Nothing Special   »   [go: up one dir, main page]

US3369593A - Axial flow regenerative heat exchangers - Google Patents

Axial flow regenerative heat exchangers Download PDF

Info

Publication number
US3369593A
US3369593A US492789A US49278965A US3369593A US 3369593 A US3369593 A US 3369593A US 492789 A US492789 A US 492789A US 49278965 A US49278965 A US 49278965A US 3369593 A US3369593 A US 3369593A
Authority
US
United States
Prior art keywords
regenerator
annular
regenerative heat
portions
axial flow
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
US492789A
Inventor
Brandt Herbert
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.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Application granted granted Critical
Publication of US3369593A publication Critical patent/US3369593A/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
    • 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

Definitions

  • This invention relates to rotary regenerative heat exchangers of the kind which includes, inter alia, a substantially cylindrical heat exchange member, referred to hereinafter as a regenerator, which comprises a casing containing a mass of plates or tubes, hereinafter referred to, for convenience, as plates, which provide passages through the regenerator, hot gas being led through the said passages in one direction, substantially parallel to the axis of the regenerator, in order to give up its heat to the said mass, whereafter air is led through the same passages in the opposite axial direction in order to pick up the heat from the said mass.
  • a regenerator which comprises a casing containing a mass of plates or tubes, hereinafter referred to, for convenience, as plates, which provide passages through the regenerator, hot gas being led through the said passages in one direction, substantially parallel to the axis of the regenerator, in order to give up its heat to the said mass, whereafter air is led through the same passages in the opposite axial direction in order to pick up the heat from the said
  • the regenerator rotates about its axis, while the means for supplying said air and hot gas to the regenerator, and for leading the cooled gas and heated air from the regenerator are stationary; in other cases the regenerator is stationary while the said air conducting means rotate about the projected axis of the regenerator.
  • the mass of plates in the regenerator acquire a higher temperature at the axial end (which will be referred to as the hot end) of the regenerator to which the hot gases are supplied and from which the heated air is withdrawn, than at the opposite axial end (which will be referred to as the cold end) of the regenerator from which the cooled gas is withdrawn and the cold air enters.
  • These temperatures differences in the regenerator cause deformation of and stresses in the mass of plates and the regenerator casing which have had to be allowed for, in the design of the heat exchanger, by expensive construction measures.
  • With the present tendency for rotary regenerative heat exchangers to increase in size considerably some regenerators have a diameter of approximately 12 meters, and an axial height of approximately 2 meters), the stresses therein become very considerable.
  • the regenerator tends to assume the form of a calotte, with a concave surface at the cold end and a convex surface at the hot end.
  • the object of the present invention is to provide improvements in regenerators of rotary regenerative heat 3,369,593 Patented Feb. 20, 1968 exchangers whereby to minimise the deformation effects of the differential temperatures of cold and hot ends thereof.
  • a substantially cylindrical regenerator of a rotary regenerative heat exchanger is characterised in that it is formed of a plurality of annular portions which are concentric with each other and are spaced apart radially to provide an annular gap therebetween.
