[go: up one dir, main page]

US2873952A - Rotary regenerative heat exchangers for gaseous media - Google Patents

Rotary regenerative heat exchangers for gaseous media Download PDF

Info

Publication number
US2873952A
US2873952A US422918A US42291854A US2873952A US 2873952 A US2873952 A US 2873952A US 422918 A US422918 A US 422918A US 42291854 A US42291854 A US 42291854A US 2873952 A US2873952 A US 2873952A
Authority
US
United States
Prior art keywords
rotor
plates
sealing
strips
heat exchangers
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
US422918A
Inventor
Mudersbach Ernst
Firgau Werner
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.)
Svenska Rotor Maskiner AB
Original Assignee
Svenska Rotor Maskiner AB
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 Svenska Rotor Maskiner AB filed Critical Svenska Rotor Maskiner AB
Priority to US422918A priority Critical patent/US2873952A/en
Application granted granted Critical
Publication of US2873952A publication Critical patent/US2873952A/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
    • F28D19/047Sealing means
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10STECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10S165/00Heat exchange
    • Y10S165/009Heat exchange having a solid heat storage mass for absorbing heat from one fluid and releasing it to another, i.e. regenerator
    • Y10S165/013Movable heat storage mass with enclosure
    • Y10S165/016Rotary storage mass
    • Y10S165/02Seal and seal-engaging surface are relatively movable
    • Y10S165/021Seal engaging a face of cylindrical heat storage mass
    • Y10S165/022Seal defining sector-shaped flow area

