US3554273A - Elements for regenerative heat exchangers - Google Patents

Elements for regenerative heat exchangers Download PDF

Info

Publication number
US3554273A
US3554273A US854854A US3554273DA US3554273A US 3554273 A US3554273 A US 3554273A US 854854 A US854854 A US 854854A US 3554273D A US3554273D A US 3554273DA US 3554273 A US3554273 A US 3554273A
Authority
US
United States
Prior art keywords
corrugations
protuberances
parallel
plates
approximately
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
US854854A
Inventor
Gerhard Kritzler
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.)
Apparatebau Rothemuehle Brandt and Kritzler GmbH
Original Assignee
Apparatebau Rothemuehle Brandt and Kritzler GmbH
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 Apparatebau Rothemuehle Brandt and Kritzler GmbH filed Critical Apparatebau Rothemuehle Brandt and Kritzler GmbH
Application granted granted Critical
Publication of US3554273A publication Critical patent/US3554273A/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
    • F28DHEAT-EXCHANGE APPARATUS, NOT PROVIDED FOR IN ANOTHER SUBCLASS, IN WHICH THE HEAT-EXCHANGE MEDIA DO NOT COME INTO DIRECT CONTACT
    • F28D17/00Regenerative heat-exchange apparatus in which a stationary intermediate heat-transfer medium or body is contacted successively by each heat-exchange medium, e.g. using granular particles
    • F28D17/02Regenerative heat-exchange apparatus in which a stationary intermediate heat-transfer medium or body is contacted successively by each heat-exchange medium, e.g. using granular particles using rigid bodies, e.g. of porous material
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F28HEAT EXCHANGE IN GENERAL
    • F28DHEAT-EXCHANGE APPARATUS, NOT PROVIDED FOR IN ANOTHER SUBCLASS, IN WHICH THE HEAT-EXCHANGE MEDIA DO NOT COME INTO DIRECT CONTACT
    • F28D19/00Regenerative heat-exchange apparatus in which the intermediate heat-transfer medium or body is moved successively into contact with each heat-exchange medium
    • F28D19/04Regenerative heat-exchange apparatus in which the intermediate heat-transfer medium or body is moved successively into contact with each heat-exchange medium using rigid bodies, e.g. mounted on a movable carrier
    • F28D19/041Regenerative heat-exchange apparatus in which the intermediate heat-transfer medium or body is moved successively into contact with each heat-exchange medium using rigid bodies, e.g. mounted on a movable carrier with axial flow through the intermediate heat-transfer medium
    • F28D19/042Rotors; Assemblies of heat absorbing masses

