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EP2458315B1 - Regenerative heat exchanger with forced rotor seal - Google Patents

Regenerative heat exchanger with forced rotor seal Download PDF

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Publication number
EP2458315B1
EP2458315B1 EP10015001.0A EP10015001A EP2458315B1 EP 2458315 B1 EP2458315 B1 EP 2458315B1 EP 10015001 A EP10015001 A EP 10015001A EP 2458315 B1 EP2458315 B1 EP 2458315B1
Authority
EP
European Patent Office
Prior art keywords
rotor
seal
heat exchanger
regenerative heat
rollers
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.)
Not-in-force
Application number
EP10015001.0A
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German (de)
French (fr)
Other versions
EP2458315A1 (en
Inventor
Erich Born
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.)
Balcke Duerr GmbH
Original Assignee
Balcke Duerr 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 Balcke Duerr GmbH filed Critical Balcke Duerr GmbH
Priority to EP10015001.0A priority Critical patent/EP2458315B1/en
Priority to US13/303,127 priority patent/US20120298326A1/en
Priority to RU2011148135/06A priority patent/RU2594034C2/en
Priority to CN201110461849.5A priority patent/CN102767981B/en
Publication of EP2458315A1 publication Critical patent/EP2458315A1/en
Application granted granted Critical
Publication of EP2458315B1 publication Critical patent/EP2458315B1/en
Not-in-force legal-status Critical Current
Anticipated expiration legal-status Critical

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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