Definitions

  • the problem is especially difiicult when the heat exchanger, due to its high capacity is of large dimensions, so that the thermal expansion is at a high value and further irregular distortion and warping of the rotor takes place as its temperature rises ascompared to idle condition and also due to the factthat the temperature will continuously vary somewhat during normal operation;
  • One solution taking the above mentioned distortion of the rotor particularly into consideration, provides for movable plates located between the rotor end faces and the stationary housing end walls and sealing off the transition zones of the rotor for separating the two main channels.
  • the movable plates are adapted to adjust themselves to distortions of the rotor which occur due to heat expansion of the rotor as a result of normal operation.
  • the rotary regenerative heat exchanger according to the invention contemplates an improvement of this type and is characterized substantially by a construction in which. the upper and the lower end sealing plates of a transition sector are connected with each other by means of a jacket plate covering the rotor at its circumference so that pairs of sealing plates follow the up and down movements of the rotor.
  • Fig. 1 illustrates in a diagrammatic view the general basic idea of the invention.
  • Fig. 2 shows a radial section through such a heat exchanger with a more detailed showing of construction details.
  • Fig. 3 shows a development of a vertical section through the rotor along a section surface adjacent the rotor jacket and concentric with the rotor axes.
  • FIG. 4 shows a fragmentary horizontal section through the heat exchanger in the range of the dead transition zone.
  • Fig. 5 shows this dead zone in a detail perspective view.
  • Fig. 6 shows a specific form of the holder of the lower sector joint.
  • the rotor shown is in a general manner formed with sectors separated byradial walls 1.
  • the heat exchanger in the present case is of the type having two channels of different cross sectional areas, with the front channel being smaller and forming the air channel whereas the rear and larger channel is the gas channel.
  • the two dead transition zones at the upper end face of the rotor are covered by plates 2 and 3 which are movable up and down whereas corresponding cover plates 2' and 3 at the lower end face of the rotor cannot be seen in this 'figure.
  • Also shown in Fig. 1 are the jacket plate 4 connecting the two end plates 2 and Z and the jacket plate 5 connecting the two end plates 3 and 3.
  • FIG. 2 More detailed features of the construction will be seen from Figs. 2 to 4 inclusive, illustrating some of the more important constructional characteristics which are also shown in Fig. 5.
  • the rotor is divided into separate annular chambers by concentric walls 7 which chambers in turn are divided by the radial walls 1.
  • the outermost concentric wall 7 which accordingly provides the outer wall of the rotor carries at its upper and lower ends circumferential flange rings 8 and 8' respectively so that outside the wall 7' an annular chamber is formed in which radial strips 9 are mounted. These strips 9 are very accurately fitted so that their outer edges as well as the outer edges of the two circumferential ring flanges 8 and 8' on the wall 7 are located on a theoretically accurate cylinder.
  • the jacket plate 4 is for this purpose adjustable in a radial direction by means of adjustable stops it] of which four are provided for each jacket plate.
  • Each stop 10 consists of a pin fixed to the jacket plate 4 and provided with a pressure spring and at its outer end carrying an adjustable nut.
  • the pressure springs bias the jacket plate towards the outer rotor wall 7 in accordance with the position of the adjustable nut.
  • the springs permit a yielding movement radially outwardly of the jacket plate 4. This is of importance in the event foreign particles enter between the wall 7 and jacket plate 4 which, without such a yieldable arrangement, would be likely to cause damage.
  • the distance between the plates 2 and 2', and 3 and 3' respectively is selectively adjustable by means of a pin 11 fixed to the plate under consideration and which like the stops are also provided with springs in order to permit a yieldable increase of the distance.
  • the sealing plates 2 and ,2 are provided at their radial edges with upwardly projecting strips 14 and 14 respectively.
  • Fixed to the stationary housing end wall are oppositely disposed corresponding strips 15 and 15.
  • the two strips of each pair of strips may accordingly move in close proximity to each other to provide a seal between the air channel L and the gas channel G which are disposed on opposite sides of the sealing device, and also results in reinforcing and accurately guiding movement of the sealing assembly.
  • spring plates 16 and 16 respectively are provided which are fixed to-the housing strips 15 and 15' and with their free edges sealingly engaging the strips 14 and 14'.
  • the space outwardly of the jacket plate 4 is closed by means of a cover 20 and the removal of this cover permits access to all of the sealing system so that accurate adjustment thereof may be made during operation.
  • the counter-weight 13 is so adjusted that it balances the whole weight of the sealing system. Naturally the influence of possible pressure differences created in the chambers 21 and 21' behind the end sealing plates 2 and 2' is not balanced. Due to the cross flow of the gaseous media from adjacent channels different pressures may arise which disturb the balance. In order to over come this the two equalizing chambers 21 and 21 are connected with each other through the chamber 22 formed behind the jacket plate 4.
  • the small adjusting movements required will then automatically follow by the balanced weight system during operation.
  • the rotor is subjected to distortion at the circumference in one direction when the boiler is placed in operation, and back in the other direction when the temperatures are again equalized.
