EP2023070B1 - Regenerativ-Wärmeaustauscher und Radialdichtung zur Verwendung für einen solchen sowie Verfahren zum Trennen von gasförmigen Medien in einem regenerativ-Wärmeaustauscher - Google Patents

Regenerativ-Wärmeaustauscher und Radialdichtung zur Verwendung für einen solchen sowie Verfahren zum Trennen von gasförmigen Medien in einem regenerativ-Wärmeaustauscher Download PDF

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Publication number
EP2023070B1
EP2023070B1 EP07014528A EP07014528A EP2023070B1 EP 2023070 B1 EP2023070 B1 EP 2023070B1 EP 07014528 A EP07014528 A EP 07014528A EP 07014528 A EP07014528 A EP 07014528A EP 2023070 B1 EP2023070 B1 EP 2023070B1
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EP
European Patent Office
Prior art keywords
heat storage
storage body
radial seal
heat exchanger
radially
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.)
Active
Application number
EP07014528A
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German (de)
English (en)
French (fr)
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EP2023070A1 (de
Inventor
Volker Halbe
Heinz-Günter Raths
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Balcke Duerr GmbH
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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
Priority to AT07014528T priority Critical patent/ATE508337T1/de
Priority to SI200730685T priority patent/SI2023070T1/sl
Application filed by Balcke Duerr GmbH filed Critical Balcke Duerr GmbH
Priority to PT07014528T priority patent/PT2023070E/pt
Priority to EP07014528A priority patent/EP2023070B1/de
Priority to DK07014528.9T priority patent/DK2023070T3/da
Priority to PL07014528T priority patent/PL2023070T3/pl
Priority to DE502007007132T priority patent/DE502007007132D1/de
Priority to RU2008130532/06A priority patent/RU2395051C2/ru
Priority to US12/178,067 priority patent/US8561672B2/en
Priority to CN2008102147448A priority patent/CN101373122B/zh
Priority to ZA200806464A priority patent/ZA200806464B/en
Publication of EP2023070A1 publication Critical patent/EP2023070A1/de
Priority to HK09107562.4A priority patent/HK1128191A1/xx
Application granted granted Critical
Publication of EP2023070B1 publication Critical patent/EP2023070B1/de
Active legal-status Critical Current
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    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F28—HEAT EXCHANGE IN GENERAL
    • F28D—HEAT-EXCHANGE APPARATUS, NOT PROVIDED FOR IN ANOTHER SUBCLASS, IN WHICH THE HEAT-EXCHANGE MEDIA DO NOT COME INTO DIRECT CONTACT
    • F28D19/00—Regenerative heat-exchange apparatus in which the intermediate heat-transfer medium or body is moved successively into contact with each heat-exchange medium
    • F28D19/04—Regenerative 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
    • F28D19/047—Sealing means

Definitions

  • the invention relates to a regenerative heat exchanger according to the preamble of claim 1 and a radial seal for use in a regenerative heat exchanger according to the preamble of claim 8. Furthermore, the invention relates to a method for separating gaseous media in a regenerative heat exchanger according to the preamble of Claim 10.
  • a regenerative heat exchanger is eg off DE 111 3534 known.
  • a normally cylindrical heat storage body which is designed for the flow of gaseous media.
  • These heat storage bodies are divided into sectors by radially extending walls, hereinafter called sector walls.
  • the sector walls extend substantially continuously from the longitudinal axis of the heat storage body to the heat storage edge and are aligned parallel to the longitudinal axis or lie in a plane therewith.
  • the sector walls are formed continuously from one heat storage end face to the other.
  • the sector walls are usually evenly distributed in the heat storage body, so that result in sectors of the same shape and the same volume.
  • the heat storage body partially have diameters of 20 m and more, the sectors are subdivided for construction reasons by the introduction of additional walls in several, permeable by gaseous media heat storage chambers, often a plurality of heat storage chambers within a sector in heat storage body radial direction are arranged one behind the other.