Definitions

  • the invention relates to a regenerative heat exchanger according to the type specified in the preamble of claim 1.
  • Regenerative heat exchangers of the type in question are used to transfer heat from at least one gas volume flow to at least one other gas volume flow.
  • a rotating heat storage the so-called rotor, alternately warmed up by at least one gas volume flow and cooled by at least one other gas volume flow again, wherein heat energy is transferred from one to the other gas volume flow.
  • the rotor has two end faces, an outer jacket and, as a rule, a segmentation for receiving the heat storage masses.
  • the rotor is rotatably mounted about a central axis of rotation, wherein this axis of rotation is preferably aligned vertically.
  • a sealing system with core, radial and / or circumferential seals is provided.
  • the radial seals are arranged on the front sides of the rotor and are intended to prevent short-circuit volume flows between the gas flow rates.
  • the circumferential seals are arranged on the front edges of the rotor and are intended to prevent leakage volume flows into the rotor housing or into the environment. These seals are arranged stationary with respect to the rotating rotor. Due to a permanent relative movement between the rotor and these seals, as well as a constantly changing thermal expansion of the rotor and associated uneven rotor deformations, high demands are placed on the sealing system in order to achieve low losses (leaks) and thus high efficiency.
  • An object of the invention is therefore to provide a regenerative heat exchanger of the type in question with a simple and effective sealing system.
  • the sealing system for the rotor has at least one fixed relative to the rotor seal, which is pressed on the one hand to the rotor or to a rotor belonging to the component (eg. By acting weights, spring cylinders, actuators and the like) and on the other hand, supported by a plurality of rollers on the rotatable rotor or on a component belonging to the rotor and thus primarily forced out in the axial direction.
  • the seal in question is subject to a quasi-forced operation, which in operation means that the seal in question with a constant and predetermined by the rollers distance of the thermally induced rotor deformation is continuously updated, whereby a small and constant sealing gap is ensured.
  • rollers are arranged in the fixed seal. Furthermore, it is provided that the rollers roll on at least one corresponding running or rolling surface on the rotor or a component belonging to the rotor or are guided between two corresponding and axially spaced-apart rolling surfaces. These rolling surfaces are interchangeable Wear plates formed, which are attached to the rotor (rotor body or a rotor-associated component). Likewise, a reverse arrangement of rollers and treads may be provided.
  • the individual rollers at least in the region and in particular only in the range of the control points or pressure points of the seal against the rotor are arranged.
  • the supported by rollers seal is preferably a radial seal.
  • the supported by rollers seal is in particular a peripheral seal. It is also possible at the same time to support both the radial seals and the peripheral seals at least on one rotor side by means of rollers on the rotating rotor.
  • At least one circumferential seal supported by rollers on the rotor is coupled to a radial seal on the same rotor side, such that the relevant radial seal is moved in the axial direction during axial movement of the peripheral seal.
  • the relevant radial seal is arranged to be movable in the axial direction.
  • the coupling between the peripheral seal and the radial seal is effected in particular by a mechanical adjusting mechanism which transmits the axial movements of the peripheral seal by means of at least one adjusting bar or the like to the relevant radial seal.
  • the sealing system on a rotor side can thus perform movements that follow the rotor movements in the axial direction.
  • This preferably radially extending adjusting bar is ideally arranged in the rotor housing of the regenerative heat exchanger and indeed between the respective radial seal and the housing wall, wherein in this area also a sealing collar can be arranged.
  • Fig. 1 shows a generally designated 1 regenerative heat exchanger, of which, however, only one half of symmetry is shown.
  • the regenerative heat exchanger 1 comprises a rotor 2, which is rotatably mounted about a vertical axis of rotation A and arranged in a rotor housing 3.
  • the rotor 2 is traversed by a plurality of gas flow rates V, wherein heat is transferred from at least one gas volume flow to at least one other gas volume flow.
  • V For sealing the guided through the regenerative heat exchanger 1 gas volume flows V is a sealing system with radial seals 4 and 5 circumferential seals provided.
  • the radial seals 4 are arranged on the end faces of the rotor 2 and are intended to prevent short-circuit volume flows between the gas volume flows V.
  • the circumferential seals 5 are arranged on the front edges of the rotor 2 and are intended to prevent leakage volume flows into the rotor housing 3.
  • the radial seals 4 and the circumferential seals 5 are arranged stationary with respect to the rotating rotor 2.
  • the radial seals 4 and the peripheral seals 5 preferably form, together with any core seals (not shown), a self-contained sealing frame.
  • the arranged on the upper end side and on the lower end face of the rotor 2 seals are formed substantially identical. The following explanations relate, unless otherwise stated, by way of example only to the upper seals and apply analogously to the lower seals.
  • the upper radial seal 4 is designed as a sealing plate and fastened or suspended in the axial direction by means of a plurality of evenly spaced actuators or spring cylinders 7, 8 and 9 on the rotor housing 3. (The lower radial seal 4 is supported accordingly with spring cylinders or the like.) Each spring cylinder 7, 8 or 9 represents a control point for the radial seal 4. Instead of the spring cylinder 7, 8 and 9 can also be worked with counterweights.
  • the radial seal 4 is formed in the radial direction with joints 41 and 42, which divide the radial seal 4 into several sections. The radial seal 4 can thus adapt to thermally induced rotor deformations. Alternatively, it is possible to perform the radial seal 4 jointless and flexible.
  • a sealing gap S With the smallest possible gap.
  • a sealing or expansion sleeve (see reference numeral 10 in the lower heat exchanger area) can be arranged, which compensates relative movements of the radial seal 4 relative to the housing wall.
  • the peripheral seal 5 is designed as an annular sealing frame and fastened or suspended with a plurality of circumferentially uniformly distributed actuators or spring cylinders 11 on the rotor housing 3.
  • the peripheral seal 5 can be segmented, executed with joints or jointless and flexible.
  • Each spring cylinder 11 represents a control point for the peripheral seal 5, wherein the peripheral seal 5, for example, is pressed against the rotor flange 6 as a result of a weight excess (weight force minus the actuating force in the spring cylinders 11).
  • the circumferential seal 5 is supported by means of a plurality of rollers 12 on the rotor flange 6 belonging to the rotor 2.
  • a roller 12 is provided at least in the region of each control point.
  • the rollers 12 are arranged in a recess in the peripheral seal 5 and preferably also rotatably mounted therein (eg. By means of an axis).
  • the rollers 12 roll on a wear plate 14 attached to the rotor flange 6.
  • the wear plate 14 is formed segmented in the circumferential direction.
  • Such a wear plate may also be provided on a corresponding rolling surface in the circumferential seal 5. It is also conceivable that the rollers 12 are guided sandwiched between two in the axial direction a spaced apart wear plates.
  • a mechanical coupling of the radial seals 4 with the peripheral seals 5 is provided both on the upper end side and on the lower end side of the rotor 2, to which the peripheral seals 5 and the radial seals 4 are non-positively connected.
  • the radial seals 4 follow the positively guided movement of the circumferential seals 5 in the axial direction a, for which purpose the radial seals 4 are movably mounted in the axial direction a.
  • the sealing of the rotor 2 is significantly improved and leaks are significantly reduced.
  • Fig. 2 shows an example in which, unlike the first embodiment of the Fig. 1 attached to the peripheral seal 5 rollers 12 between two axially spaced Rotor flanges 61 and 62 are guided with corresponding rolling surfaces. As a result, a "direct" positive guidance for the peripheral seal 5 is made possible. Otherwise, the explanations concerning the first exemplary embodiment of FIG Fig. 1 ,
  • a mechanical coupling of the circumferential seals 5 is also provided with the radial seals 4.
  • the circumferential seals 5 are each connected to a radially extending adjusting bar 16, which brings about a plurality of actuators 17, an adjustment of the respective radial seal 4 (on the same rotor side) in the axial direction a. D. h.
  • the positively driven movement of a peripheral seal 5 is transmitted according to the lever ratios to the relevant radial seal 4 and on the individual sections, including the radial seals 4 movably mounted in the axial direction or z. B. are also flexible.
  • the radially extending adjusting bars 16 are arranged in the interior of the rotor housing 3. Likewise, the adjusting bars 16 could also be arranged outside the rotor housing 3.
  • Fig. 4 shows a third embodiment in which the radial seals 4 are supported by means of rollers 18 on the end faces of the rotor 2.
  • the rollers 18 are arranged in the region of the control points or spring cylinders 7, 8 and 9.
  • At the end faces of the rotor 2 corresponding rolling surfaces are formed. These rolling surfaces may be formed on wear plates 19, as exemplified for the lower, radially inner roller 18.

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  • 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)
  • Sealing Devices (AREA)
  • Sealing Using Fluids, Sealing Without Contact, And Removal Of Oil (AREA)

Description

Die Erfindung betrifft einen regenerativen Wärmetauscher gemäß der im Oberbegriff des Anspruchs 1 angegebenen Art.The invention relates to a regenerative heat exchanger according to the type specified in the preamble of claim 1.