  • the position of the flange rings 8 and 8 is then displaced at the circumference with respect to the hub.
  • the exact circular form of the flange rings will however be maintained. They are only displaced in a direction parallel to the axes.
  • the sealing plates are therefore only displaced due to changes in temperature when starting or stopping. During normal operation they will remain in their adjusted operating position.
  • the pivots or joints 6 and 6' by means of which the two opposite sealing plates are mounted near the rotor shaft, may be made adjustable from the outside, and for this purpose there may be provided a screw or a link projecting outwardly to a convenient point.
  • An exact adjustment of the distance from the sealing plates at the rotor ends to the rotor end faces is also possible at the inner pivoted ends. In many instances it is enough to adjust the pivots before putting the heat exchanger into operation and to leave it in the adjusted position.
  • the movements of the rotor end faces influenced by the temperature difference adjacent the shaft are relatively small. It may however, in spite of this, be of value to provide an automatic readjustment at this point.
  • the rotor In the present heat exchangers of this type the rotor is carried by an upper main support bearing. At the lower end the vertically suspended shaft rests on the rotor hub. Due to the higher temperature present during operation this supporting point will move downwardly to a certain extent.
  • the rotor-hub supported at its lower end expands in an upward direction so that at the upper hub end the expansion of the shaft may be lower temperature than the hub this compensation results in substantially maintaining the upper end of the hub in fixed vertical position. Accordingly additional adjusting means at this point may be dispensed with. It is enough to make the above mentioned adjustment manually for the upper pivot point of the upper sealing plate. At the lower pivots however this change of vertical position between a cold condition and a warm operating condition is to be taken into account.
  • Such a pivot holder for automatically adjusting the lower sealing plate is shown in Fig. 6 and the automatic adjustment is obtained here by means of the bearing.
  • the basic idea of this construction is moreover adaptable not only for the above disclosed embodiments but in general for rotary heat exchangers with the rotor carried at the top, and further also for such heat exchangers with a vertical rotor as well as for those having a horizontal rotor shaft.
  • the lower end of the rotor shaft 23 carried at its top is provided with a supporting ring 24 to which the rotor hub 25 is attached.
  • a guiding bearing 26 For exact central guiding of the shaft 23. there is pro vided a guiding bearing 26.
  • the bearing shells 33 of this guiding bearing 26 are not rigidly mounted but are slidable in order that they may follow the up and down movements of the lower end of the shaft 23.
  • the new and characteristic feature of this hearing resides in the fact that the bolt 28 which serves as a pivot point for the end sealing plates is connected with the guiding bearing 26.
  • a bolt 29 which at its upper end carries the bolt 28.
  • the nut 30 on the bolt 29 determines the distance between the plates as a spring 31, which abuts against a plate 34 resting on the bearing shells 33, urges the bolt 29 upwards against the nut-stop 30.
  • the spring 31 permits a yielding movement upon an increase of the distance between the sealing plate and the rotor end face.
  • the pivots of the sealing plates 2' and 3' are not diametrically opposite relative to the geometric axes of the rotor shaft but are at one side.
  • the weight of the two sealing plates which rest on one side of the guiding bearing 26 results in an unbalanced loading of the bearing shells. It is however possible to balance this by loading the other side of the bearing to the same extent.
  • a spring 32 may be employed which is so dimensioned that its force corresponds to the loading from the sealing plates.
  • a rotary regenerative heat exchanger for gaseous media of the character described comprising a rotor and stationary housing structure, said housing structure including end plates having apertures therein separated by sector shaped portions of said end plates and providing two channels for flow of difierent heat exchanging media through said heat exchanger, said rotor having radial partitions dividing the rotor into a plurality of sectorshaped compartments, sealing plates at the ends of the rotor confronting said sector shaped portions of said end plates arranged to seal the ends of said compartments in the transition zones separating the channels for said different media, said sealing plates being hinged at their inner ends and jacket plates sealingly interconnecting each set of the sealing plates at the opposite ends of the rotor, for sealing the rotor at its circumference, the assemblies of said movable sealing plates and said connecting jacket plates being movable to adjust themselves to compensate for distortions of the rotor structure caused by difierential thermal expansion of the latter.
  • the rotor includes an outer cylindrical shell around which the annular flanges at the ends of the rotor extend, and a plurality of circumferentially spaced axially extending radial strips which are located between said flanges, the outer edges of said strips and the outer circumferences of said flanges being defined by the envelope of a common cylinder.
  • said rotor includes a central rotor shaft, said rotor shaft having a fixed bearing for axially locating one end of the shaft relative to said stationary housing structure and an axially movable guide hearing at the other end of the shaft, the sealing plates at the end of the rotor at which said guide bearing is located being pivotally mounted and adjustably connected to said guide bearing.
  • Structure as defined in claim 10 including spring means located on the side of the rotor axis opposite the pivotal connection of said sealing plates for balancing the loading on said guide bearing.