  • recuperative or regenerative heat exchanger systems are available for exchanging heat between gaseous media.
  • the flow of the heat-emitting medium is applied directly to one or more streams of heat-absorbing media and the heat is transferred directly through a partition wall.
  • regenerators is transfer the heat by means of a heat-storing intermediate medium.
  • heat-storing intermediate media are arranged in regenerative heat exchangers in the heat storage chambers of the heat storage body. These are often layered sheet steel layers, which can be enamelled if necessary. These are often designed as basket systems, which can then be used as a whole in a heat storage chamber and fill them. Alternatively, some ceramic bodies or heating surfaces made of plastic are used as heat-storing intermediate media.
  • the heat storage body is either fixed or rotatable about its longitudinal axis, wherein in the former case of a "stator" and in the latter case of a "rotor” speaks.
  • the rotor housing including the gas duct connections attached thereto, is fixed, so that the rotor rotates through the different gas flows.
  • so-called rotary hoods are arranged. In both variants, therefore, the various areas of the heat storage body alternately flows through all the existing gas flows.
  • the heat-emitting gaseous medium flows through the heat storage body from one end face to the other and thereby heats the heating elements arranged therein in the individual heat storage chambers, which store this heat. Further, one or more heat-receiving gaseous media flow through the heat storage body, also from one end face to the other.
  • the heated heating elements are flowed through by the cold gas streams and thus heat them.
  • a hot, heat-emitting exhaust gas flow and a cold, heat-absorbing air flow are often passed through the heat storage body. This is the process of air preheating (Luvos). Subsequently, the heated air is supplied to a furnace and accordingly referred to as combustion air or combustion air.
  • combustion air or combustion air The increased heat of combustion air by the heat exchanger substituted parts of the energy contained in the fuel, whereby the amount of fuel required for the firing is reduced. Consequently, the amount of CO 2 released during firing is also reduced.
  • heat exchangers can also be used for gas preheating (Gavos).
  • heat exchangers which are designed as so-called DeSOx systems, for example, a hot raw gas with a high SOx content is cooled and heated a clean gas with a low SOx content.
  • DeNOx plants in turn, a hot clean gas with a low NOx content is cooled and a crude gas is heated with a high NOx content.
  • the heat-emitting gas stream and the one or more heat-absorbing gas streams according to the countercurrent principle are conducted opposite one another through the heat storage body.
  • the heat-absorbing gas is led out of the heat storage body.
  • the hot side of the heat exchanger On the opposite side, the cooled, heat-emitting gas is blown out and the still cool heat-absorbing gas is blown. Accordingly, this is the so-called cold side.
  • a regenerative heat exchanger which is designed, for example, for air preheating, it therefore has a casein inlet and an air outlet on its hot side and a gas outlet and an air inlet on its cold side.
  • the exhaust gas thus flows through an exhaust gas region which extends from the hot to the cold side of the heat exchanger, while the combustion air flows through a combustion air region which extends from the cold to the hot side.
  • the division of the heat storage body into heat storage chambers is provided to prevent the various gas streams from mixing with each other. Through the various chambers, separated from each other, simultaneously heat-emitting gas or heat-absorbing gas out. In order to ensure a flow through or around the heat storage intermediate chambers located in the heat storage chambers, the heat storage chambers are open at the end faces of the heat storage body.
  • a radial seal is often formed as a bar or bar and extends orthogonal to the axis of rotation or longitudinal axis of the heat storage body extending over the diameter of the heat storage body. In this case, it is usually flat and runs through the heat storage body center. It is often made of metal or other materials such as e.g. Made of plastic and may be formed in one piece or in several pieces.
  • the radial seal may be designed to be adjustable in the direction of the heat storage body longitudinal axis, that is to say away from the heat storage body or towards the heat storage body. Frequently, the radial seals are performed in this way to compensate for heat-induced deformation of the heat storage body can.
  • the sealing gap between the radial seal and the heat storage body face can be minimized to leakage between the various To reduce gas flows.