Definitions

  • the present'invention has the object of improving the heat transfer in the narrow flow ducts between the metal heating elements, with the packing density remaining unchanged, by creation of periodically repeated delays and accelerations of the flow, which areco'nnected withan increased turbulence.
  • this object is fulfilled in that the spacing metal heating element'shape between the planar 0r shallowly undulated plates is provided at specified distances with deep corrugations, which run parallel to the direction of flow of media through the pack and delimit the small gas passage ducts between the metal plates, which form with a specified hydraulic radius sihalL'rectangular flow cross sections for the gases, the'broader delimitation walls of which have at intervals in the flow direction laminar protuberances,
  • the distance apart of the deep corrugations shall amount to 10-20 times the size of the hydraulic radius of the small flow passages between the metal plates, whilst the length along the direction of tlow of the laminar protuberances between these corrugations shall amount to 10-15 times the size of this hydraulic radius.
  • a metal element 1 shows part of a metal element 1 with one wave of anapproximately sinusoidal corrugation each of an amplitudec/Z 1.0 to 1.2 r,,, of a wave length of l to 6.3 r,, and parallel to each other at distances of a 10-20 r where r, is the hydraulic radius of gas passage ducts which are formed by the corrugations.
  • the plates 1 are made up into packs with shallowly undulated plates '2 or plane plates 2a alternately with the plates 1.
  • the packs are placed in a regenerator chamber so that the corrugations are along the axial direction, and gas flow takes place in the directions of the arrows F1 and F2.
  • Thecorrugations, parallel to the flow direction space apart the plates 2. or hand the corrugated metal plates 1, so that the gas passage ducts are formed between them.
  • the plates are placed alternately on each other. Only a portion of a whole pack is shown in the FIG.
  • the major walls of 1 these have, however, generally square-shaped flatridges and furrows which are protuberances 3 pressed alternately from opposite sides into the spacing elements 1 at distances b 10- 151,, and having in each case a transverse width of 0.8- 1.0 b.
  • approximately square protuberances 3 of the wider wall parts form within the gasflow ducts between the heating elements-1 and 2 alternately quite considerable cross-sectional constrictions and correspondingly big expansions, because their protuberance depth-h amounts to approximately 0.3 to 0.7 r,,.
  • a regenerative heat exchanger element pack formed of alternately assembled metal plates and spacing plates, which spacing plates are provided at intervals with deep corrugations, running parallel to the flow direction of gases through the pack and delimiting gas passage ducts between the plates
  • the improvement comprising in the flow cross sections of these small gas passage ducts having a small hydraulic radius r,, and a generally rectangular cross section with major and minor walls, the major delimitation walls of which having at equal distances behind each other in the flow direction flat protuberances of a generally square shape and of a height h, which are alternately arranged and directed opposite to each other in such a way, that they alternately constrict the flow cross section of the gas passage ducts, whereby this protuberance height h amounts to 0.30.7 r,,.
  • a metal spacing plate having a mean plane, parallel spaced-apart corrugations passing through that plane, and, between the conugations, protuberances projecting out of the mean plane, adjacent protuberances in directions parallel to the corrugations projecting out of the said plane in opposite directions to an equal height, the said adjacent protuberances being llat surfaced and having a length equal to their width in a direction perpendicular to the direction of the corrugations.
  • a metal spacing plate according to claim 5 wherein the said adjacent protuberances are spaced apart, in a direction parallel to the corrugations, by a distance approximately equal to their length.

Abstract

A corrugated plate for use in the regenerative mass of a rotary regenerative heat exchanger has also alternating, approximately square-shaped, flat-topped protuberances between the corrugations so that the gas passage formed between it and an adjacent plate of the pack and defined laterally by the corrugations is alternately and regularly constricted and expanded.