Regenerative Wärmetauscher der betreffenden Art dienen der Wärmeübertragung von wenigstens einem Gasvolumenstrom auf wenigstens einen anderen Gasvolumenstrom. Hierbei wird eine drehender Wärmespeicher, der so genannte Rotor, abwechselnd durch wenigstens einen Gasvolumenstrom aufgewärmt und durch wenigstens einen anderen Gasvolumenstrom wieder abgekühlt, wobei Wärmeenergie von dem einen auf den anderen Gasvolumenstrom übertragen wird. Hierdurch kann einer der Gasvolumenströme aufgewärmt und ein anderer Gasvolumenstrom abgekühlt werden. Der Rotor weist zwei Stirnseiten, einen Außenmantel und in der Regel eine Segmentierung zur Aufnahme der Wärmespeichermassen auf. Der Rotor ist um eine zentrale Drehachse drehbar gelagert, wobei diese Drehachse vorzugsweise vertikal ausgerichtet ist.Regenerative heat exchangers of the type in question are used to transfer heat from at least one gas volume flow to at least one other gas volume flow. In this case, a rotating heat storage, the so-called rotor, alternately warmed up by at least one gas volume flow and cooled by at least one other gas volume flow again, wherein heat energy is transferred from one to the other gas volume flow. As a result, one of the gas volume flows can be warmed up and another gas volume flow can be cooled. The rotor has two end faces, an outer jacket and, as a rule, a segmentation for receiving the heat storage masses. The rotor is rotatably mounted about a central axis of rotation, wherein this axis of rotation is preferably aligned vertically.

Zur Abdichtung der durch den regenerativen Wärmetauscher geführten Gasvolumenströme ist ein Dichtungssystem mit Kern-, Radial- und/oder Umfangsdichtungen vorgesehen. Die Radialdichtungen sind an den Stirnseiten des Rotors angeordnet und sollen Kurzschluss-Volumenströme zwischen den Gasvolumenströmen verhindern. Die Umfangsdichtungen sind an den stirnseitigen Rändern des Rotors angeordnet und sollen Leckage-Volumenströme in das Rotorgehäuse hinein oder in die Umgebung verhindern. Diese Dichtungen sind bezüglich des drehenden Rotors ortsfest angeordnet. Aufgrund einer permanenten Relativbewegung zwischen dem Rotor und diesen Dichtungen, sowie einer sich ständig verändernden Wärmeausdehnung des Rotors und hiermit einhergehenden ungleichmäßigen Rotorverformungen, sind hohe Ansprüche an das Dichtungssystem zu stellen, um geringe Verluste (Leckagen) und somit einen hohen Wirkungsgrad zu erzielen.For sealing the guided through the regenerative heat exchanger gas flow rates a sealing system with core, radial and / or circumferential seals is provided. The radial seals are arranged on the front sides of the rotor and are intended to prevent short-circuit volume flows between the gas flow rates. The circumferential seals are arranged on the front edges of the rotor and are intended to prevent leakage volume flows into the rotor housing or into the environment. These seals are arranged stationary with respect to the rotating rotor. Due to a permanent relative movement between the rotor and these seals, as well as a constantly changing thermal expansion of the rotor and associated uneven rotor deformations, high demands are placed on the sealing system in order to achieve low losses (leaks) and thus high efficiency.

Aus dem Stand der Technik sind diverse Dichtungssysteme bekannt, die im Betrieb einen relativ geringen Dichtspalt zwischen Dichtung und Rotor ermöglichen sollen. Diesbezüglich wird z. B. auf die US 3,246,686 , die EP 1 777 478 A1 oder auf die EP 2 177 855 A1 verwiesen. Die bekannten Dichtungssysteme sind in der Praxis jedoch häufig unverhältnismäßig aufwändig und teuer.Various sealing systems are known from the prior art, which should allow a relatively small sealing gap between the seal and rotor during operation. In this regard, z. B. on the US 3,246,686 , the EP 1 777 478 A1 or on the EP 2 177 855 A1 directed. However, the known sealing systems are often disproportionately expensive and expensive in practice.

Eine Aufgabe der Erfindung ist es daher, einen regenerativen Wärmetauscher der betreffenden Art mit einem einfachen und effektiven Dichtungssystem anzugeben.An object of the invention is therefore to provide a regenerative heat exchanger of the type in question with a simple and effective sealing system.

Diese Aufgabe wird gelöst von einem regenerativen Wärmetauscher mit den Merkmalen des Anspruchs 1. Bevorzugte Weiterbildungen und Ausgestaltungen sind in den abhängigen Ansprüchen angegeben.This object is achieved by a regenerative heat exchanger with the features of claim 1. Preferred developments and refinements are specified in the dependent claims.

Die Lösung der obenstehenden Aufgabe gelingt, indem das Dichtungssystem für den Rotor wenigstens eine gegenüber dem Rotor feststehende Dichtung aufweist, die einerseits an den Rotor oder an ein zum Rotor gehörendes Bauteil angedrückt wird (bspw. durch wirkende Gewichtskräfte, Federzylinder, Stellglieder und dergleichen) und die andererseits mittels einer Vielzahl von Laufrollen am drehbaren Rotor oder an einem zum Rotor gehörenden Bauteil abgestützt und somit vorrangig in axialer Richtung zwangsgeführt ist. D. h. die betreffende Dichtung unterliegt quasi einer Zwangsführung, was im Betrieb dazu führt, dass die betreffende Dichtung mit einem konstanten und durch die Laufrollen vorgegebenen Abstand der thermisch bedingten Rotorverformung fortwährend nachgeführt wird, wodurch ein geringer und konstanter Dichtspalt gewährleistet ist.The solution of the above object is achieved by the sealing system for the rotor has at least one fixed relative to the rotor seal, which is pressed on the one hand to the rotor or to a rotor belonging to the component (eg. By acting weights, spring cylinders, actuators and the like) and on the other hand, supported by a plurality of rollers on the rotatable rotor or on a component belonging to the rotor and thus primarily forced out in the axial direction. Ie. the seal in question is subject to a quasi-forced operation, which in operation means that the seal in question with a constant and predetermined by the rollers distance of the thermally induced rotor deformation is continuously updated, whereby a small and constant sealing gap is ensured.

