaxial with the pressure vessel, and pairs of adjacent plates being defined by a folded sheet.
2. A heat exchanger as claimed in Claim 1 wherein a plurality of the plates are defined by a single long sheet folded into a zig-zag.
3.. A heat exchanger as claimed in Claim 2 wherein all the plates are defined by a single long sheet folded into a zig-zag.
4. A heat exchanger as claimed in any one of the. preceding Claims wherein the said radial planes are at equally spaced angles around the longitudinal axis of the vessel.
5. A heat exchanger as claimed in any one of the preceding Claims wherein the radial width of the annular region is about half the radius of the plate assembly.
6. A heat exchanger as claimed in any one of the preceding Claims wherein the heat transfer surface area within the heat exchanger is more than 100 m2/m3.
- 13
7. A heat exchanger as claimed in Claim 6 wherein the heat transfer surface area is more than 200 M2/M3.
8. A heat exchanger as claimed in any one of the preceding Claims wherein the ducts support the plate assembly within the pressure vessel.
9. A heat exchanger as claimed in Claim 8 wherein the ducts are both connected to the same end of the plate assembly.
10. A heat exchanger as claimed in any one of the preceding Claims including pairs of plates interleaved between the aforementioned pairs of plates and arranged to define passages for a third fluid, the passages for the third fluid extending in radial planes and communicating at their radially outermost parts with headers for the third fluid.
11. A heat exchanger suitable for heat exchange between two fluids at least one of which is at a high pressure of at least 10 atmospheres substantially as hereinbefore described with reference to, and as shown in, Figures 1 and 2, or Figure 3, 4, 5 or 6 of the accompanying drawings.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB909027994A GB9027994D0 (en) | 1990-12-22 | 1990-12-22 | Heat exchanger |
Publications (3)
Publication Number | Publication Date |
---|---|
GB9124898D0 GB9124898D0 (en) | 1992-01-15 |
GB2251299A true GB2251299A (en) | 1992-07-01 |
GB2251299B GB2251299B (en) | 1994-04-27 |
Family
ID=10687577
Family Applications (2)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB909027994A Pending GB9027994D0 (en) | 1990-12-22 | 1990-12-22 | Heat exchanger |
GB9124898A Expired - Fee Related GB2251299B (en) | 1990-12-22 | 1991-11-22 | Heat exchanger |
Family Applications Before (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB909027994A Pending GB9027994D0 (en) | 1990-12-22 | 1990-12-22 | Heat exchanger |
Country Status (3)
Country | Link |
---|---|
EP (1) | EP0492799A1 (en) |
JP (1) | JPH04292789A (en) |
GB (2) | GB9027994D0 (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2360577A (en) * | 1999-12-23 | 2001-09-26 | Framo Developements As | Heat exchanger construction |
DE102012003347A1 (en) * | 2012-02-21 | 2013-08-22 | Babcock Borsig Steinmüller Gmbh | Annular recuperator for transferring heat from warmer fluid stream to cold fluid stream for micro gas turbine plant, has two passages that are separated from each other by wall, and fluid streams comprising filling arranged in passages |
Families Citing this family (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP3685890B2 (en) * | 1996-10-17 | 2005-08-24 | 本田技研工業株式会社 | Heat exchanger |
DE69812671T2 (en) * | 1997-01-27 | 2003-11-06 | Honda Motor Co Ltd | Heat Exchanger |
GB2343643B (en) * | 1998-11-10 | 2002-01-16 | Centrax Ltd | Heat exchanger |
US20020079085A1 (en) * | 2000-12-27 | 2002-06-27 | Rentz Lawrence Edward | Turbine recuperator |
US6729387B2 (en) * | 2002-06-12 | 2004-05-04 | Avava Technology Corp. | Double sided heat exchanger core |
Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB235674A (en) * | 1924-04-07 | 1925-06-25 | Aircraft Disposal Company Ltd | Improvements in radiators for cooling liquids for internal combustion engines |
GB320279A (en) * | 1928-12-11 | 1929-10-10 | Heenan & Froude Ltd | Improvements in heat exchangers |