  • the maintenance of a minimum sealing gap is necessary to ensure the rotatability of heat storage body and radial seal relative to each other.
  • the radial seal consists of two or more seal arms, with a seal arm extending substantially from the axis of rotation to the outer edge of the heat storage body.
  • the number of seal arms usually depends on the number of different gas streams present. Flow, for example, in a heat exchanger using a rotor as a heat storage body, two gas flows through the rotor, two sealing arms are provided both on the cold and on the hot side, with three gas flows three sealing arms, etc. in that the radial direction relative is arranged stationary to the rotational movement of the rotor, the openings of the heat storage chambers rotate under the radial seal therethrough. In one complete revolution of the rotor, each point of the end faces of the rotor is once below or above each seal arm.
  • the radial seals have been formed in known regenerative heat exchangers so that in each rotational position, that is, any position of the heat storage body and radial seal to each other, a sector wall below and above a sealing arm.
  • the various gas areas for example, the combustion air area and the exhaust gas area, always separated by a radially extending from the axis of rotation to the heat storage body edge sector wall.
  • the continuous closing and opening of the heat storage chambers creates permanent, mechanical vibrations. These are caused by the different pressure conditions that occur when opening and closing the heat storage chambers and have a pulsating effect on the radial seals. This process is also referred to as "pumping" the seals.
  • the intensity of this pumping and thus also the intensity of the action on the radial seal is dependent on the existing pressure differences between the different Casströmen and the surface of the seals. As this process is repeated continuously, the mean sealing gap height increases.
  • the wear of the radial seals and the end faces of the heat storage body is considerably increased. These factors result in an increase in leakage.
  • a heat exchanger is known in which the radial seal identifies two dovetail-shaped sealing arms.
  • a simultaneous coverage of all chambers or heat storage chambers is achieved, which are arranged in the radial direction of a sector of the rotor formed as a heat storage body.
  • Such simultaneous coverage of the chambers is also apparent from the patents DE 11 13 534 B . GB 676,129 A . US 3,968,569 A and WO 93/19339 A known. Again, the adverse pumping of the seals occurs, as described above.
  • the invention is therefore based on the object to show ways how the pumping of the seals and thus the leakage between the different gas areas, as well as the wear on the radial seals and on the end faces of a heat storage body can be reduced.
  • the regenerative heat exchanger thus has a cylindrical heat storage body, which is divided by a plurality of radial sector walls into sectors, wherein in each sector at least two radially arranged in succession heat storage chambers are provided.
  • the heat storage chambers are designed to flow through the gaseous media and accordingly have openings in the region of the end faces of the heat storage body.
  • the radial seal is designed so that it covers each heat storage chamber opening alternately completely upon rotation of the rotor or the rotary hoods.
  • the openings of the heat storage chambers are constantly closed and reopened during operation, each opening is covered at least once from each radial seal at a complete rotor circulation or rotary hood circulation.
  • the heat chambers are continuously formed from one end face to the other, it is expedient to shape and arrange the radial seals on the two end faces in such a way that both openings of a chamber are closed and opened substantially simultaneously and thus this chamber is completely closed with a corresponding rotational position. This is advantageously achieved in that the arranged on the two end faces, opposite radial seals are formed substantially uniform and congruent.
  • the radial seal is now designed so that it at least partially covers the opening of at least one of these heat storage chambers of the radially successively arranged heat storage chambers of a sector in each rotational position, that is, in any position of heat storage body and radial seal.
  • the basic idea of the invention is thus to arrange the opening surfaces of the heat storage chambers arranged one behind the other within a sector and the covering surface of the radial seal relative to one another such that never all radially consecutively arranged heat storage chambers of a sector at the same time and thus at no angular position of the rotor or the rotary hood are covered by the radial seal.
  • this relative arrangement can be achieved both by a corresponding design of the radial seal and by a corresponding design of the heat storage chamber geometries.
  • the geometries of the sector walls and the heat storage chambers are maintained and the adjustment is made in the radial seal.