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

2 Sheets-Sheet 1 Feb. 17,1959 E. MUDERSBACH ETAL ROTARY REGENERATIVE HEAT EXCHANGERS FOR GASEOUS MEDIA Filed April '15, 1954 imimrgki B) M W E. MUDERSBACH ETAL 2,873,952
ROTARY REGENERATIVE HEAT EXCHANGERS FOR GASEOUS MEDIA Feb. 17, 1959 2 Sheets-Sheet 2 Filed April 13, 1954 llll .rllli rill! nited States ROTARY REGENERATIVE HEAT EXCHANGERS FOR GASEOUS MEDIA Ernst Mudersbach, Heidelberg, and Werner Firgau, Heidelberg-Pfatfengrund, Germany, assignors, by mesne assignments, to Svenska Rotor Maskiner Aktiebolag, Nacka, Sweden, a corporation of Sweden Application April 13, 1954, Serial No. 422,918
12 Claims. (Cl. 2576) heat absorbing media flow must be sealed off from one another, so that a cross flow of the media from one channel to the other is prevented. Several proposals have already been made to obtain this result as far as possible, the problem often being solved by applying different proposals simultaneously in order to obtain a cooperation of their effects.
The problem is especially difiicult when the heat exchanger, due to its high capacity is of large dimensions, so that the thermal expansion is at a high value and further irregular distortion and warping of the rotor takes place as its temperature rises ascompared to idle condition and also due to the factthat the temperature will continuously vary somewhat during normal operation;
One solution, taking the above mentioned distortion of the rotor particularly into consideration, provides for movable plates located between the rotor end faces and the stationary housing end walls and sealing off the transition zones of the rotor for separating the two main channels. The movable plates are adapted to adjust themselves to distortions of the rotor which occur due to heat expansion of the rotor as a result of normal operation.
The rotary regenerative heat exchanger according to the invention contemplates an improvement of this type and is characterized substantially by a construction in which. the upper and the lower end sealing plates of a transition sector are connected with each other by means of a jacket plate covering the rotor at its circumference so that pairs of sealing plates follow the up and down movements of the rotor.
The principle of inter-connecting the two end sealing plates so that they move in pairs is known per se, but heretofore separate connecting rods have been used whereas the jacket sealing plate, also known per se, has formed a separate structural element. These connecting rods accordingly did not follow the up and down movements of the two sealing plates located opposite each other on either side of the rotor.
To interconnect all three of the plates of a dead sector results in a simpler construction and also aifords several constructional advantages which will be disclosed more in detail with reference to the drawings. Various improvements according to the invention will also be seen from the drawings.
Fig. 1 illustrates in a diagrammatic view the general basic idea of the invention.
Fig. 2 shows a radial section through such a heat exchanger with a more detailed showing of construction details.
Fig. 3 shows a development of a vertical section through the rotor along a section surface adjacent the rotor jacket and concentric with the rotor axes.
ate'nt Fig. 4 shows a fragmentary horizontal section through the heat exchanger in the range of the dead transition zone.
Fig. 5 shows this dead zone in a detail perspective view.
Fig. 6 shows a specific form of the holder of the lower sector joint.
The general basic idea of the invention will best appear from the diagrammatic view of Fig. 1.
The rotor shown is in a general manner formed with sectors separated byradial walls 1. The heat exchanger in the present case is of the type having two channels of different cross sectional areas, with the front channel being smaller and forming the air channel whereas the rear and larger channel is the gas channel. The two dead transition zones at the upper end face of the rotor are covered by plates 2 and 3 which are movable up and down whereas corresponding cover plates 2' and 3 at the lower end face of the rotor cannot be seen in this 'figure. Also shown in Fig. 1 are the jacket plate 4 connecting the two end plates 2 and Z and the jacket plate 5 connecting the two end plates 3 and 3. Near the rotor shaft the two end faces covering plates2 and 3 are pivotally mounted by means of a joint 6 for tilting upv and down. At the lower end of the rotor this joint corresponds to a joint 6 not visible in Fig. 1. From Fig. 1 it will be evident that upon distortion of the rotor each of the two plate systems may follow the up and down movements of the rotor without difliculty so that the distances between the rotor end faces and the end plates will remain unchanged.
More detailed features of the construction will be seen from Figs. 2 to 4 inclusive, illustrating some of the more important constructional characteristics which are also shown in Fig. 5.
The rotor is divided into separate annular chambers by concentric walls 7 which chambers in turn are divided by the radial walls 1. The outermost concentric wall 7 which accordingly provides the outer wall of the rotor carries at its upper and lower ends circumferential flange rings 8 and 8' respectively so that outside the wall 7' an annular chamber is formed in which radial strips 9 are mounted. These strips 9 are very accurately fitted so that their outer edges as well as the outer edges of the two circumferential ring flanges 8 and 8' on the wall 7 are located on a theoretically accurate cylinder.
In a similar manner all intermediate walls 1 and 7 extend the full height of the rotor. The two end faces of the rotor and the end surfaces of the two ring flanges 8 and 8 are turned in a lathe so as to obtain a completely even surface. Also at their outer circumferences the two flange rings are turned off so that they form true circles and permit an accurate adjustment of the strips 9.