  • FIG. 1 is a diagrammatic sectional elevation of a rotary regenerative heat exchanger
  • FIGS. 2 and 3 are diagrammatic sectional elevations of a regenerator which has been subjected to the differential temperatures
  • FIG. 4 is a diagrammatic sectional elevation of a rotary regenerative heat exchanger embodying a regenerator according to this invention
  • FIG. 5 is a diagrammatic end view of the regenerator included in the heat exchanger shown in F164, looking along the axis thereof;
  • FIG. 6 is a diagrammatic sectional elevation illustrating, in an exaggerated manner, the deformation of the regenerator shown in FIG. 4.
  • FIG. 7 is a fragmentary enlarged diagrammatic sectional elevation of part of FIG. 4.
  • FIG. 8 is a fragmentary plan view corresponding to FIG. 7.
  • a cylindrical regenerator 11 contains a mass 12 of heat exchange plates. Hot gas is supplied to the hot end 13 of the regenerator, in the direction of the arrow 14, through a duct 15, and the gas, after being cooled by transfer of its heat to the mass 12 of plates, leaves the cold end 16 of the regenerator and is led away through a duct 17.
  • Cold air is supplied to the cold end 16 of the regenerator, in the direction of the arrow 18, through a duct 19, and the air, after being heated by transfer of heat from the mass 12, leaves the hot end 13 of the regenerator and is led away through a duct 20.
  • the regenerator 11 may rotate around its axis 21, while the ducts 15, 17, 19 and 20 remain stationary, or the regenerator 11 and the gas ducts 15 and 17 may be stationary while the air ducts 19 and 20 rotate about the projected axis 21. In either event there is relative rotation between the regenerator 11 and the air ducts 19 and 20.
  • the regenerator is made, according to the present invention, in the form shown, by way of example, in FIGS. 4 and 5.
  • the regenerator is constructed of a plurality of separate concentric annular portions. In FIGS. 4 and 5, two annular regenerator portions 22 and 23 are shown, but there may be three or more such annular concentric regenerator portions.
  • annular regenerator portion 22 is surrounded by an outer annular portion 23, the two portions being separated from each other, but connected to each other, so that the two portions are supported relatively to each other, by connecting means 24. Consequently, the two annular portions 22 and 23 will expand and deform independently of each other; they may each assume a substantially calotte formation, and such deformation may assume the form shown, in exaggerated manner, in FIG. 6.
  • the concave cold end surface 16 of the regenerator is broken up (compared with the form shown in FIG. 3) into several separate concave surfaces each of which is of less depth (axially of the regenerator) than the depth of the concave cold end surface shown in FIG. 3; the convex hot end surface 13 of the regenerator similarly is broken up into several separate convex surface portions.
  • FIGS. 7 and 8 are an enlarged fragmentary sectional elevation and plan respectively.
  • a bracket 27 on the inner face of the outer annular portion 23 is engaged by another bracket 28 on the outer face of the inner annular portion 22, and bolts 29 pass through the two brackets.
  • An axial flow regenerator for a rotary regenerative heat exchanger which comprises a plurality of annular regenerator portions concentric with each other and carrying a heat storage mass and means for interconnecting said annular portions so that each portion is'supported relative to each other portion and so that an annular gap between adjacent annular portions is provided and each annular portion is freely adjustable independently of each other annular portion,