Hierdurch können mit einem verhältnismäßig geringen baulichen Aufwand minimale Dichtspalte realisiert werden, wodurch Kurzschluss- und/oder Leckage-Volumenströme äußerst gering ausfallen. Bei regenerativen Wärmetauschern mit Absaugung reduziert sich die abzusaugende Gasmenge. Ebenso reduziert sich bei Einsatz von Sperrgas die Sperrgasmenge. Zudem erweist sich das erfindungsgemäße Konzept als sehr montagefreundlich und einfach in der Handhabung und Wartung. Ein weiterer Vorteil ist darin zu sehen, dass auf die aus dem Stand der Technik bekannten elektromechanischen und meist sensorgesteuerten Verstelleinrichtungen für die Dichtungen verzichtet werden kann.As a result, minimal sealing gaps can be realized with a relatively low structural complexity, whereby short-circuit and / or leakage volume flows are extremely low. With regenerative heat exchangers with extraction, the amount of gas to be extracted is reduced. Likewise, the amount of purge gas is reduced when using purge gas. In addition, the inventive concept proves to be very easy to install and easy to use and maintain. A further advantage is the fact that it is possible to dispense with the electromechanical and usually sensor-controlled adjusting devices for the seals known from the prior art.

Es ist vorgesehen, dass die Laufrollen in der feststehenden Dichtung angeordnet sind. Weiterhin ist vorgesehen, dass die Laufrollen auf wenigstens einer korrespondierenden Lauf- bzw. Rollfläche am Rotor oder einem zum Rotor gehörenden Bauteil abrollen oder zwischen zwei korrespondierenden und axial zueinander beabstandeten Rollflächen geführt sind. Diese Rollflächen sind an austauschbaren Verschleißplatten ausgebildet, die am Rotor (Rotorkörper oder einem zum Rotor gehörenden Bauteil) befestigt sind. Ebenso kann auch eine umgekehrte Anordnung von Laufrollen und Laufflächen vorgesehen sein.It is envisaged that the rollers are arranged in the fixed seal. Furthermore, it is provided that the rollers roll on at least one corresponding running or rolling surface on the rotor or a component belonging to the rotor or are guided between two corresponding and axially spaced-apart rolling surfaces. These rolling surfaces are interchangeable Wear plates formed, which are attached to the rotor (rotor body or a rotor-associated component). Likewise, a reverse arrangement of rollers and treads may be provided.

Um insbesondere in den kritischen Bereichen in denen die Dichtung an den Rotor angedrückt wird (Stellpunkte) einen minimalen Dichtspalt zu gewährleisten, ist bevorzugt vorgesehen, dass die einzelnen Laufrollen zumindest im Bereich und insbesondere nur im Bereich der Stellpunkte bzw. Andrückpunkte der Dichtung gegen den Rotor angeordnet sind.In order to ensure a minimum sealing gap, in particular in the critical areas in which the seal is pressed onto the rotor, it is preferably provided that the individual rollers at least in the region and in particular only in the range of the control points or pressure points of the seal against the rotor are arranged.

Bei der mittels Laufrollen abgestützten Dichtung handelt es sich bevorzugt um eine Radialdichtung. Bei der mittels Laufrollen abgestützten Dichtung handelt es sich insbesondere um eine Umfangsdichtung. Ebenso ist möglich, zugleich sowohl die Radialdichtungen als auch die Umfangsdichtungen zumindest an einer Rotorseite mittels Laufrollen am sich drehenden Rotor abzustützen.The supported by rollers seal is preferably a radial seal. The supported by rollers seal is in particular a peripheral seal. It is also possible at the same time to support both the radial seals and the peripheral seals at least on one rotor side by means of rollers on the rotating rotor.

Nach einer besonders bevorzugten Weiterbildung ist vorgesehen, dass wenigstens eine mittels Laufrollen am Rotor abgestützte Umfangsdichtung mit einer Radialdichtung an derselben Rotorseite gekoppelt ist, derart, dass die betreffende Radialdichtung beim axialen Bewegen der Umfangsdichtung in axialer Richtung mitbewegt wird. Hierzu ist die betreffende Radialdichtung in axialer Richtung beweglich angeordnet. Die Kopplung zwischen der Umfangsdichtung und der Radialdichtung erfolgt insbesondere durch einen mechanischen Stellmechanismus, der die axialen Bewegungen der Umfangsdichtung mittels wenigstens eines Stellbalkens oder dergleichen auf die betreffende Radialdichtung überträgt. Das Dichtsystem an einer Rotorseite kann somit Bewegungen ausführen, die den Rotorbewegungen in axialer Richtung folgen. Dieser vorzugsweise radial verlaufende Stellbalken ist idealerweise im Rotorgehäuse des regenerativen Wärmetauschers angeordnet und zwar zwischen der betreffenden Radialdichtung und der Gehäusewandung, wobei in diesem Bereich auch eine Dichtmanschette angeordnet sein kann.According to a particularly preferred embodiment, it is provided that at least one circumferential seal supported by rollers on the rotor is coupled to a radial seal on the same rotor side, such that the relevant radial seal is moved in the axial direction during axial movement of the peripheral seal. For this purpose, the relevant radial seal is arranged to be movable in the axial direction. The coupling between the peripheral seal and the radial seal is effected in particular by a mechanical adjusting mechanism which transmits the axial movements of the peripheral seal by means of at least one adjusting bar or the like to the relevant radial seal. The sealing system on a rotor side can thus perform movements that follow the rotor movements in the axial direction. This preferably radially extending adjusting bar is ideally arranged in the rotor housing of the regenerative heat exchanger and indeed between the respective radial seal and the housing wall, wherein in this area also a sealing collar can be arranged.

