EP0117820A1 - Segmental baffle high performance shell and tube heat exchanger - Google Patents

Segmental baffle high performance shell and tube heat exchanger Download PDF

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Publication number
EP0117820A1
EP0117820A1 EP84400377A EP84400377A EP0117820A1 EP 0117820 A1 EP0117820 A1 EP 0117820A1 EP 84400377 A EP84400377 A EP 84400377A EP 84400377 A EP84400377 A EP 84400377A EP 0117820 A1 EP0117820 A1 EP 0117820A1
Authority
EP
European Patent Office
Prior art keywords
shell
heat exchanger
tube heat
baffles
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.)
Granted
Application number
EP84400377A
Other languages
German (de)
French (fr)
Other versions
EP0117820B1 (en
Inventor
David R. Geary
Katherine K. Flamm
Frank T. Morrison
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.)
Baltimore Aircoil Co Inc
Original Assignee
Baltimore Aircoil Co Inc
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 Baltimore Aircoil Co Inc filed Critical Baltimore Aircoil Co Inc
Priority to AT84400377T priority Critical patent/ATE30769T1/en
Publication of EP0117820A1 publication Critical patent/EP0117820A1/en
Application granted granted Critical
Publication of EP0117820B1 publication Critical patent/EP0117820B1/en
Expired legal-status Critical Current

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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

Definitions

  • the invention relates to a high performance shell and tube heat exchanger and a method of obtaining high overall heat transfer coefficients at low pressure drops and low flow rates in said shell and tube heat exchangers wherein the shell and tube heat exchangers utilize segmented shell-side baffles which are oriented one from the other along the line of tubes in the shell and tube heat exchanger at angles other than 180° and preferably at lesser angles such as about 90°.
  • Figure 1 shows a cutaway view of a typical shell and tube heat exchanger with the segmented baffles therein
  • Figure 2 shows the same cutaway view of the baffles and shell without the individual tubes of the shell and tube heat exchanger.
  • Figure 3 shows another embodiment of the baffle having a typical 270° segmental baffle arc angle.
  • FIG. 1 a central portion 1 of a typical shell and tube heat exchanger is shown.
  • Typical flanges for enclosing the shell ends, inlet and outlet piping portions and tube sheets or tube end walls are not shown in the diagram but would be well known to those skilled in the art.
  • This heat exchanger consists of a housing or shell portion 2 shown in cutaway views having therein a plurality of fluted tubes 3. These tubes can be arranged within the heat exchanger in a typical spaced pattern, and the number and size of the tubes will vary dependinq on the type of heat exchanger one is using.
  • the fluid or material to be cooled is typically, though not necessarily always, within the shell 2 of the heat exchanger 1 flowing in one direction whereas the heat exchange fluid inside of the tubes 3 flows in the opposite direction.
  • the tubes 3 are continuously fluted 9, along substantially the complete tube length, except for each tube end 8, where the tube surface is smooth to permit a proper seal or tube end attachment to a separating tube end wall at the ends of tubes which encloses and seals the outside of all tube ends from the outer shell region 10.
  • baffles 4 Located within the shell and tube heat exchanger 1 are a plurality of segmented-circular baffles 4, 5, 6, and 7. These baffles are in the form of a circular segment having an arc of from 90° to about 340°, as shown in Figure 3. These baffles are provided in the heat exchanger 1 such that adjacent baffles are oriented at an angle less than 180° from each other. The baffles are constructed with holes such that they fit snugly over the plurality of tubes 3 provided within the heat exchanger and would prevent the flow of fluid outside the tubes where the baffle is located since the baffle forms a wall against fluid flowing in the direction of the baffle, thereby causing a rotating flow direction or a combination rotating flow with undulating flow pattern.
  • the plurality of baffles 4 through 7 are oriented at an angle of 90° from each other in such a way so that fluid flowing within the shell 2 forms a helical spiral configuration (shown as 815) as it flows along.
  • a portion of the fluid also flows in a wavelike undulating pattern (shown as 816), and it is the combination of the wavelike undulating pattern along with the spiral helical flow pattern that brings about the higher heat transfer efficiency of this type of shell and tube heat exchanger.
  • the baffles can be constructed of any material such as for example metal or other material which preferably is noncorrosive to the fluid flowing therethrough.
  • any angle less than 180° from the previous baffle would be satisfactory; although the preferred angle is substantially 90°.
  • the particular 90° angle is shown in Figure 2 such that if one takes baffle no. 4 with one side of the angle as the diameter line 60 which is an extension of the diameter line of the baffle (9) or chord line 63 of a baffle of the type shown in Figure 3, and one takes the diameter or chord line of the next adjacent baffle (shown as line 61), it can be seen that the twist angle of difference thereto is 90°. This follows similarly with baffles 5 and 6 where the angle is also 90° taken as an extension of the diameters of the adjacent baffles.
  • the baffles are spaced apart in the shell and tube heat exchanger at such a distance as to provide a natural spiral helical and wave-like flow path of any fluid therethrough.
  • the baffles must be located a distance apart at least 0.7 times the diameter of the baffle or shell but not greater than 6.0 times the diamter of the shell and cannot be at such a close or extremely far distance so that any spiral and wave-like pattern of fluid flowing therethrough would be difficult to form.
  • baffles have an outside diametric clearance to fit within the shell with ease.
  • the baffles are not physically attached to the inside wall of the shell, but rather held in position axially by rods (not shown) which parallel the tubes. Therefore, it is conceivable that the baffles can vibrate within the shell due to the clearance tolerances.
  • segmental baffles at 180° twist positions can vibrate over a greater distance in the direction perpendicular to the straight cut segment side, than in any other direction. Therefore, orienting each second baffle at 90° rather than 180° will prevent vibration in the assembly by means of alternate supporting baffle orientation of the straight edge.
  • baffle angle may logically be varied from about 90° to 340° maximum and still arrive at good heat transfer results depending on relative fluid properties and mass transfer rates.