  • all geometries that produce the effect described above can be used for the radial seal.
  • the radial seal is designed such that it completely covers at most one heat storage chamber of the heat storage chambers arranged one behind the other of a sector at any given time, that is, at each rotational angle position of the rotor or the rotary hoods.
  • each radial seal comprises at least two sealing arms.
  • at least two sealing arms of the radial seal which extend substantially from the longitudinal axis radially outwardly to the heat storage body edge, at least one sealing arm is formed asymmetrically.
  • the geometry of the at least one Sealing arm is shaped such that the surface of the sealing arm is not symmetrical in a plan view. This excludes both axis symmetry and point symmetry. It can therefore find no axis or no point around which the Dichtarm Structure can be mirrored. Such a design can be achieved particularly well a time-delayed coverage of the individual heat storage chambers.
  • the individual sealing arms of the radial seal are subdivided into sealing arm segments.
  • the individual segments are arranged one behind the other in the radial direction and close directly to each other, so that they assemble into a seal arm.
  • the two outer edges of a segment are each formed substantially linear.
  • the outer edges of adjacent Dichtungsarmsegmente offset from each other and alternatively or additionally angled with respect to their adjacent outer edges.
  • the outer edges are considered on the same seal arm side.
  • the heat storage bodies are formed so that they have a plurality of coaxial annular walls. These annular walls are often cylindrical and have the heat storage body longitudinal axis as a common axis. Thus, the annular walls cut through the individual sectors and divide them into subsectors in the radial direction. These subsectors may correspond to the dimensions of a heat storage chamber. However, it is also possible in principle to subdivide the subsectors further into several heat storage chambers. When a heat storage body is subdivided by such annular walls into subsectors, it is preferred that the individual seal arm segments of the seal arms be configured to extend radially across substantially one subsector or a plurality of adjacent subsectors.
  • seal arm segment Corresponds to a subsector of a heat storage chamber, it is appropriate that over this subsector extending seal arm segment is formed to cover the chamber. It is thereby achieved that the edge offset between two sealing arm segments, or the point of intersection between two mutually angled outer edges of two adjacent sealing elements, is arranged substantially over a region against which two heat storage chambers or two subsectors abut one another.
  • the formation of the individual sealing arm segments can be better adapted to individual sub-sectors, so that the covering order of the individual sub-sectors or heat-storing chambers can be optimized during operation, whereby the oscillation volume is further reduced overall.
  • At least one seal arm is divided into three seal arm segments, wherein the inner segment closest to the axis of rotation is cone-shaped.
  • the cone-shaped inner segment is aligned so that it widens substantially in the radial direction.
  • the adjoining middle segment tapers in the radial direction and preferably at least one edge of the middle segment is offset relative to the adjacent edge of the inner segment in the heat storage body circumferential direction. Due to the tapering of the middle segment in the radial direction, the edges of the middle segment are angled with respect to the inner cone-shaped outwardly widening segment.
  • the cross-sectional area of the outer segment widens again in the radial direction and its edges are thus arranged angled relative to those of the middle segment.
  • the radial seal is formed so that the inflow and outflow surfaces are substantially equal for the respective gaseous media.
  • the inflow and outflow surfaces of the various gaseous media may further vary in size and may be adapted to the specific requirements of each such, e.g. maximum permissible pressure losses, to be adjusted.
  • the existing of at least two sealing arms radial seal thus has at least one sealing arm, which is formed asymmetrically. Such a design reduces the amount of pumping acting on the seals.
  • the method therefore consists of alternately completely covering the openings of the various heat storage chambers in the heat exchanger operation in the case of an already described heat storage body of a regenerative heat exchanger with sectors and in the radial direction one behind the other, throughflowable heat storage chambers for separating the different gas flows. That is, the heat storage chambers are permanently closed and reopened. As a result, a separation between the individual gas streams is achieved.