Nachfolgend wird die Erfindung anhand von in der Zeichnung dargestellten Ausführungsbeispielen weiter beschrieben. Es zeigen in schematischen Schnitt-Teildarstellungen:

  • Fig. 1 ein erstes Ausführungsbeispiel eines regenerativen Wärmetauschers;
  • Fig. 2 ein Beispiel eines regenerativen Wärmetauschers;
  • Fig. 3 ein zweites Ausführungsbeispiel eines regenerativen Wärmetauschers; und
  • Fig. 4 ein drittes Ausführungsbeispiel eines regenerativen Wärmetauschers.
The invention will be further described with reference to embodiments shown in the drawings. Shown in schematic sectional partial representations:
  • Fig. 1 a first embodiment of a regenerative heat exchanger;
  • Fig. 2 an example of a regenerative heat exchanger;
  • Fig. 3 a second embodiment of a regenerative heat exchanger; and
  • Fig. 4 A third embodiment of a regenerative heat exchanger.

Fig. 1 zeigt einen insgesamt mit 1 bezeichneten regenerativen Wärmetauscher, von dem jedoch nur eine Symmetriehälfte dargestellt ist. Der regenerative Wärmetauscher 1 umfasst einen Rotor 2, der um eine vertikale Drehachse A drehbar gelagert und in einem Rotorgehäuse 3 angeordnet ist. Der Rotor 2 wird von mehreren Gasvolumenströmen V durchströmt, wobei Wärme von wenigstens einem Gasvolumenstrom auf wenigstens einen anderen Gasvolumenstrom übertragen wird. Zur Abdichtung der durch den regenerativen Wärmetauscher 1 geführten Gasvolumenströme V ist ein Dichtungssystem mit Radialdichtungen 4 und Umfangsdichtungen 5 vorgesehen. Die Radialdichtungen 4 sind an den Stirnseiten des Rotors 2 angeordnet und sollen Kurzschluss-Volumenströme zwischen den Gasvolumenströmen V verhindern. Die Umfangsdichtungen 5 sind an den stirnseitigen Rändern des Rotors 2 angeordnet und sollen Leckage-Volumenströme in das Rotorgehäuse 3 hinein verhindern. Die Radialdichtungen 4 und die Umfangsdichtungen 5 sind bezüglich des drehenden Rotors 2 ortsfest angeordnet. Die Radialdichtungen 4 und die Umfangsdichtungen 5 bilden bevorzugt, zusammen mit etwaigen Kerndichtungen (nicht dargestellt), einen in sich geschlossenen Dichtrahmen aus. Die an der oberen Stirnseite und an der unteren Stirnseite des Rotors 2 angeordneten Dichtungen sind im Wesentlichen identisch ausgebildet. Die nachfolgenden Erläuterungen beziehen sich, falls nicht anders angegeben, beispielhaft nur auf die oberen Dichtungen und gelten analog für die unteren Dichtungen. Fig. 1 shows a generally designated 1 regenerative heat exchanger, of which, however, only one half of symmetry is shown. The regenerative heat exchanger 1 comprises a rotor 2, which is rotatably mounted about a vertical axis of rotation A and arranged in a rotor housing 3. The rotor 2 is traversed by a plurality of gas flow rates V, wherein heat is transferred from at least one gas volume flow to at least one other gas volume flow. For sealing the guided through the regenerative heat exchanger 1 gas volume flows V is a sealing system with radial seals 4 and 5 circumferential seals provided. The radial seals 4 are arranged on the end faces of the rotor 2 and are intended to prevent short-circuit volume flows between the gas volume flows V. The circumferential seals 5 are arranged on the front edges of the rotor 2 and are intended to prevent leakage volume flows into the rotor housing 3. The radial seals 4 and the circumferential seals 5 are arranged stationary with respect to the rotating rotor 2. The radial seals 4 and the peripheral seals 5 preferably form, together with any core seals (not shown), a self-contained sealing frame. The arranged on the upper end side and on the lower end face of the rotor 2 seals are formed substantially identical. The following explanations relate, unless otherwise stated, by way of example only to the upper seals and apply analogously to the lower seals.