Since in this Way there is provided an accurately running rotor it is possible to accurately adjust the jacket plate 4 with respect to the rotor. The jacket plate 4 is for this purpose adjustable in a radial direction by means of adjustable stops it] of which four are provided for each jacket plate. Each stop 10 consists of a pin fixed to the jacket plate 4 and provided with a pressure spring and at its outer end carrying an adjustable nut. The pressure springs bias the jacket plate towards the outer rotor wall 7 in accordance with the position of the adjustable nut. The springs, however, permit a yielding movement radially outwardly of the jacket plate 4. This is of importance in the event foreign particles enter between the wall 7 and jacket plate 4 which, without such a yieldable arrangement, would be likely to cause damage. In a corresponding manner the distance between the plates 2 and 2', and 3 and 3' respectively is selectively adjustable by means of a pin 11 fixed to the plate under consideration and which like the stops are also provided with springs in order to permit a yieldable increase of the distance.
The whole of this device comprising the end sealing plates and the jacket plates, is suspended from one end of a double armed lever 12 the other end of which is loaded by an accurately adjustable counter-weight 13. Due to this weight-balance the whole sealing system may, accordingly, very easily follow all up and down movements of the rotor.
The sealing plates 2 and ,2 are provided at their radial edges with upwardly projecting strips 14 and 14 respectively. Fixed to the stationary housing end wall are oppositely disposed corresponding strips 15 and 15. The two strips of each pair of strips may accordingly move in close proximity to each other to provide a seal between the air channel L and the gas channel G which are disposed on opposite sides of the sealing device, and also results in reinforcing and accurately guiding movement of the sealing assembly. In order to improve the sealing, spring plates 16 and 16 respectively are provided which are fixed to-the housing strips 15 and 15' and with their free edges sealingly engaging the strips 14 and 14'. These details are clearly shown in Fig. 3 and also in Fig. 5 in which the spring plate 16 is shown somewhat shortened in order to show the position of the strip.
An exactly corresponding seal is provided for the jacket plate 4 which at its outer edges is provided with strips 17 cooperating with strips 18 rigidly secured to the housing. The space between the two strips is covered by spring plates 19.
The space outwardly of the jacket plate 4 is closed by means of a cover 20 and the removal of this cover permits access to all of the sealing system so that accurate adjustment thereof may be made during operation.
The counter-weight 13 is so adjusted that it balances the whole weight of the sealing system. Naturally the influence of possible pressure differences created in the chambers 21 and 21' behind the end sealing plates 2 and 2' is not balanced. Due to the cross flow of the gaseous media from adjacent channels different pressures may arise which disturb the balance. In order to over come this the two equalizing chambers 21 and 21 are connected with each other through the chamber 22 formed behind the jacket plate 4.
The above details described in connection with the jacket plate 4 are also to be found in connection with the jacket plate 5.
From the figures and the foregoing description it will be understood that the two channels are well sealed and that only small forces are necessary for adjusting the sealing system. The greatest movement naturally takes place at the circumference of the rotor. The stops 10 and 11 are adjusted during normal operation.
The small adjusting movements required will then automatically follow by the balanced weight system during operation. The rotor is subjected to distortion at the circumference in one direction when the boiler is placed in operation, and back in the other direction when the temperatures are again equalized. The position of the flange rings 8 and 8 is then displaced at the circumference with respect to the hub. The exact circular form of the flange rings will however be maintained. They are only displaced in a direction parallel to the axes. The sealing plates are therefore only displaced due to changes in temperature when starting or stopping. During normal operation they will remain in their adjusted operating position.
The pivots or joints 6 and 6', by means of which the two opposite sealing plates are mounted near the rotor shaft, may be made adjustable from the outside, and for this purpose there may be provided a screw or a link projecting outwardly to a convenient point. An exact adjustment of the distance from the sealing plates at the rotor ends to the rotor end faces is also possible at the inner pivoted ends. In many instances it is enough to adjust the pivots before putting the heat exchanger into operation and to leave it in the adjusted position. The movements of the rotor end faces influenced by the temperature difference adjacent the shaft are relatively small. It may however, in spite of this, be of value to provide an automatic readjustment at this point.
In the present heat exchangers of this type the rotor is carried by an upper main support bearing. At the lower end the vertically suspended shaft rests on the rotor hub. Due to the higher temperature present during operation this supporting point will move downwardly to a certain extent. The rotor-hub supported at its lower end expands in an upward direction so that at the upper hub end the expansion of the shaft may be lower temperature than the hub this compensation results in substantially maintaining the upper end of the hub in fixed vertical position. Accordingly additional adjusting means at this point may be dispensed with. It is enough to make the above mentioned adjustment manually for the upper pivot point of the upper sealing plate. At the lower pivots however this change of vertical position between a cold condition and a warm operating condition is to be taken into account.
Such a pivot holder for automatically adjusting the lower sealing plate is shown in Fig. 6 and the automatic adjustment is obtained here by means of the bearing. The basic idea of this construction is moreover adaptable not only for the above disclosed embodiments but in general for rotary heat exchangers with the rotor carried at the top, and further also for such heat exchangers with a vertical rotor as well as for those having a horizontal rotor shaft.