Description

United States Patent [72] Inventor Gerhard Kritzler Freudenberg, Germany [21 Appl. No. 854,854
[22] Filed Sept. 3, 1969 [45] Patented Jan. 12, 1971 [73] Assignee Apparatebau Rothemuhle Brandt &
Kritzler Westphalia, Germany a company of Germany [32] Priority Sept. 7, 1968 I 33] Germany [54] ELEMENTS FOR REGENERATIVE HEAT EXCHANGERS 6 Claims, 1 Drawing Fig.
[52] US. Cl 165/10, 165/ 166 [51] Int. Cl. F28d 19/00 WWI/l wyygew [50] Field of Search 165/ 10, 151, I66
[56] References Cited UNITED STATES PATENTS 2,696,976 12/1954 Boestad et al. 165/10 2,940,736 6/1960 Odman 165/166 3,151,675 10/1964 Lysholm 165/166 Primary Examiner-Albert W. Davis, Jr. AttorneyLackenbach & Lackenbach ABSTRACT: A corrugated plate for use in the regenerative mass of a rotary regenerative heat exchanger has also alternating, approximately square-shaped, flat-topped protuberances between the corrugations so that the gas passage formed between it and an adjacent plate of the pack and defined laterally by the corrugations is alternately and regularly constricted and expanded.
I I I I PATENTEU JAN 12 I971 I 8; 554,273
--- #if a Ill INVENTOR GERHARD KRITZLER BWW ATTORNEYS BACKGROUND OF THE INVENTION and of forming narrow channels parallel to the axial direction of the regenerator, through which the heat-exchanging media periodicallypass, alternating in counterflow, whilst the protuberances between the corrugations-in the walls of thenarrow gas passage ducts which are formed between the adjoining metal plates, are intended to create morefavorable flow conditions for the heat exchange.
It is known in the artthat IfOl' fulfillment of these requirements the metal platesmustbepacked as densely as possible, so that the gas passage ducts, which are formed between the alternatingly adjoining metal plates have the smallestpossible hydraulic radii, which are-normally chosen of a size ranging between 3to mm, in the range of gasvelocities of 5-15 meters/second, which areusually used, such small hydraulic radii create a laminarflow, with a heat transfer which is substantiallylowerthan thatof-aturbulent flow. The shaping of the gas passage ducts and: consequently the design of the protuberances in the plates themselves has therefore-a chief aim of influencingthe flow in such a way that this results in heat transfer coeff cients which will bev approximately the same as those ofturbulent tlow. r
Forthis purpose it has already been attempted to increase the extent of the heat transfer between the flowing gases and the metal plates by designingthe walls of the narrow gas passage ducts irregularlyandintermittently, wherebyan increased vortex shedding'within the flow. is obtained.
Experience has shown, however, that stronger and irregular vortexsheddings of this ,type cannot increase the heat transfer proportionallyto the increased loss in pressureduring passage ofthe flow. through a pack of such'm'etal heating elements.
One example of 1 what has, therefore, been normal practice to usein metal heating element-packsfor regenerative heat lic radius of approximately 3.5 mm.
SUMMARY OF THE INVENTION The present'invention has the object of improving the heat transfer in the narrow flow ducts between the metal heating elements, with the packing density remaining unchanged, by creation of periodically repeated delays and accelerations of the flow, which areco'nnected withan increased turbulence.
According to the present, invention this object is fulfilled in that the spacing metal heating element'shape between the planar 0r shallowly undulated plates is provided at specified distances with deep corrugations, which run parallel to the direction of flow of media through the pack and delimit the small gas passage ducts between the metal plates, which form with a specified hydraulic radius sihalL'rectangular flow cross sections for the gases, the'broader delimitation walls of which have at intervals in the flow direction laminar protuberances,
mainly of a square shape, which-are alternately arranged and directed opposite to each other in such away, that they constrict theflow cross, sections at one position into a small gap protuberance height, and this protuberance height amounting to approximately 50 percent of the distance of the plates from each other.
For further development of the invention the distance apart of the deep corrugations shall amount to 10-20 times the size of the hydraulic radius of the small flow passages between the metal plates, whilst the length along the direction of tlow of the laminar protuberances between these corrugations shall amount to 10-15 times the size of this hydraulic radius.
DESCRIPTION OF A PARTICULAR EMBODIMENT One part of an example of the invention is shown schematically in the drawing, which is a perspective, partly cutaway view.
It shows part of a metal element 1 with one wave of anapproximately sinusoidal corrugation each of an amplitudec/Z 1.0 to 1.2 r,,, of a wave length of l to 6.3 r,, and parallel to each other at distances of a 10-20 r where r, is the hydraulic radius of gas passage ducts which are formed by the corrugations. The plates 1 are made up into packs with shallowly undulated plates '2 or plane plates 2a alternately with the plates 1. The packs are placed in a regenerator chamber so that the corrugations are along the axial direction, and gas flow takes place in the directions of the arrows F1 and F2. Thecorrugations, parallel to the flow direction, space apart the plates 2. or hand the corrugated metal plates 1, so that the gas passage ducts are formed between them. The plates are placed alternately on each other. Only a portion of a whole pack is shown in the FIG.