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)
  • Turbine Rotor Nozzle Sealing (AREA)

Description

Feb, 20, 1968 H. BRANDT 3,369,593
AXIAL FLOW REGENERATIVE HEAT EXCHANGERS Filed Oct. 4, 1965 5 Sheets-Sheet l T 1'5- 1 I]; J
H. BRANDT AXIAL FLOW REGENERATIVE HEAT EXCHANGERS Feb. 20, 1968 3 Sheets-Sheet 5 Filed Oct. 4, 1965 United States Patent 3 Claims. Cl. 165-40) ABSTRACT OF THE DISCLOSURE The deformation of and stresses in the mass of plates in rotary regenerative heat exchangers as a result of the temperature differences-of the hot and cold ends can be minimized by constructing the regenerator portion as an axial flow structure which comprises a plurality of annular portions concentric with each other together with means for interconnecting the annular portions in such a way that each portion is supported relative to each other portion and in such a way as to provide an annular gap between adjacent portions and free adjustability of each annular portion independently of each other annular portion.
This invention relates to rotary regenerative heat exchangers of the kind which includes, inter alia, a substantially cylindrical heat exchange member, referred to hereinafter as a regenerator, which comprises a casing containing a mass of plates or tubes, hereinafter referred to, for convenience, as plates, which provide passages through the regenerator, hot gas being led through the said passages in one direction, substantially parallel to the axis of the regenerator, in order to give up its heat to the said mass, whereafter air is led through the same passages in the opposite axial direction in order to pick up the heat from the said mass. In some cases the regenerator rotates about its axis, while the means for supplying said air and hot gas to the regenerator, and for leading the cooled gas and heated air from the regenerator are stationary; in other cases the regenerator is stationary while the said air conducting means rotate about the projected axis of the regenerator.
The mass of plates in the regenerator acquire a higher temperature at the axial end (which will be referred to as the hot end) of the regenerator to which the hot gases are supplied and from which the heated air is withdrawn, than at the opposite axial end (which will be referred to as the cold end) of the regenerator from which the cooled gas is withdrawn and the cold air enters. These temperatures differences in the regenerator cause deformation of and stresses in the mass of plates and the regenerator casing which have had to be allowed for, in the design of the heat exchanger, by expensive construction measures. With the present tendency for rotary regenerative heat exchangers to increase in size considerably (some regenerators have a diameter of approximately 12 meters, and an axial height of approximately 2 meters), the stresses therein become very considerable.
In consequence of such tendency of the regenerator parts to deform, and of restoring forces applied thereto, the regenerator tends to assume the form of a calotte, with a concave surface at the cold end and a convex surface at the hot end.
Consequently, the means for sealing the adjacent, relatively rotating, end surfaces of the regenerator and of the air conducting means, to prevent undue leakage of gas and air therebetween, become very complicated in design and construction. 1
The object of the present invention is to provide improvements in regenerators of rotary regenerative heat 3,369,593 Patented Feb. 20, 1968 exchangers whereby to minimise the deformation effects of the differential temperatures of cold and hot ends thereof.
According to this invention, a substantially cylindrical regenerator of a rotary regenerative heat exchanger is characterised in that it is formed of a plurality of annular portions which are concentric with each other and are spaced apart radially to provide an annular gap therebetween.
Referring to the accompanying drawings:
FIG. 1 is a diagrammatic sectional elevation of a rotary regenerative heat exchanger;
FIGS. 2 and 3 are diagrammatic sectional elevations of a regenerator which has been subjected to the differential temperatures;
FIG. 4 is a diagrammatic sectional elevation of a rotary regenerative heat exchanger embodying a regenerator according to this invention;
FIG. 5 is a diagrammatic end view of the regenerator included in the heat exchanger shown in F164, looking along the axis thereof;
FIG. 6 is a diagrammatic sectional elevation illustrating, in an exaggerated manner, the deformation of the regenerator shown in FIG. 4.
FIG. 7 is a fragmentary enlarged diagrammatic sectional elevation of part of FIG. 4; and
FIG. 8 is a fragmentary plan view corresponding to FIG. 7.
Referring to FIG. 1, which shows a known form of rotary regenerative heat exchanger, a cylindrical regenerator 11 contains a mass 12 of heat exchange plates. Hot gas is supplied to the hot end 13 of the regenerator, in the direction of the arrow 14, through a duct 15, and the gas, after being cooled by transfer of its heat to the mass 12 of plates, leaves the cold end 16 of the regenerator and is led away through a duct 17.
Cold air is supplied to the cold end 16 of the regenerator, in the direction of the arrow 18, through a duct 19, and the air, after being heated by transfer of heat from the mass 12, leaves the hot end 13 of the regenerator and is led away through a duct 20.
The regenerator 11 may rotate around its axis 21, while the ducts 15, 17, 19 and 20 remain stationary, or the regenerator 11 and the gas ducts 15 and 17 may be stationary while the air ducts 19 and 20 rotate about the projected axis 21. In either event there is relative rotation between the regenerator 11 and the air ducts 19 and 20.