  • the heat storage chambers are covered in such a way that in the case of heat storage chambers arranged radially behind one another within a sector in each operating state of the heat exchanger at least one heat storage chamber is at most partially covered.
  • the opening of at most one of these heat storage chambers is completely covered in each operating state.
  • Fig. 1 shows a plan view of a rotor 10 of a regenerative heat exchanger.
  • a shaft 11 around which the rotor 10 rotates.
  • the rotation of the rotor 10 by means of a motor drive (not shown here).
  • a motor drive (not shown here).
  • the sector walls 12 are rectilinear and extend from one end face of the rotor 10 to the other. All sector walls 12 have a common point of intersection in the center 14 of the rotor 10.
  • the sector walls 12 are distributed uniformly and circumferentially in the rotor 10, so that each two adjacent sector walls 12 form equal sectors 15. Overall, the rotor 10 is divided into twenty equal sectors 15. A sector 15 is thus limited on its two sides by a respective sector wall 12, on its inner side by the shaft 11 and on its outer side by the edge 13 of the rotor 10, which is designed as a cylindrical outer jacket.
  • annular walls 16 are disposed within the rotor, which are each formed circumferentially and in itself closed.
  • the annular walls 16 are arranged coaxially with each other, wherein the common axis is the axis of rotation passing through the center 14.
  • the annular walls 16 are approximately cylindrical, wherein the portion of an annular wall 16 between two sector walls 12 is formed in each case rectilinear and is slightly angled relative to the adjacent annular wall portions.
  • the annular walls 16 extend through the entire rotor 10 from one end face to the other.
  • Each of the four outer subsectors 17 of each sector 15 is divided by a radially extending partition wall 18 into two heat storage chambers 19, with the four outer subsectors 17 extending through the approximately center Between each wall 18 each sub-sector 17 two approximately equal heat storage chambers 19 result.
  • the use of partitions 18 is not mandatory and takes place in the present example, for design reasons.
  • the inner two subsectors 17 are not further subdivided, so that these two subsectors 17 each form a heat storage chamber 19.
  • the number of heat storage chambers per sector can be varied and usually results as a function of the size of the particular heat storage body present.
  • the heat storage chambers 19 in the present embodiment are filled with heating elements (not shown here), such as steel sheets.
  • a radial seal 20 is arranged, which extends in the radial direction of the rotor from one side to the other.
  • the radial seal 20 is enclosed in a likewise on the rotor front side
  • the radial seal 20 consists of an upper seal arm 201 and a lower seal arm 202, which abut each other in the region of the horizontal, passing through the center 14 of the rotor 10 center line 23.
  • the radial seal 20, consisting of the two sealing arms 201 and 202 divides the rotor 10 into two gas areas, one to the right of the radial seal 20 and one to the left thereof.
  • heat can be transferred from a gaseous medium to another.
  • the radial seal 20 and the circumferentially enclosing circumferential seal 21 are arranged stationary relative to the rotational movements of the rotor 10, so that the rotor 10 rotates below the radial seal 20.
  • the upper seal arm 201 is formed in accordance with the prior art known radial seals while the lower seal arm 202 is formed in accordance with the present invention.
  • Sealing arm 201 is shown here in accordance with embodiments known from the prior art in order to be able to illustrate the differences between the radial seal according to the invention and the prior art more clearly.
  • a regenerative heat exchanger according to the invention therefore of course all sealing arms are formed according to the seal arm 202.
  • Both sealing arms 201, 202 each have an inner, semi-annular part 2011, 2021 which abut each other and thus form a complete ring with a circular base. In the middle of the ring, a recess for the shaft 11 is provided.
  • the semi-ring 2011 of the sealing arm 201 is adjoined by a sealing web 2012 which extends linearly and radially outwards and which extends from the half-ring 2011 to the rotor rim 13.
  • the sealing bar 2012 has over its entire. Course a constant width.
  • the seal arm 201 is formed symmetrically, wherein the center line 14 extending vertically through the center 14 of the rotor 10 at the same time also forms its mirror axis.