Between the corrugations, therefore, there are generally rectangular section gas passage ducts. The major walls of 1 these have, however, generally square-shaped flatridges and furrows which are protuberances 3 pressed alternately from opposite sides into the spacing elements 1 at distances b 10- 151,, and having in each case a transverse width of 0.8- 1.0 b.
In the perspective illustration of the metal heating element 1 a cutaway portion of one of the metal plates 2 with shallow undulations has been shown on the top left-hand comer and also a next succeeding spacing element la. The undulations of these metal plates 2 which are alternately arranged between the-metalplates l have an amplitude height of 0.4 n, and an undulation length (wavelength) of approximately'5 r,,.
Compared with these rather weakly undulated intermediate plates Zthe ridges of the luminar, approximately square protuberances 3 of the wider wall parts form within the gasflow ducts between the heating elements-1 and 2 alternately quite considerable cross-sectional constrictions and correspondingly big expansions, because their protuberance depth-h amounts to approximately 0.3 to 0.7 r,,.
By means of a metal heating element pack,.whichis formed in c this way with alternately assembled plane or eundulated metal. plates 2 or 2a and themetal heating velements11;..with deep spacing corrugations, running parallel ,to the flow direction, periodically repeated delays .and accelerationsv of the flow are obtained within the flow ducts. between. the metal plates because of the considerable crossrsectional. constrictions and the cross-sectionalexpansion being alternatelyprovided thereto, which are due to the approximately la fand a p'roturberance depth h, said delays and accelerations increasing theturbulence'to such an extent that compared 1 to.= the previously conventional metal heating element pack,- for-.example according to the German Utility Model 1-,903,543,with parallel ducts and triangular flow cross sections, aconsiderable increase of the heat transfer coefficient is obtained in line with a simultaneous lowering of the pressure losses.
The proportional increase of the heat transfer FIGS.
amounts in the velocity range of the gas flow from "El- 6 meters/second to approximately 20 percent whilst the 1 pressure losses, compared to those of the previously used metal heating element packs, are about 40 percent lower, if flow-velocities of up to 6 meters per second are concerned.
and at anotherinto a larger-gap, the gapsdiffering by an equal I claim:
1. In a regenerative heat exchanger element pack formed of alternately assembled metal plates and spacing plates, which spacing plates are provided at intervals with deep corrugations, running parallel to the flow direction of gases through the pack and delimiting gas passage ducts between the plates, the improvement comprising in the flow cross sections of these small gas passage ducts having a small hydraulic radius r,, and a generally rectangular cross section with major and minor walls, the major delimitation walls of which having at equal distances behind each other in the flow direction flat protuberances of a generally square shape and of a height h, which are alternately arranged and directed opposite to each other in such a way, that they alternately constrict the flow cross section of the gas passage ducts, whereby this protuberance height h amounts to 0.30.7 r,,.
2. The improvement according to claim 1, being thereby characterized that one approximately sinusoidal corrugation each of an amplitude height of /2 1.0-1.2 r,, is provided at parallel distances of a -20 r, in the spacing plates and parallel to flow direction.
3. The improvement according to claim 2 being thereby characterized, that the approximately sinusoidal corrugation has an undulation length of l to 6.3 r,,
4. The improvement according to claim 1 being thereby characterized that the approximately square protuberances are indented behind each other in flow direction at distances of b l0- l 5 r with an area size of approximately I)".
5. In a regenerative heat exchanger element pack, a metal spacing plate having a mean plane, parallel spaced-apart corrugations passing through that plane, and, between the conugations, protuberances projecting out of the mean plane, adjacent protuberances in directions parallel to the corrugations projecting out of the said plane in opposite directions to an equal height, the said adjacent protuberances being llat surfaced and having a length equal to their width in a direction perpendicular to the direction of the corrugations.
6. A metal spacing plate according to claim 5 wherein the said adjacent protuberances are spaced apart, in a direction parallel to the corrugations, by a distance approximately equal to their length.