In the embodiment illustrated the lower end of the rotor shaft 23 carried at its top is provided with a supporting ring 24 to which the rotor hub 25 is attached. For exact central guiding of the shaft 23. there is pro vided a guiding bearing 26. The bearing shells 33 of this guiding bearing 26 are not rigidly mounted but are slidable in order that they may follow the up and down movements of the lower end of the shaft 23. The new and characteristic feature of this hearing resides in the fact that the bolt 28 which serves as a pivot point for the end sealing plates is connected with the guiding bearing 26. As the bearing shells 33 of the guiding bearing follow the up and down movements of the lower end of the shaft 23 due to temperature changes, the pivots of the sealing plates will accordingly accurately follow such movement. It is accordingly only necessary to adjust the desired plate distance once.
For this purpose there is provided a bolt 29 which at its upper end carries the bolt 28. The nut 30 on the bolt 29 determines the distance between the plates as a spring 31, which abuts against a plate 34 resting on the bearing shells 33, urges the bolt 29 upwards against the nut-stop 30. Also the spring 31 permits a yielding movement upon an increase of the distance between the sealing plate and the rotor end face.
It is to be noted that the pivots of the sealing plates 2' and 3' are not diametrically opposite relative to the geometric axes of the rotor shaft but are at one side. The weight of the two sealing plates which rest on one side of the guiding bearing 26 results in an unbalanced loading of the bearing shells. It is however possible to balance this by loading the other side of the bearing to the same extent. For this purpose a spring 32 may be employed which is so dimensioned that its force corresponds to the loading from the sealing plates.
We claim:
1. A rotary regenerative heat exchanger for gaseous media of the character described comprising a rotor and stationary housing structure, said housing structure including end plates having apertures therein separated by sector shaped portions of said end plates and providing two channels for flow of difierent heat exchanging media through said heat exchanger, said rotor having radial partitions dividing the rotor into a plurality of sectorshaped compartments, sealing plates at the ends of the rotor confronting said sector shaped portions of said end plates arranged to seal the ends of said compartments in the transition zones separating the channels for said different media, said sealing plates being hinged at their inner ends and jacket plates sealingly interconnecting each set of the sealing plates at the opposite ends of the rotor, for sealing the rotor at its circumference, the assemblies of said movable sealing plates and said connecting jacket plates being movable to adjust themselves to compensate for distortions of the rotor structure caused by difierential thermal expansion of the latter.
2. Structure as defined in claim 1 which includes stop members cooperating with said sealing plates and permitting adjustment of the distance between the two plates at the respective ends of the rotor.
3. Structure as defined in claim 1 which includes stop members cooperating with said jacket plates and permitting selective adjustment of the radial location of said plates.
4. Structure as defined in claim 3 in which the adjustable stop members yieldably press the sealing plates toward the rotor and positively limit the minimum space of said plates while permitting resilient yielding of the plates away from the rotor.
5. Structure as defined in claim 1 in which the radial partitions of the rotor extend through the full height of the rotor and at their opposite ends are in alignment with a circumferential annular flange at each end of the rotor, the entire end face of the rotor being formed to provide a surface accurately formed to lie in a common plane.
6. Structure as defined in claim 5 in which the rotor includes an outer cylindrical shell around which the annular flanges at the ends of the rotor extend, and a plurality of circumferentially spaced axially extending radial strips which are located between said flanges, the outer edges of said strips and the outer circumferences of said flanges being defined by the envelope of a common cylinder.
7. Structure as defined in claim 1 in which the end and the circumferential sealing plates at each transition zone are provided with flanges projecting toward said stationary housing and said stationary housing is provided with strips rigidly secured thereto and in proximity to said flanges, said strips and flanges together with said sealing plates and the adjacent parts of said stationary housing structure forming a chamber closed on all sides.
8. Structure as defined in claim 7 including resilient sealing members mounted on certain of said strips and in resilient contact with said flanges in cooperative relation with the strips upon which said sealing members are mounted.
9. Structure as defined in claim 7 in which said chambers formed at each transition zone are in communication with one another.
10. Structure as defined in claim 1 in which said rotor includes a central rotor shaft, said rotor shaft having a fixed bearing for axially locating one end of the shaft relative to said stationary housing structure and an axially movable guide hearing at the other end of the shaft, the sealing plates at the end of the rotor at which said guide bearing is located being pivotally mounted and adjustably connected to said guide bearing.
11. Structure as defined in claim 10 including spring means located on the side of the rotor axis opposite the pivotal connection of said sealing plates for balancing the loading on said guide bearing.
12. Structure as defined in claim 11 including adjustable stop means for limiting the distance between the inner ends of the sealing plates and the end face of the rotor.
References Cited in the file of this patent UNITED STATES PATENTS
US422918A 1952-09-06 1954-04-13 Rotary regenerative heat exchangers for gaseous media Expired - Lifetime US2873952A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US422918A US2873952A (en) 1952-09-06 1954-04-13 Rotary regenerative heat exchangers for gaseous media