Due to different temperatures at the hot end 13 and the cold end 16 of the regenerator, there is greater expansion at the hot end 13 than at the cold end 16. If such expansion were not impeded (by thecasing and other constructional elements of the heat exchanger), the regenerator would tend to take up the form shown, in an exaggerated manner, in FIG. 2. However, due to restoring forces which operate upon the regenerator, t-he regenerator cannot assume the form shown in FIG. 2, and therefore assumes the form of a calotte, shown in exaggerated form in FIG. 3.
In order to minimise the deformation of the regenerator 11 to the form shown in FIG. 3, the regenerator is made, according to the present invention, in the form shown, by way of example, in FIGS. 4 and 5. The regenerator is constructed of a plurality of separate concentric annular portions. In FIGS. 4 and 5, two annular regenerator portions 22 and 23 are shown, but there may be three or more such annular concentric regenerator portions.
In FIGS. 4 and 5, an inner annular regenerator portion 22 is surrounded by an outer annular portion 23, the two portions being separated from each other, but connected to each other, so that the two portions are supported relatively to each other, by connecting means 24. Consequently, the two annular portions 22 and 23 will expand and deform independently of each other; they may each assume a substantially calotte formation, and such deformation may assume the form shown, in exaggerated manner, in FIG. 6.
In FIG. 6 it will be seen that the concave cold end surface 16 of the regenerator is broken up (compared with the form shown in FIG. 3) into several separate concave surfaces each of which is of less depth (axially of the regenerator) than the depth of the concave cold end surface shown in FIG. 3; the convex hot end surface 13 of the regenerator similarly is broken up into several separate convex surface portions.
The effect of this arrangement of the regenerator is that the sealing means (shown diagrammatically at 25 and 26) between the regenerator and the air ducts, and between the regenerator and the surrounding casing of the heat exchanger, can more efiiciently minimise any leakage of gas or air.
The connecting means 24 between the annular concentric regenerator portions 22 and 23 are shown in FIGS. 7 and 8 which are an enlarged fragmentary sectional elevation and plan respectively. A bracket 27 on the inner face of the outer annular portion 23 is engaged by another bracket 28 on the outer face of the inner annular portion 22, and bolts 29 pass through the two brackets. There are four sets of interengaging brackets 27 and 28 disposed in the annular gap 30 between the concentric annular portions 22 and 23, at intervals of 90 degrees; however, there may be any number, more than two, of such sets, spaced around the regenerator at suitable angular intervals. Thereby, the outer annular portion 23 of the regenerator, which portion is itself supported on fixed structures 31 (FIG. 4) of the heat exchanger, in turn supports the inner annular portion 22. Such an arrangement is sufficient if the regenerator is stationary. If the regenerator rotates, then horizontally disposed bolts may have to be disposed between the brackets 22 and 23 (which will then have to be provided with vertical lugs to receive the bolts) to providedrag means so that a rotary drive applied to one of the annular regenerator portions is transmitted to the other portion; alternatively, interengaging claw devices may be provided between the two annular portions of the regenerator so that a rotary drive may be transmitted from 4. one portion to the other. Except at such interengaging connecting means 24, the two annular regenerator portions 22 and 23 may move independently of each other.
At suitable angular intervals around the annular gap 30 there are disposed vertical ribs 32 extending inwardly, parallel to the axis, of the regenerator, from the regenerator portion 23 into channels 33, also parallel to the axis of the regenerator, secured to the portion 22 to provide substantial seals against the circumferential flow of gas or air in the gap.
What I claim and desire to secure by Letters Patent is:
1. An axial flow regenerator for a rotary regenerative heat exchanger which comprises a plurality of annular regenerator portions concentric with each other and carrying a heat storage mass and means for interconnecting said annular portions so that each portion is'supported relative to each other portion and so that an annular gap between adjacent annular portions is provided and each annular portion is freely adjustable independently of each other annular portion,
2. An axial flow regenerator according to claim 1 wherein said interconnecting means is disposed in the gap between each separate concentric annular portion and comprises brackets attached at one face to their respective annular portions and attached at their common face, by
means which secure the adjacent annular portions in a supporting manner to one another and allow each annular portion to move independently of each other annular portion.
3. An axial flow regenerator according to claim 1 wherein said interconnecting means overlap one another to prevent circumferential flow of fluid in said gap.
References Cited UNITED STATES PATENTS I 2,432,198 12/1947 Karlsson et al 0 -40 2,503,651 4/1950 Alcock 1658 2,944,798 7/1960 Muller 165-10 3,216,486 11/1965 Hall et al. 1658 3,301,316 1/1967 Mason 16510 X ROBERT A. OLEARY, Primary Examiner.
A. W. DAVIS, JR., Assistant Examiner.
US492789A 1964-10-03 1965-10-04 Axial flow regenerative heat exchangers Expired - Lifetime US3369593A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DEA47246A DE1237150B (en) 1964-10-03 1964-10-03 Support structure for the heat storage of rotating regenerative heat exchangers through which the media flows axially in countercurrent