Die obere Radialdichtung 4 ist als Dichtplatte ausgeführt und in axialer Richtung mittels mehrerer gleichmäßig beabstandeter Stellglieder oder Federzylinder 7, 8 und 9 am Rotorgehäuse 3 befestigt bzw. abgehangen. (Die untere Radialdichtung 4 ist entsprechend mit Federzylindern oder dergleichen abgestützt.) Jeder Federzylinder 7, 8 oder 9 repräsentiert einen Stellpunkt für die Radialdichtung 4. Anstelle der Federzylinder 7, 8 und 9 kann auch mit Gegengewichten gearbeitet werden. Die Radialdichtung 4 ist in radialer Richtung mit Gelenken 41 und 42 ausgebildet, die die Radialdichtung 4 in mehrere Abschnitte unterteilen. Die Radialdichtung 4 kann sich damit thermisch bedingten Rotorverformungen anpassen. Alternativ ist es möglich, die Radialdichtung 4 gelenklos und flexibel auszuführen. Zwischen der Radialdichtung 4 und der oberen Stirnseite des Rotors 2 besteht ein Dichtspalt S mit einem möglichst geringen Spaltmaß. Zwischen der Radialdichtung 4 und der Gehäusewandung des Rotorgehäuses 3 kann eine Dicht- bzw. Dehnungsmanschette (siehe Bezugszeichen 10 im unteren Wärmetauscherbereich) angeordnet sein, die Relativbewegungen der Radialdichtung 4 gegenüber der Gehäusewandung ausgleicht.The upper radial seal 4 is designed as a sealing plate and fastened or suspended in the axial direction by means of a plurality of evenly spaced actuators or spring cylinders 7, 8 and 9 on the rotor housing 3. (The lower radial seal 4 is supported accordingly with spring cylinders or the like.) Each spring cylinder 7, 8 or 9 represents a control point for the radial seal 4. Instead of the spring cylinder 7, 8 and 9 can also be worked with counterweights. The radial seal 4 is formed in the radial direction with joints 41 and 42, which divide the radial seal 4 into several sections. The radial seal 4 can thus adapt to thermally induced rotor deformations. Alternatively, it is possible to perform the radial seal 4 jointless and flexible. Between the radial seal 4 and the upper end face of the rotor 2 there is a sealing gap S with the smallest possible gap. Between the radial seal 4 and the housing wall of the rotor housing 3, a sealing or expansion sleeve (see reference numeral 10 in the lower heat exchanger area) can be arranged, which compensates relative movements of the radial seal 4 relative to the housing wall.

Die Umfangsdichtung 5 ist als kreisringförmiger Dichtrahmen ausgeführt und mit mehreren in Umfangsrichtung gleichmäßig verteilten Stellgliedern oder Federzylindern 11 am Rotorgehäuse 3 befestigt bzw. abgehangen. Die Umfangsdichtung 5 kann segmentiert, mit Gelenken oder gelenklos und flexibel ausgeführt sein. In dem gezeigten Ausführungsbeispiel dichtet die Umfangsdichtung 5 bzw. der Dichtrahmen gegen einen vom Rotorkörper radial nach außen vorstehenden Rotorflansch 6 ab. Zwischen der Umfangsdichtung 5 und dem Rotorflansch 6 des Rotors 2 besteht ebenfalls ein Dichtspalt mit einem möglichst geringen Spaltmaß. Jeder Federzylinder 11 repräsentiert einen Stellpunkt für die Umfangsdichtung 5, wobei die Umfangsdichtung 5 bspw. infolge eines Gewichtsüberschusses (Gewichtskraft abzgl. Stellkraft in den Federzylindern 11) an den Rotorflansch 6 angedrückt wird.The peripheral seal 5 is designed as an annular sealing frame and fastened or suspended with a plurality of circumferentially uniformly distributed actuators or spring cylinders 11 on the rotor housing 3. The peripheral seal 5 can be segmented, executed with joints or jointless and flexible. In the embodiment shown seals the circumferential seal 5 and the Sealing frame against a radially outwardly projecting from the rotor body rotor flange 6 from. Between the circumferential seal 5 and the rotor flange 6 of the rotor 2 there is likewise a sealing gap with the smallest possible gap. Each spring cylinder 11 represents a control point for the peripheral seal 5, wherein the peripheral seal 5, for example, is pressed against the rotor flange 6 as a result of a weight excess (weight force minus the actuating force in the spring cylinders 11).

Um unabhängig von thermisch bedingten Rotorverformungen einen definierten Dichtspalt zwischen der Umfangsdichtung 5 und dem Rotorflansch 6 zu gewährleisten, ist die Umfangsdichtung 5 mittels einer Vielzahl von Laufrollen 12 am zum Rotor 2 gehörenden Rotorflansch 6 abgestützt. Bevorzugt ist zumindest im Bereich eines jeden Stellpunktes eine Laufrolle 12 vorgesehen. Hierdurch behält im Betrieb die Umfangsdichtung 5 einen konstanten Abstand zum Rotorflansch 6 und wird gleichzeitig zumindest den axialen Rotorverformungen nachgeführt.In order to ensure a defined sealing gap between the circumferential seal 5 and the rotor flange 6 irrespective of thermally induced rotor deformations, the circumferential seal 5 is supported by means of a plurality of rollers 12 on the rotor flange 6 belonging to the rotor 2. Preferably, a roller 12 is provided at least in the region of each control point. As a result, the circumferential seal 5 maintains a constant distance to the rotor flange 6 during operation and at the same time tracks at least the axial rotor deformations.