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE737964X 1952-09-06
US422918A US2873952A (en) 1952-09-06 1954-04-13 Rotary regenerative heat exchangers for gaseous media

Publications (1)

Publication Number Publication Date
US2873952A true US2873952A (en) 1959-02-17

Family

ID=25947313

Family Applications (1)

Application Number Title Priority Date Filing Date
US422918A Expired - Lifetime US2873952A (en) 1952-09-06 1954-04-13 Rotary regenerative heat exchangers for gaseous media

Country Status (1)

Country Link
US (1) US2873952A (en)

Cited By (21)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2945681A (en) * 1956-04-19 1960-07-19 Air Preheater Floating sector seals
US3022051A (en) * 1958-04-07 1962-02-20 Thompson Ramo Wooldridge Inc Controlled clearance regenerator seal
US3108632A (en) * 1960-04-20 1963-10-29 Combustion Eng Rotor arrangement for rotary regenerative heat exchanger
US3122200A (en) * 1960-05-24 1964-02-25 Koch Jakob Dynamic sealing means for rotary regenerative heat exchangers
US3166118A (en) * 1960-03-02 1965-01-19 Koch Jakob Rotor end sealing means for rotary regenerative heat exchangers
US3166119A (en) * 1961-04-13 1965-01-19 Combustion Eng Radial seal for rotary regenerative heat exchanger
US3181602A (en) * 1961-06-05 1965-05-04 Davidson & Co Ltd Heat exchangers
US3181601A (en) * 1960-12-05 1965-05-04 Appbau Rothemuhle Dr Brandt & Regenerative heat exchangers
US3246686A (en) * 1962-03-05 1966-04-19 Svenska Rotor Maskiner Ab Regenerative preheater including heat transfer mass and floating sealing plates
US3246687A (en) * 1964-03-31 1966-04-19 Air Preheater Thermal actuated sector plate
US3250316A (en) * 1963-04-19 1966-05-10 Svenska Rotor Maskiner Ab Regenerative heat exchangers
US3373797A (en) * 1965-11-29 1968-03-19 Svenska Rotor Maskiner Ab Regenerative heat exchanger
US3409073A (en) * 1965-07-27 1968-11-05 Botkachik Iosif Azarievich Device for sealing the rotor of a regenerative air heater
US3785431A (en) * 1970-09-08 1974-01-15 Svenska Rotor Maskiner Ab Rotary regenerative heat exchangers
US3786868A (en) * 1972-04-24 1974-01-22 Air Preheater Self-compensating sector plate
US3800859A (en) * 1967-07-20 1974-04-02 Munters C Transferrer of the thermodynamic characteristics of two gases
US4106553A (en) * 1976-04-26 1978-08-15 Toyota Jidosha Kogyo Kabushiki Kaisha Sealing device for a rotary regenerative heat exchanger
US4166496A (en) * 1978-08-21 1979-09-04 The Air Preheater Company, Inc. Static seal
WO2002081997A1 (en) * 2001-02-21 2002-10-17 Alstom (Switzerland) Ltd Axial seal plate for air preheaters
US6505679B2 (en) * 2001-02-21 2003-01-14 Alstom Power N.V. Low-distortion sector plate for air preheaters
US20230073822A1 (en) * 2020-05-13 2023-03-09 Howden Group Limited Parabolically deforming sector plate

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2055071A (en) * 1930-11-06 1936-09-22 Air Preheater Sealing means for heat exchangers
DE709143C (en) * 1938-09-08 1941-08-08 Ljungstroems Aangturbin Ab Circulating regenerative heat exchanger
US2678194A (en) * 1950-01-04 1954-05-11 Jarvis C Marble Sealing device for rotary heat exchangers
US2681209A (en) * 1949-02-09 1954-06-15 Jarvis C Marble Suction device for rotary regenerative preheaters
US2744731A (en) * 1950-05-12 1956-05-08 Brandt Herbert Regenerative heat exchanger

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2055071A (en) * 1930-11-06 1936-09-22 Air Preheater Sealing means for heat exchangers
DE709143C (en) * 1938-09-08 1941-08-08 Ljungstroems Aangturbin Ab Circulating regenerative heat exchanger
US2681209A (en) * 1949-02-09 1954-06-15 Jarvis C Marble Suction device for rotary regenerative preheaters
US2678194A (en) * 1950-01-04 1954-05-11 Jarvis C Marble Sealing device for rotary heat exchangers
US2744731A (en) * 1950-05-12 1956-05-08 Brandt Herbert Regenerative heat exchanger