Abstract

The invention comprises a high performance segmented baffled shell and tube heat exchanger (1) in which baffles (4, 5, and 7) are oriented at angles less than 180° adjacent one another.

Description

    BACKGROUND OF THE INVENTION
  • In the past, several methods were used to obtain better heat transfer coefficients in shell and tube heat exchangers. Briefly, these methods were 1) increasing the flow rate and increasing the pressure drop in typical shell and tube heat exchangers, 2) by increasing the heat transfer surface area in shell and tube heat exchangers, such as by using a fluted tube, or 3) by using a different type of heat exchanger than the shell and tube heat exchanger altogether, such as a plate and frame heat exchanger, which utilizes extremely narrow flow passages to enhance heat transfer. Thus, those skilled in the art continue to look for designs of shell and tube heat exchangers of more compact size which occupy less space and/or which lead to high overall heat transfer coefficients combined with low pressure drops over a broad range of fluid flow rates in the shell and tube heat exchangers.
  • SUMMARY OF THE INVENTION
  • The invention relates to a high performance shell and tube heat exchanger and a method of obtaining high overall heat transfer coefficients at low pressure drops and low flow rates in said shell and tube heat exchangers wherein the shell and tube heat exchangers utilize segmented shell-side baffles which are oriented one from the other along the line of tubes in the shell and tube heat exchanger at angles other than 180° and preferably at lesser angles such as about 90°. Further, it has been found that if one uses fluted or corrugated tubes in the shell and tube heat exchanger along with the segmented baffles being spaced adjacent from one another at angles less than 180°, along the direction of flow of the fluid within the shell, overall heat transfer coefficients are improved to a greater extent than one would expect by summing the improvements that are obtained from using (a) fluted tubes with no shell-side baffles plus (b) smooth tubes with non-180° segmental shell-side baffles. This is to say that one expects a given improvement in thermal overall heat transfer coefficient Uo or K when using either (a) or (b) above rather than smooth tubes in a 180° segmentally baffled heat exchanger. However, the unexpected finding is that the given improvement in K when using both (a) and (b) simultaneously is greater than the sum of individual improvements (a) plus (b).
  • Thus, it is an object of this invention to obtain high overall heat transfer coefficients at low pressure drops and low fluid flows in shell and tube heat exchangers by using a shell and tube heat exchanger having segmented shell-side baffles therein which are oriented at angles less than 180° adjacent each other and along the flow direction of the fluid within the shell of said shell and tube heat exchanger.
  • It is a further object of this invention to provide a high performance shell and tube heat exchanger which utilizes the segmented baffles and which also has therein fluted tubes for better heat transfer characteristics.
  • It is a further object of this invention to provide a heat exchanger which eliminates or reduces the amount of tube vibration that may exist due to tube support baffle peripheral clearance tolerances.
  • To better describe the invention there are included herein Figures 1, 2 and 3.
  • Figure 1 shows a cutaway view of a typical shell and tube heat exchanger with the segmented baffles therein, and Figure 2 shows the same cutaway view of the baffles and shell without the individual tubes of the shell and tube heat exchanger. Figure 3 shows another embodiment of the baffle having a typical 270° segmental baffle arc angle.
  • Referring now to Figures 1 and 2, a central portion 1 of a typical shell and tube heat exchanger is shown. Typical flanges for enclosing the shell ends, inlet and outlet piping portions and tube sheets or tube end walls are not shown in the diagram but would be well known to those skilled in the art. This heat exchanger consists of a housing or shell portion 2 shown in cutaway views having therein a plurality of fluted tubes 3. These tubes can be arranged within the heat exchanger in a typical spaced pattern, and the number and size of the tubes will vary dependinq on the type of heat exchanger one is using. The fluid or material to be cooled is typically, though not necessarily always, within the shell 2 of the heat exchanger 1 flowing in one direction whereas the heat exchange fluid inside of the tubes 3 flows in the opposite direction. Also, the tubes 3 are continuously fluted 9, along substantially the complete tube length, except for each tube end 8, where the tube surface is smooth to permit a proper seal or tube end attachment to a separating tube end wall at the ends of tubes which encloses and seals the outside of all tube ends from the outer shell region 10.