In dem in Fig. 1 gezeigten Ausführungsbeispiel sind die Laufrollen 12 in einer Ausnehmung in der Umfangsdichtung 5 angeordnet und bevorzugt darin auch drehbar gelagert (bspw. mittels einer Achse). Beim Drehen des Rotors 2 rollen die Laufrollen 12 auf einer am Rotorflansch 6 befestigten Verschleißplatte 14 ab. Bevorzugt ist die Verschleißplatte 14 in Umfangsrichtung segmentiert ausgebildet. Eine solche Verschleißplatte kann auch an einer korrespondierenden Rollfläche in der Umfangsdichtung 5 vorgesehen sein. Ebenso ist denkbar, dass die Laufrollen 12 sandwichartig zwischen zwei in axialer Richtung a zueinander beabstandeten Verschleißplatten geführt sind. Bei der Auslegung und/oder Einstellung (Justage) der Federzylinder 11 (evt. auch der Gegengewichte, falls mit solchen gearbeitet wird) sollte allgemein darauf geachtet werden, dass der Andruck zwischen den Laufrollen 12 und den korrespondierenden Rollflächen gering gehalten wird. Dies gelingt z. B. dadurch, dass die oberen Federzylinder 11 die Gewichtslast der Umfangsdichtung 5 im Wesentlichen aufnehmen oder zumindest reduzieren.In the in Fig. 1 Shown embodiment, the rollers 12 are arranged in a recess in the peripheral seal 5 and preferably also rotatably mounted therein (eg. By means of an axis). When rotating the rotor 2, the rollers 12 roll on a wear plate 14 attached to the rotor flange 6. Preferably, the wear plate 14 is formed segmented in the circumferential direction. Such a wear plate may also be provided on a corresponding rolling surface in the circumferential seal 5. It is also conceivable that the rollers 12 are guided sandwiched between two in the axial direction a spaced apart wear plates. In the design and / or adjustment (adjustment) of the spring cylinder 11 (possibly also the counterweights, if used with such) should generally be taken to ensure that the pressure between the rollers 12 and the corresponding rolling surfaces is kept low. This succeeds z. B. in that the upper spring cylinder 11, the weight load of the circumferential seal 5 substantially absorb or at least reduce.

Bei dem in Fig. 1 gezeigten Ausführungsbeispiels ist sowohl an der oberen Stirnseite als auch an der unteren Stirnseite des Rotors 2 eine mechanische Kopplung der Radialdichtungen 4 mit den Umfangsdichtungen 5 vorgesehen, wozu die Umfangsdichtungen 5 und die Radialdichtungen 4 kraftschlüssig miteinander verbunden sind. Dies führt dazu, dass die Radialdichtungen 4 der zwangsgeführten Bewegung der Umfangsdichtungen 5 in axialer Richtung a folgen, wozu die Radialdichtungen 4 in Axialrichtung a beweglich gelagert sind. Hierdurch wird die Abdichtung des Rotors 2 deutlich verbessert und Leckagen werden erheblich reduziert.At the in Fig. 1 shown embodiment, a mechanical coupling of the radial seals 4 with the peripheral seals 5 is provided both on the upper end side and on the lower end side of the rotor 2, to which the peripheral seals 5 and the radial seals 4 are non-positively connected. As a result, the radial seals 4 follow the positively guided movement of the circumferential seals 5 in the axial direction a, for which purpose the radial seals 4 are movably mounted in the axial direction a. As a result, the sealing of the rotor 2 is significantly improved and leaks are significantly reduced.

Fig. 2 zeigt ein Beispiel, bei dem abweichend zum ersten Ausführungsbeispiel der Fig. 1 die an der Umfangsdichtung 5 befestigten Laufrollen 12 zwischen zwei axial beabstandeten Rotorflanschen 61 und 62 mit entsprechenden Rollflächen geführt sind. Hierdurch wird eine "direkte" Zwangsführung für die Umfangsdichtung 5 ermöglicht. Im Übrigen gelten die Erläuterungen zum ersten Ausführungsbeispiel der Fig. 1. Fig. 2 shows an example in which, unlike the first embodiment of the Fig. 1 attached to the peripheral seal 5 rollers 12 between two axially spaced Rotor flanges 61 and 62 are guided with corresponding rolling surfaces. As a result, a "direct" positive guidance for the peripheral seal 5 is made possible. Otherwise, the explanations concerning the first exemplary embodiment of FIG Fig. 1 ,

Bei dem in Fig. 3 gezeigten zweiten Ausführungsbeispiel ist ebenfalls eine mechanische Kopplung der Umfangsdichtungen 5 mit den Radialdichtungen 4 vorgesehen. Hierzu sind die Umfangsdichtungen 5 jeweils mit einem radial verlaufenden Stellbalken 16 verbunden, der über mehrere Stellglieder 17 eine Verstellung der betreffenden Radialdichtung 4 (an der selben Rotorseite) in Axialrichtung a herbeiführt. D. h., die zwangsgeführte Bewegung einer Umfangsdichtung 5 wird entsprechend den Hebelverhältnissen auf die betreffende Radialdichtung 4 bzw. auf deren einzelnen Abschnitte übertragen, wozu die Radialdichtungen 4 in Axialrichtung a beweglich gelagert oder z. B. auch flexibel ausgebildet sind. Die radial verlaufenden Stellbalken 16 sind im Inneren des Rotorgehäuses 3 angeordnet. Ebenso könnten die Stellbalken 16 auch außerhalb des Rotorgehäuses 3 angeordnet sein.At the in Fig. 3 shown second embodiment, a mechanical coupling of the circumferential seals 5 is also provided with the radial seals 4. For this purpose, the circumferential seals 5 are each connected to a radially extending adjusting bar 16, which brings about a plurality of actuators 17, an adjustment of the respective radial seal 4 (on the same rotor side) in the axial direction a. D. h., The positively driven movement of a peripheral seal 5 is transmitted according to the lever ratios to the relevant radial seal 4 and on the individual sections, including the radial seals 4 movably mounted in the axial direction or z. B. are also flexible. The radially extending adjusting bars 16 are arranged in the interior of the rotor housing 3. Likewise, the adjusting bars 16 could also be arranged outside the rotor housing 3.