Cited By (24)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2945681A (en) * 1956-04-19 1960-07-19 Air Preheater Floating sector seals
US3022051A (en) * 1958-04-07 1962-02-20 Thompson Ramo Wooldridge Inc Controlled clearance regenerator seal
US3166118A (en) * 1960-03-02 1965-01-19 Koch Jakob Rotor end sealing means for rotary regenerative heat exchangers
US3108632A (en) * 1960-04-20 1963-10-29 Combustion Eng Rotor arrangement for rotary regenerative heat exchanger
US3122200A (en) * 1960-05-24 1964-02-25 Koch Jakob Dynamic sealing means for rotary regenerative heat exchangers
US3181601A (en) * 1960-12-05 1965-05-04 Appbau Rothemuhle Dr Brandt & Regenerative heat exchangers
US3166119A (en) * 1961-04-13 1965-01-19 Combustion Eng Radial seal for rotary regenerative heat exchanger
US3181602A (en) * 1961-06-05 1965-05-04 Davidson & Co Ltd Heat exchangers
US3246686A (en) * 1962-03-05 1966-04-19 Svenska Rotor Maskiner Ab Regenerative preheater including heat transfer mass and floating sealing plates
US3250316A (en) * 1963-04-19 1966-05-10 Svenska Rotor Maskiner Ab Regenerative heat exchangers
US3246687A (en) * 1964-03-31 1966-04-19 Air Preheater Thermal actuated sector plate
US3409073A (en) * 1965-07-27 1968-11-05 Botkachik Iosif Azarievich Device for sealing the rotor of a regenerative air heater
US3373797A (en) * 1965-11-29 1968-03-19 Svenska Rotor Maskiner Ab Regenerative heat exchanger
US3800859A (en) * 1967-07-20 1974-04-02 Munters C Transferrer of the thermodynamic characteristics of two gases
US3785431A (en) * 1970-09-08 1974-01-15 Svenska Rotor Maskiner Ab Rotary regenerative heat exchangers
US3786868A (en) * 1972-04-24 1974-01-22 Air Preheater Self-compensating sector plate
US4106553A (en) * 1976-04-26 1978-08-15 Toyota Jidosha Kogyo Kabushiki Kaisha Sealing device for a rotary regenerative heat exchanger
US4166496A (en) * 1978-08-21 1979-09-04 The Air Preheater Company, Inc. Static seal
FR2441112A1 (en) * 1978-08-21 1980-06-06 Svenska Rotor Maskiner Ab STATIC SEAL
WO2002081997A1 (en) * 2001-02-21 2002-10-17 Alstom (Switzerland) Ltd Axial seal plate for air preheaters
US6505679B2 (en) * 2001-02-21 2003-01-14 Alstom Power N.V. Low-distortion sector plate for air preheaters
US6543520B2 (en) 2001-02-21 2003-04-08 Alstom Power N.V. Low-distortion axial seal plate for air preheaters
US20230073822A1 (en) * 2020-05-13 2023-03-09 Howden Group Limited Parabolically deforming sector plate
US12007174B2 (en) * 2020-05-13 2024-06-11 Howden Group Limited Parabolically deforming sector plate

Similar Documents

Publication Publication Date Title
US2873952A (en) Rotary regenerative heat exchangers for gaseous media
US2692760A (en) Yieldingly mounted circumferential seal
US2890009A (en) Vessel support
US2471995A (en) Adjustable circumferential seal for preheaters
US3185631A (en) Assembly comprising a heat source and associated apparatus
US2055071A (en) Sealing means for heat exchangers
US2287777A (en) Regenerative heat exchanger
US3250316A (en) Regenerative heat exchangers
US3010703A (en) Sealing arrangement
US3234999A (en) Regenerator seal
US3830287A (en) Rotor structure
US3368611A (en) Rotary regenerator seal with high pressure fluid recovery
US3108632A (en) Rotor arrangement for rotary regenerative heat exchanger
US3968569A (en) Clearance monitoring probe for rotary regenerative heat exchanger
US2684230A (en) End plate support in housing of regenerative heat exchange apparatus
US3246686A (en) Regenerative preheater including heat transfer mass and floating sealing plates
US2852234A (en) Rotary regenerative preheaters for gaseous media
US3024005A (en) Rotor adjusting arrangement
US3147952A (en) Pin-block, adjustable diaphragm support
US2229691A (en) Regenerative heat exchanger
US5628360A (en) Adjustable axial seal plates for rotary regenerative air preheaters
US3404727A (en) Rotary regenerative heat exchangers
US2765150A (en) Air preheater sealing
US3144903A (en) Rotary heat exchange apparatus with support therefor
US2892615A (en) Heat exchangers of the rotary regenerator type