Publications (1)

Publication Number Publication Date
US3369593A true US3369593A (en) 1968-02-20

Family

ID=6935692

Family Applications (1)

Application Number Title Priority Date Filing Date
US492789A Expired - Lifetime US3369593A (en) 1964-10-03 1965-10-04 Axial flow regenerative heat exchangers

Country Status (3)

Country Link
US (1) US3369593A (en)
DE (1) DE1237150B (en)
GB (1) GB1108644A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3710850A (en) * 1971-08-04 1973-01-16 Air Preheater Unrestrained rotor
US3710851A (en) * 1971-08-19 1973-01-16 Air Preheater Ball-and-socket coupling for rotor
US6264464B1 (en) 2000-05-12 2001-07-24 Megtec Systems, Inc. Angled bed for regenerative heat exchanger

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2432198A (en) * 1945-01-12 1947-12-09 Air Preheater Heat exchange surface for air preheaters
US2503651A (en) * 1946-12-05 1950-04-11 Harry Ralph Ricardo Heat exchanger
US2944798A (en) * 1955-06-22 1960-07-12 Air Preheater Guide plates for rotary regenerator
US3216486A (en) * 1963-09-19 1965-11-09 Air Preheater Rotary heat exchanger
US3301316A (en) * 1964-08-24 1967-01-31 Gen Motors Corp Regenerator matrix

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE818960C (en) * 1949-02-15 1951-10-29 Andrew Thomson Bowden Circulating regenerative heat exchanger
DE1118389B (en) * 1954-12-30 1961-11-30 Svenska Rotor Maskiner Ab Air preheater / feed water preheater arrangement in steam generator systems
DE1117813B (en) * 1960-07-28 1961-11-23 Babcock & Wilcox Dampfkessel Regenerative air preheater with relief slots in the rotor

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2432198A (en) * 1945-01-12 1947-12-09 Air Preheater Heat exchange surface for air preheaters
US2503651A (en) * 1946-12-05 1950-04-11 Harry Ralph Ricardo Heat exchanger
US2944798A (en) * 1955-06-22 1960-07-12 Air Preheater Guide plates for rotary regenerator
US3216486A (en) * 1963-09-19 1965-11-09 Air Preheater Rotary heat exchanger
US3301316A (en) * 1964-08-24 1967-01-31 Gen Motors Corp Regenerator matrix

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3710850A (en) * 1971-08-04 1973-01-16 Air Preheater Unrestrained rotor
US3710851A (en) * 1971-08-19 1973-01-16 Air Preheater Ball-and-socket coupling for rotor
US6264464B1 (en) 2000-05-12 2001-07-24 Megtec Systems, Inc. Angled bed for regenerative heat exchanger

Also Published As

Publication number Publication date
DE1237150B (en) 1967-03-23
GB1108644A (en) 1968-04-03

Similar Documents

Publication Publication Date Title
US3490521A (en) Tube and shell heat exchanger
US3301317A (en) Thermal regenerators
US2287777A (en) Regenerative heat exchanger
US2055071A (en) Sealing means for heat exchangers
US4310046A (en) Regenerative heat exchanger
KR800000074Y1 (en) Unrestrained rotor
US3372735A (en) Rotary heat-exchangers and hot-gas engines
US3369593A (en) Axial flow regenerative heat exchangers
US3830287A (en) Rotor structure
US3710851A (en) Ball-and-socket coupling for rotor
US3191666A (en) Regenerative fluid heater
US3276515A (en) Gas turbine regenerator
US3216488A (en) Rotary regenerative heat exchange apparatus
US2229691A (en) Regenerative heat exchanger
US3155152A (en) Rotor structure for rotary regenerative heat exchanger
US4316499A (en) Rotary, regenerative heat exchanger having floating sealing rings
US3058723A (en) Regenerative heat exchangers
US2732184A (en) Pivotally supported housing for rotary regenerators
US2615685A (en) Regenerative heat exchanger
US4040475A (en) Axially movable sector plate support for rotary regenerative heat exchanger
US2892615A (en) Heat exchangers of the rotary regenerator type
US3990503A (en) Regenerative heat exchanger
US3572425A (en) Rotary regenerative heat exchangers
US3446279A (en) Air-cooled radiation recuperator
US3229753A (en) Regenerative heat exchangers