Fig. 4 zeigt ein drittes Ausführungsbeispiel, bei dem auch die Radialdichtungen 4 mittels Laufrollen 18 auf den Stirnseiten des Rotors 2 abgestützt sind. Auf diese Weise können die Radialdichtungen 4 im Betrieb mit konstantem Abstand zu den Stirnseiten des Rotors 2 zwangsgeführt und den axialen Rotorverformungen fortwährend nachgeführt werden. Die Laufrollen 18 sind im Bereich der Stellpunkte bzw. Federzylinder 7, 8 und 9 angeordnet. An den Stirnseiten des Rotors 2 sind korrespondierende Rollflächen ausgebildet. Diese Rollflächen können an Verschleißplatten 19 ausgebildet sein, wie beispielhaft für die untere, radial innere Laufrolle 18 dargestellt. Fig. 4 shows a third embodiment in which the radial seals 4 are supported by means of rollers 18 on the end faces of the rotor 2. In this way, the radial seals 4 can be forcibly guided in operation at a constant distance to the end faces of the rotor 2 and the axial rotor deformations are constantly updated. The rollers 18 are arranged in the region of the control points or spring cylinders 7, 8 and 9. At the end faces of the rotor 2 corresponding rolling surfaces are formed. These rolling surfaces may be formed on wear plates 19, as exemplified for the lower, radially inner roller 18.

Es soll ausdrücklich darauf hingewiesen werden, dass die Merkmale der zuvor im Zusammenhang mit den Figuren erläuterten Ausführungsbeispiele miteinander kombiniert werden können, sofern sich hieraus kein technischer Widerspruch ergibt.It should be expressly pointed out that the features of the previously explained in connection with the figures embodiments can be combined with each other, provided that there is no technical contradiction.

Claims (7)

  1. A regenerative heat exchanger (1) with a heat storage configured as a rotor (2) which is mounted so as to be rotatable about a central rotational axis (A) and transmits heat of at least one gas volume flow (V) passing through the rotor (2) onto at least one other gas volume flow passing through the rotor (2), and with a sealing system for the rotor (2), the sealing system comprising at least one seal (4, 5) which is fixed in relation to the rotor (2) and is, on the one hand, pressed against the rotor (2) and is, on the other hand, supported on the rotatable rotor (2) by a plurality of rollers (12) which are rotatably mounted by means of axles, the rollers (12) rolling off on at least one corresponding rolling surface on the rotor (2),
    characterized in that
    the rollers (12) are arranged in the seal (4, 5), and
    that at least one of the rolling surfaces, i.e., a rolling surface in the seal or said rolling surface on the rotor (2), is formed on an exchangeable wear plate (14, 19).
  2. The regenerative heat exchanger (1) according to claim 1,
    characterized in that
    the individual rollers (12) are arranged at least in the region of actuating points of the seal (4, 5).
  3. The regenerative heat exchanger (1) according to any one of the preceding claims,
    characterized in that
    the seal supported by means of rollers (12) is a circumferential seal (5) and/or a radial seal (4).
  4. The regenerative heat exchanger (1) according to claim 3,
    characterized in that
    the supported circumferential seal (5) is coupled with a radial seal (4), as a result of which said radial seal (4) is co-moved in axial direction (a) during axial movement of the circumferential seal (5).
  5. The regenerative heat exchanger (1) according to claim 4,
    characterized in that
    the coupling between the circumferential seal (5) and the radial seal (4) occurs by a mechanical actuating mechanism which transmits the axial movements of the circumferential seal (5) by means of an actuating bar (16) onto the radial seal (4).
  6. The regenerative heat exchanger (1) according to claim 5,
    characterized in that
    the actuating bar (16) is arranged within a rotor housing (3) enclosing the rotor (2).
  7. The regenerative heat exchanger (1) according to any one of the preceding claims,
    characterized in that
    at least one sealing collar (10) is arranged between the seal (4, 5) and the rotor housing (3).
EP10015001.0A 2010-11-25 2010-11-25 Regenerative heat exchanger with forced rotor seal Not-in-force EP2458315B1 (en)

Priority Applications (4)

Application Number Priority Date Filing Date Title
EP10015001.0A EP2458315B1 (en) 2010-11-25 2010-11-25 Regenerative heat exchanger with forced rotor seal
US13/303,127 US20120298326A1 (en) 2010-11-25 2011-11-22 Regenerative heat exchanger with a rotor seal with forced guidance
RU2011148135/06A RU2594034C2 (en) 2010-11-25 2011-11-25 Regenerative heat exchanger with forced input of rotor seal
CN201110461849.5A CN102767981B (en) 2010-11-25 2011-11-25 There is the regenerative heat exchanger of mandatory guidance type rotor seal part

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
EP10015001.0A EP2458315B1 (en) 2010-11-25 2010-11-25 Regenerative heat exchanger with forced rotor seal

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EP2458315A1 EP2458315A1 (en) 2012-05-30
EP2458315B1 true EP2458315B1 (en) 2017-01-04

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US (1) US20120298326A1 (en)
EP (1) EP2458315B1 (en)
CN (1) CN102767981B (en)
RU (1) RU2594034C2 (en)

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Publication number Publication date
CN102767981B (en) 2016-06-29
EP2458315A1 (en) 2012-05-30
RU2594034C2 (en) 2016-08-10
RU2011148135A (en) 2013-05-27
CN102767981A (en) 2012-11-07
US20120298326A1 (en) 2012-11-29

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