  • Located within the shell and tube heat exchanger 1 are a plurality of segmented- circular baffles 4, 5, 6, and 7. These baffles are in the form of a circular segment having an arc of from 90° to about 340°, as shown in Figure 3. These baffles are provided in the heat exchanger 1 such that adjacent baffles are oriented at an angle less than 180° from each other. The baffles are constructed with holes such that they fit snugly over the plurality of tubes 3 provided within the heat exchanger and would prevent the flow of fluid outside the tubes where the baffle is located since the baffle forms a wall against fluid flowing in the direction of the baffle, thereby causing a rotating flow direction or a combination rotating flow with undulating flow pattern.
  • As can be seen in Figure 2, the plurality of baffles 4 through 7 are oriented at an angle of 90° from each other in such a way so that fluid flowing within the shell 2 forms a helical spiral configuration (shown as 815) as it flows along. In addition to forming a helical spiral fluid flow (β15) a portion of the fluid also flows in a wavelike undulating pattern (shown as 816), and it is the combination of the wavelike undulating pattern along with the spiral helical flow pattern that brings about the higher heat transfer efficiency of this type of shell and tube heat exchanger.
  • The baffles can be constructed of any material such as for example metal or other material which preferably is noncorrosive to the fluid flowing therethrough.
  • Although the angles at which the baffles are oriented one from the other is shown in Figure 2 as 90°, one skilled in the art would realize that any angle less than 180° from the previous baffle would be satisfactory; although the preferred angle is substantially 90°. The particular 90° angle is shown in Figure 2 such that if one takes baffle no. 4 with one side of the angle as the diameter line 60 which is an extension of the diameter line of the baffle (9) or chord line 63 of a baffle of the type shown in Figure 3, and one takes the diameter or chord line of the next adjacent baffle (shown as line 61), it can be seen that the twist angle of difference thereto is 90°. This follows similarly with baffles 5 and 6 where the angle is also 90° taken as an extension of the diameters of the adjacent baffles.
  • The baffles are spaced apart in the shell and tube heat exchanger at such a distance as to provide a natural spiral helical and wave-like flow path of any fluid therethrough. The baffles must be located a distance apart at least 0.7 times the diameter of the baffle or shell but not greater than 6.0 times the diamter of the shell and cannot be at such a close or extremely far distance so that any spiral and wave-like pattern of fluid flowing therethrough would be difficult to form.
  • These baffles have an outside diametric clearance to fit within the shell with ease. However, it should be noted that the baffles are not physically attached to the inside wall of the shell, but rather held in position axially by rods (not shown) which parallel the tubes. Therefore, it is conceivable that the baffles can vibrate within the shell due to the clearance tolerances. It is further important to note that segmental baffles at 180° twist positions can vibrate over a greater distance in the direction perpendicular to the straight cut segment side, than in any other direction. Therefore, orienting each second baffle at 90° rather than 180° will prevent vibration in the assembly by means of alternate supporting baffle orientation of the straight edge.
  • Although in Fig. 3 there is shown a segmental baffle angel of 270°, the baffle angle may logically be varied from about 90° to 340° maximum and still arrive at good heat transfer results depending on relative fluid properties and mass transfer rates.
  • The above description refers to an illustration of the invention and is not intended to be limitative thereof. For example, the invention includes consideration for any generic type of segmental baffle, such as single, double, triple, or any multiple-segmental baffle component. Those skilled in the art would realize that other embodiments falling within this invention are possible and these embodiments are intended to be claimed by Applicants.