  • the sealing arm 201 covers from the outer four subsectors 17 of a sector 15 each from the right one behind the other arranged heat storage chambers 19, and the two inner heat storage chambers 19.
  • the seal arm 201 covers from the outer four subsectors 17 of a sector 15 each from the right one behind the other arranged heat storage chambers 19, and the two inner heat storage chambers 19.
  • the sealing arms are designed so that they do not cover all in the rotor radial direction one behind the other heat storage chambers 19 of a sector 15 at a given time. Whether, as in the exemplary embodiment shown here, in addition to the arrangement of the heat storage chambers 19 arranged one behind the other in the rotor radial direction, some heat storage chambers 19 within a sector 15 are also partially arranged next to each other, is irrelevant in this context.
  • the right heat storage chambers 19 of the outer four subsectors 17 of a sector 15 and the two inner heat storage chambers 19 and subsectors 17 of the same sector 15 and also the left heat storage chambers 19 of the four outer subsectors 17 together with the two inner heat storage chambers are located one behind the other 19th
  • an inner arm segment 2022 adjoins the half-ring 2021. This is cone-shaped, wherein the narrow side rests against the half-ring 2021, so that the inner segment 2022 widens in the radial direction. In the radial direction, the seal arm segment 2022 extends to the second annular wall 16, seen from the inside outwards.
  • the inner seal arm segment 2022 is formed, the part of the first sub-sector 17 and the second sub-sector, seen from the inside out, not covered by the half-ring 2021 Cover 17 of each ring sector 15 with appropriate rotor position.
  • the inner seal arm segment 2022 is followed in the radial direction by a middle seal arm segment 2023.
  • the right outer edge of the middle seal segment 2023 is slightly offset from the right outer edge of the inner seal arm segment 2022.
  • the middle seal arm segment 2023 is adjoined by an outer and last seal arm segment 2024 which extends to the edge of the rotor 13.
  • the outer edges are linear. They connect directly to the outer edges of the middle seal arm 2023 and are each angled towards the left.
  • the cross-sectional area of the outer sealing arm 2024 expands slightly, so that its greatest width is in the area of the rotor rim 13.
  • the outer seal arm segment 2024 extends from the third annular wall 16 to the rotor edge 13 and thus extends approximately over three sub-sectors 17 in the radial direction.
  • the seal arm 202 is asymmetrical.
  • the geometric design of the sealing arm 202 has the effect that, in each position of the rotor 10, at least one of the heat storage chambers 19 of a sector 15 arranged one behind the other is not or only partially covered by the sealing arm 202.
  • the two outer located below the seal arm 202 successively arranged heat storage chambers 19 are only partially covered.
  • the other four heat storage chambers 19, which are also below the arm 202 are completely covered.
  • the rotor 10 would rotate in a clockwise direction, first the middle two of the covered heat storage chambers 19 would be opened before the two outer, partially covered heat storage chambers 19 would be completely covered. Nevertheless, each heat storage chamber 19 is once completely covered by the seal arm 202 at each rotor revolution, so that a separation of the two gas regions from each other is always ensured.
  • Fig. 2 the rotor is off Fig. 1 shown in a perspective side view. All walls, that is, the sector walls 12, the annular walls 16 and the intermediate walls 18; pass through the entire rotor 10 in the axial direction from one end face to the other.
  • Fig. 3 shows a plan view of a section of a heat storage body 10 of a regenerative heat exchanger.
  • the heat storage body 10 shown here is in contrast to the heat storage body of the Fig. 1 and 2 designed as a stator, ie it is stationary and thus fixed.
  • the structure of the stator 10, that is, the division into sectors, sub-sectors and heat storage chambers, is substantially equal to the structure of the rotor of the Fig. 1 and 2 .
  • two inventively designed radial sealing arms 202 are provided, which are respectively disposed above and below the stator 10 and adjacent thereto.
  • the seal arms 202 also have as the seal arm according to the invention from the Fig.