Claims (6)

1. In a regenerative heat exchanger element pack formed of alternately assembled metal plates and spacing plates, which spacing plates are provided at intervals with deep corrugations, running parallel to the flow direction of gases through the pack and delimiting gas passage ducts between the plates, the improvement comprising in the flow cross sections of these small gas passage ducts having a small hydraulic radius rh and a generally rectangular cross section with major and minor walls, the major delimitation walls of which having at equal distances behind each other in the flow direction flat protuberances of a generally square shape and of a height h, which are alternately arranged and directed opposite to each other in such a way, that they alternately constrict the flow cross section of the gas passage ducts, whereby this protuberance height h amounts to 0.30.7 rh.
2. The improvement according to claim 1, being thereby characterized that one approximately sinusoidal corrugation each of an amplitude height of c/2 1.0- 1.2 rh is provided at parallel distances of a 10- 20 rh in the spacing plates and parallel to flow direction.
3. The improvement according to claim 2 being thereby characterized, that the approximately sinusoidal corrugation has an undulation length of 1 to 6.3 rh
4. The improvement according to claim 1 being thereby characterized that the approximately square protuberances are indented behind each other in flow direction at distances of b 10- 15 rh, with an area size of approximately b2.
5. In a regenerative heat exchanger element pack, a metal spacing plate having a mean plane, parallel spaced-apart corrugations passing through that plane, and, between the corrugations, protuberances projecting out of the mean plane, adjacent protuberances in directions parallel to the corrugations projecting out of the said plane in opposite directions to an equal height, the said adjacent protuberances being flat surfaced and having a length equal to their width in a direction perpendicular to the direction of the corrugations.
6. A metal spacing plate according to claim 5 wherein the said adjacent protuberances are spaced apart, in a direction parallel to the corrugations, by a distance approximately equal to their length.
US854854A 1968-09-07 1969-09-03 Elements for regenerative heat exchangers Expired - Lifetime US3554273A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE6751210U DE6751210U (en) 1968-09-07 1968-09-07 HEATING PLATES FOR REGENERATIVE HEAT EXCHANGERS

Publications (1)

Publication Number Publication Date
US3554273A true US3554273A (en) 1971-01-12

Family

ID=6591929

Family Applications (1)

Application Number Title Priority Date Filing Date
US854854A Expired - Lifetime US3554273A (en) 1968-09-07 1969-09-03 Elements for regenerative heat exchangers

Country Status (2)

Country Link
US (1) US3554273A (en)
DE (1) DE6751210U (en)

Cited By (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4125149A (en) * 1976-04-15 1978-11-14 Apparatebau Rothemuhle Brandt & Kritzler Heat exchange elements
US4291759A (en) * 1979-08-28 1981-09-29 Hisaka Works, Limited Cross-current type plate heat exchanger
EP0424677A1 (en) * 1989-10-25 1991-05-02 Abb Air Preheater, Inc. Heat transfer element assembly
US5836379A (en) * 1996-11-22 1998-11-17 Abb Air Preheater, Inc. Air preheater heat transfer surface
US5899261A (en) * 1997-09-15 1999-05-04 Abb Air Preheater, Inc. Air preheater heat transfer surface
US6019160A (en) * 1998-12-16 2000-02-01 Abb Air Preheater, Inc. Heat transfer element assembly
US6470878B1 (en) 2000-10-23 2002-10-29 Carrier Corporation Furnace heat exchanger
US6484798B1 (en) 2000-10-23 2002-11-26 Carrier Corporation Furnace heat exchanger
US20030024697A1 (en) * 2001-08-06 2003-02-06 Toyoaki Matsuzaki Heat transfer member and method for manufacturing same
US6516871B1 (en) * 1999-08-18 2003-02-11 Alstom (Switzerland) Ltd. Heat transfer element assembly
US6793015B1 (en) 2000-10-23 2004-09-21 Carrier Corporation Furnace heat exchanger
US6892795B1 (en) * 2000-10-04 2005-05-17 Airxchange, Inc. Embossed regenerator matrix for heat exchanger
US7096933B1 (en) 2000-10-24 2006-08-29 Carrier Corporation Furnace heat exchanger
US9683474B2 (en) 2013-08-30 2017-06-20 Dürr Systems Inc. Block channel geometries and arrangements of thermal oxidizers

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2696976A (en) * 1949-06-22 1954-12-14 Jarvis C Marble Element set for air preheaters
US2940736A (en) * 1949-05-25 1960-06-14 Svenska Rotor Maskiner Ab Element set for heat exchangers
US3151675A (en) * 1957-04-02 1964-10-06 Lysholm Alf Plate type heat exchanger