Claims (6)

1. A shell and tube heat exchanger comprising:
a) an outer shell;
b) a plurality of tubes within said shell;
c) a series of segmental baffles surrounding said tubes and blocking the fluid flow around said tubes, said baffles being adjacent one another and being at an angle of orientation from the next adjacent baffles less than 180°.
2. The shell and tube heat exchanger of Claim 1 wherein the angle at which each adjacent baffle is oriented from the other is substantially 90°.
3. The shell and tube heat exchanger of Claim 1 wherein the tubes are substantially fluted tubes.
4. The shell and tube heat exchanger of Claim 1 wherein the baffles cause a combination of undulating and rotating helical flow in the shell flow area outside of the tubes.
5. The shell and tube heat exchanger of Claim 1 wherein the baffles are circular in form and are located a distance apart of at least 0.7 times the diameter of the baffle but not greater than 6 times the diameter of the baffle.
6. The shell and tube heat exchanger of Claim 1 wherein the segmental baffles have arc angles of from 90° to 340°.
EP84400377A 1983-02-28 1984-02-24 Segmental baffle high performance shell and tube heat exchanger Expired EP0117820B1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
AT84400377T ATE30769T1 (en) 1983-02-28 1984-02-24 SEGMENT BUFFER PLATES FOR A HIGH PERFORMANCE SHELL AND TUBE HEAT EXCHANGER.

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US47080583A 1983-02-28 1983-02-28
US470805 1999-12-22

Publications (2)

Publication Number Publication Date
EP0117820A1 true EP0117820A1 (en) 1984-09-05
EP0117820B1 EP0117820B1 (en) 1987-11-11

Family

ID=23869115

Family Applications (1)

Application Number Title Priority Date Filing Date
EP84400377A Expired EP0117820B1 (en) 1983-02-28 1984-02-24 Segmental baffle high performance shell and tube heat exchanger

Country Status (13)

Country Link
EP (1) EP0117820B1 (en)
JP (1) JPS59164895A (en)
AT (1) ATE30769T1 (en)
AU (1) AU562526B2 (en)
BR (1) BR8304340A (en)
CA (1) CA1218357A (en)
DE (1) DE3467399D1 (en)
DK (1) DK157707C (en)
GR (1) GR79819B (en)
IE (1) IE55000B1 (en)
MX (1) MX158862A (en)
NZ (1) NZ207208A (en)
ZA (1) ZA841421B (en)

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO1985003563A1 (en) * 1984-02-03 1985-08-15 Mellsjoe Carl Gustaf Heat exchanger
GB2298913A (en) * 1995-03-07 1996-09-18 Ngk Insulators Ltd Gas swirling in shell-and-tube heat exchangers
WO2008131616A1 (en) * 2007-04-26 2008-11-06 Dalian Haite Oil Refining Tech A short-circuit-proof heat-exchanger with helical baffles
ES2394406A1 (en) * 2009-11-18 2013-01-31 Valeo Térmico, S.A. Heat exchanger for gases, in particular for the exhaust gases of an engine
CN108469191A (en) * 2018-05-25 2018-08-31 南京科技职业学院 A kind of spiral-plate heat exchanger
CN109186312A (en) * 2018-10-23 2019-01-11 辽宁科技大学 One kind can scale removal baffling plate heat dissipating device
DE102019126535A1 (en) * 2019-10-01 2021-04-01 Bitzer Kühlmaschinenbau Gmbh Heat exchanger, refrigeration or heating system with such a heat exchanger
EP4006476A4 (en) * 2019-07-25 2023-08-02 LG Electronics Inc. Heat exchanger

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN100386586C (en) * 2006-03-20 2008-05-07 西安交通大学 Multiple shell pass screw baffle pipe shell type heat exchanger
JP2012172907A (en) * 2011-02-22 2012-09-10 Cku:Kk Heat exchanger of shell-and-tube system with fin arranged in spiral staircase shape

Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR65106E (en) * 1953-12-31 1956-01-26 Chausson Usines Sa heat exchanger in particular for aircraft and similar applications
CH442380A (en) * 1966-05-31 1967-08-31 Bbc Brown Boveri & Cie Device for sealing a tubular heat exchanger
FR2036806A7 (en) * 1969-04-03 1970-12-31 Ara Barrenechea Constanc Heat-exchanger
US3630276A (en) * 1970-02-10 1971-12-28 Nasa Shell-side liquid metal boiler
US3696863A (en) * 1970-01-02 1972-10-10 Itt Inner-outer finned heat transfer tubes
DE2410292A1 (en) * 1974-03-04 1975-09-18 Cass International Gmbh Shell-and-tube heat exchanger - with sector-shaped tube-supporting baffle plates
US4183401A (en) * 1977-09-28 1980-01-15 Carrier Corporation Combination tube sheet and baffle

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5577481A (en) * 1978-11-30 1980-06-11 Matsushita Electric Works Ltd Motor driver

Patent Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR65106E (en) * 1953-12-31 1956-01-26 Chausson Usines Sa heat exchanger in particular for aircraft and similar applications
CH442380A (en) * 1966-05-31 1967-08-31 Bbc Brown Boveri & Cie Device for sealing a tubular heat exchanger
FR2036806A7 (en) * 1969-04-03 1970-12-31 Ara Barrenechea Constanc Heat-exchanger
US3696863A (en) * 1970-01-02 1972-10-10 Itt Inner-outer finned heat transfer tubes
US3630276A (en) * 1970-02-10 1971-12-28 Nasa Shell-side liquid metal boiler
DE2410292A1 (en) * 1974-03-04 1975-09-18 Cass International Gmbh Shell-and-tube heat exchanger - with sector-shaped tube-supporting baffle plates
US4183401A (en) * 1977-09-28 1980-01-15 Carrier Corporation Combination tube sheet and baffle

Cited By (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO1985003563A1 (en) * 1984-02-03 1985-08-15 Mellsjoe Carl Gustaf Heat exchanger
US4697636A (en) * 1984-02-03 1987-10-06 Mellsjoe Carl G Heat exchanger with helical fluid flow
GB2298913A (en) * 1995-03-07 1996-09-18 Ngk Insulators Ltd Gas swirling in shell-and-tube heat exchangers
GB2298913B (en) * 1995-03-07 1999-08-11 Ngk Insulators Ltd Heat exchangers
WO2008131616A1 (en) * 2007-04-26 2008-11-06 Dalian Haite Oil Refining Tech A short-circuit-proof heat-exchanger with helical baffles
ES2394406A1 (en) * 2009-11-18 2013-01-31 Valeo Térmico, S.A. Heat exchanger for gases, in particular for the exhaust gases of an engine
CN108469191A (en) * 2018-05-25 2018-08-31 南京科技职业学院 A kind of spiral-plate heat exchanger
CN108469191B (en) * 2018-05-25 2024-04-16 南京科技职业学院 Spiral plate heat exchanger
CN109186312A (en) * 2018-10-23 2019-01-11 辽宁科技大学 One kind can scale removal baffling plate heat dissipating device
CN109186312B (en) * 2018-10-23 2023-09-26 辽宁科技大学 Heat radiator with scale-removing baffle plate
EP4006476A4 (en) * 2019-07-25 2023-08-02 LG Electronics Inc. Heat exchanger
DE102019126535A1 (en) * 2019-10-01 2021-04-01 Bitzer Kühlmaschinenbau Gmbh Heat exchanger, refrigeration or heating system with such a heat exchanger
EP3800418A1 (en) 2019-10-01 2021-04-07 BITZER Kühlmaschinenbau GmbH Heat exchanger, refrigerating or heating system with such a heat exchanger

Also Published As

Publication number Publication date
DK105184A (en) 1984-08-29
DK157707B (en) 1990-02-05
NZ207208A (en) 1987-02-20
MX158862A (en) 1989-03-20
DK105184D0 (en) 1984-02-27
AU2507584A (en) 1984-09-06
ZA841421B (en) 1985-10-30
DK157707C (en) 1990-06-25
EP0117820B1 (en) 1987-11-11
IE840449L (en) 1984-08-28
DE3467399D1 (en) 1987-12-17
ATE30769T1 (en) 1987-11-15
GR79819B (en) 1984-10-31
IE55000B1 (en) 1990-04-11
AU562526B2 (en) 1987-06-11
JPS59164895A (en) 1984-09-18
BR8304340A (en) 1984-11-06
CA1218357A (en) 1987-02-24

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