Family Cites Families (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE729339C (en) * | 1937-03-12 | 1942-12-14 | Krupp Ag | Heat exchanger for pressurized heat exchange media for carrying out chemical processes |
NL66306C (en) * | 1945-06-21 | |||
DE887951C (en) * | 1949-03-13 | 1953-11-12 | Ernst Goebels | Heat exchanger |
US2953110A (en) * | 1954-01-22 | 1960-09-20 | W J Fraser & Co Ltd | Reciprocally folded sheet metal structures |
NL7105840A (en) * | 1971-04-29 | 1972-10-31 | ||
US4109710A (en) * | 1974-04-30 | 1978-08-29 | Kernforschungsanlage Julich Gesellschaft Mit Beschrankter Haftung | Heat exchanger |
CA1038369A (en) * | 1974-05-01 | 1978-09-12 | Des Champs Laboratories | Heat exchanger and heat recovery system |
US3983933A (en) * | 1974-11-05 | 1976-10-05 | Nasa | Heat exchanger |
US4267882A (en) * | 1980-03-03 | 1981-05-19 | Combustion Engineering, Inc. | Heat exchanger for cooling a high pressure gas |
FR2647198B1 (en) * | 1989-05-22 | 1991-07-19 | Packinox Sa | PLATE CONDUIT HEAT EXCHANGER |
-
1990
- 1990-12-22 GB GB909027994A patent/GB9027994D0/en active Pending
-
1991
- 1991-11-22 EP EP91310773A patent/EP0492799A1/en not_active Withdrawn
- 1991-11-22 GB GB9124898A patent/GB2251299B/en not_active Expired - Fee Related
- 1991-12-20 JP JP3338921A patent/JPH04292789A/en active Pending
Patent Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB235674A (en) * | 1924-04-07 | 1925-06-25 | Aircraft Disposal Company Ltd | Improvements in radiators for cooling liquids for internal combustion engines |
GB320279A (en) * | 1928-12-11 | 1929-10-10 | Heenan & Froude Ltd | Improvements in heat exchangers |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2360577A (en) * | 1999-12-23 | 2001-09-26 | Framo Developements As | Heat exchanger construction |
DE102012003347A1 (en) * | 2012-02-21 | 2013-08-22 | Babcock Borsig Steinmüller Gmbh | Annular recuperator for transferring heat from warmer fluid stream to cold fluid stream for micro gas turbine plant, has two passages that are separated from each other by wall, and fluid streams comprising filling arranged in passages |
Also Published As
Publication number | Publication date |
---|---|
EP0492799A1 (en) | 1992-07-01 |
GB2251299B (en) | 1994-04-27 |
GB9124898D0 (en) | 1992-01-15 |
GB9027994D0 (en) | 1991-02-13 |
JPH04292789A (en) | 1992-10-16 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US3610330A (en) | Heat exchanger | |
US20090065185A1 (en) | Tube Bundle Heat Exchanger | |
EP2118611B1 (en) | Assembly of baffles and seals | |
JPH01130939A (en) | Honeycomb structure assembly | |
AU2008257595B2 (en) | Heat exchanger shell assembly and method of assembling | |
BR0202426B1 (en) | plate assembly for a heat exchanger and heat exchanger. | |
EP1347258B1 (en) | Heat exchanger with tube supports | |
EP2594884A1 (en) | Plate heat exchanger and method for manufacturing of a plate heat exchanger | |
US5871045A (en) | Heat exchanger | |
GB2251299A (en) | Heat exchanger | |
WO2011149617A2 (en) | Multipass tubular heat exchanger and associated pass partition plate, channel cover, and methods | |
US4554135A (en) | Ammonia converter | |
JP3052121B2 (en) | Heat exchanger | |
JP3582741B2 (en) | Cooling system | |
Reay | Compact heat exchangers: A review of current equipment and R&D in the field | |
JP2020131164A (en) | Reaction apparatus | |
JPH08126837A (en) | Vessel | |
US4921684A (en) | Ammonia conversion process | |
JPH0325038Y2 (en) | ||
JP3374345B2 (en) | Channel cover for multi-tube heat exchanger | |
JPS61500178A (en) | Heat exchanger | |
SU909559A1 (en) | Heat-exchanging element | |
GB2284472A (en) | Spirally wound plate heat exchanger | |
AU628099B2 (en) | High pressure gas/liquid heat exchanger | |
JPS61291894A (en) | Finned pipe for heat exchanger and heat exchanger using it |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
PCNP | Patent ceased through non-payment of renewal fee |
Effective date: 19951122 |