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2940736A (en) * 1949-05-25 1960-06-14 Svenska Rotor Maskiner Ab Element set for heat exchangers
US2696976A (en) * 1949-06-22 1954-12-14 Jarvis C Marble Element set for air preheaters
US3151675A (en) * 1957-04-02 1964-10-06 Lysholm Alf Plate type heat exchanger

Cited By (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4125149A (en) * 1976-04-15 1978-11-14 Apparatebau Rothemuhle Brandt & Kritzler Heat exchange elements
US4291759A (en) * 1979-08-28 1981-09-29 Hisaka Works, Limited Cross-current type plate heat exchanger
EP0424677A1 (en) * 1989-10-25 1991-05-02 Abb Air Preheater, Inc. Heat transfer element assembly
US5836379A (en) * 1996-11-22 1998-11-17 Abb Air Preheater, Inc. Air preheater heat transfer surface
US5899261A (en) * 1997-09-15 1999-05-04 Abb Air Preheater, Inc. Air preheater heat transfer surface
US6019160A (en) * 1998-12-16 2000-02-01 Abb Air Preheater, Inc. Heat transfer element assembly
US6516871B1 (en) * 1999-08-18 2003-02-11 Alstom (Switzerland) Ltd. Heat transfer element assembly
US6892795B1 (en) * 2000-10-04 2005-05-17 Airxchange, Inc. Embossed regenerator matrix for heat exchanger
US6484798B1 (en) 2000-10-23 2002-11-26 Carrier Corporation Furnace heat exchanger
US6793015B1 (en) 2000-10-23 2004-09-21 Carrier Corporation Furnace heat exchanger
US6470878B1 (en) 2000-10-23 2002-10-29 Carrier Corporation Furnace heat exchanger
US7096933B1 (en) 2000-10-24 2006-08-29 Carrier Corporation Furnace heat exchanger
US20030024697A1 (en) * 2001-08-06 2003-02-06 Toyoaki Matsuzaki Heat transfer member and method for manufacturing same
US20050092054A1 (en) * 2001-08-06 2005-05-05 Xenesys Inc. Heat transfer member and method for manufacturing same
US20050150644A1 (en) * 2001-08-06 2005-07-14 Xenesys, Inc. Heat transfer member and method for manufacturing same
US7069982B2 (en) 2001-08-06 2006-07-04 Xenesys, Inc. Heat transfer member and method for manufacturing same
US9683474B2 (en) 2013-08-30 2017-06-20 Dürr Systems Inc. Block channel geometries and arrangements of thermal oxidizers
US10337378B2 (en) 2013-08-30 2019-07-02 Dürr Systems Inc. Block channel geometries and arrangements of thermal oxidizers

Also Published As

Publication number Publication date
DE6751210U (en) 1969-01-30

Similar Documents

Publication Publication Date Title
US3554273A (en) Elements for regenerative heat exchangers
US4002200A (en) Extended fin heat exchanger panel
EP0272266B1 (en) Plate heat exchanger
JPS5928225Y2 (en) Plate heat exchanger
US3759323A (en) C-flow stacked plate heat exchanger
US3810509A (en) Cross flow heat exchanger
US4449573A (en) Regenerative heat exchangers
GB1238491A (en)
KR850008713A (en) heat transmitter
US4307779A (en) Plate heat exchanger
US3495656A (en) Plate-type heat exchanger
SE7900410L (en) PLATTVERMEVEXLARE
GB1153403A (en) Plate Type Heat Exchangers.
US2587116A (en) Heat exchanging device
GB2071304A (en) Finned-tube heat exchanger
US4470453A (en) Primary surface for compact heat exchangers
US4470454A (en) Primary surface for compact heat exchangers
ES8301010A1 (en) Plate floor heat exchanger
US4407357A (en) Thin sheet metal heat exchanger
US3244227A (en) Plate type heat exchangers
US3669186A (en) Distributor for plate type heat exchangers having end headers
US2620169A (en) Plate type heat exchanger
US4330035A (en) Heat exchanger
CA1069883A (en) Compact primary surface heat exchanger
GB1471944A (en) Heat exchangers