  • the sealing arms 202 are mounted on the underside of the outer edge of a rotary hood (not shown here) and rotate together with this around the center 14. At each end face of the stator 10, at least one rotary hood is arranged.
  • the central axes 2025 of the two sealing arms 202 intersect at the center 14 of the stator 10 at an angle of approximately 90 °. The area enclosed by this angle is covered by the rotary hoods.
  • sealing arms 202 are respectively arranged on the outer edges of the rotary hood, the regions lying outside the rotary hood are sealed off from the area enclosed by the rotary hood.
  • the alignment of the sealing arms 202 at an angle of 90 ° to each other is preferred for the embodiments with a stator as the heat storage body 10, since this configuration corresponds to the dimensions of the rotary hoods commonly used.
  • two rotary hoods are arranged axially symmetrical to one another in known embodiments on each end face, so that in these embodiments a total of four sealing arms 202 according to the invention are to be arranged on each end face.

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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)
  • Separation By Low-Temperature Treatments (AREA)
  • Air Supply (AREA)
  • Vaporization, Distillation, Condensation, Sublimation, And Cold Traps (AREA)
EP07014528A 2007-07-24 2007-07-24 Regenerativ-Wärmeaustauscher und Radialdichtung zur Verwendung für einen solchen sowie Verfahren zum Trennen von gasförmigen Medien in einem regenerativ-Wärmeaustauscher Active EP2023070B1 (de)

Priority Applications (12)

Application Number Priority Date Filing Date Title
SI200730685T SI2023070T1 (sl) 2007-07-24 2007-07-24 Regenerativni prenosnik toplote in radialno tesnilo za uporabo z njim kot tudi postopek ločevanja plinastih medijev v regenerativnem prenosniku toplote
PT07014528T PT2023070E (pt) 2007-07-24 2007-07-24 Permutador de calor regenerativo e vedante para utilização com o mesmo e processo de separação de meios gasosos num permutador de calor regenerativo
EP07014528A EP2023070B1 (de) 2007-07-24 2007-07-24 Regenerativ-Wärmeaustauscher und Radialdichtung zur Verwendung für einen solchen sowie Verfahren zum Trennen von gasförmigen Medien in einem regenerativ-Wärmeaustauscher
DK07014528.9T DK2023070T3 (da) 2007-07-24 2007-07-24 Regenerativ varmeveksler og radialtætning til anvendelse i en sådan samt fremgangsmåde til adskillelse af gasformige medier i en regenerativ varmeveksler
PL07014528T PL2023070T3 (pl) 2007-07-24 2007-07-24 Regeneracyjny wymiennik ciepła i uszczelka promieniowa do stosowania do takiego wymiennika ciepła oraz sposób oddzielania gazowych ośrodków w regeneracyjnym wymienniku ciepła
DE502007007132T DE502007007132D1 (de) 2007-07-24 2007-07-24 Regenerativ-Wärmeaustauscher und Radialdichtung zur Verwendung für einen solchen sowie Verfahren zum Trennen von gasförmigen Medien in einem regenerativ-Wärmeaustauscher
AT07014528T ATE508337T1 (de) 2007-07-24 2007-07-24 Regenerativ-wärmeaustauscher und radialdichtung zur verwendung für einen solchen sowie verfahren zum trennen von gasförmigen medien in einem regenerativ-wärmeaustauscher
US12/178,067 US8561672B2 (en) 2007-07-24 2008-07-23 Regenerative heat exchanger with a plurality of radial seals for separating gaseous media
RU2008130532/06A RU2395051C2 (ru) 2007-07-24 2008-07-23 Регенеративный теплообменник, радиальное уплотнение для такого теплообменника и способ разделения газообразных сред в регенеративном теплообменнике
CN2008102147448A CN101373122B (zh) 2007-07-24 2008-07-24 再生式换热器及其径向密封件及用于分离气态介质的方法
ZA200806464A ZA200806464B (en) 2007-07-24 2008-07-24 Regenerative heat exchanger, radial seal therefor and method of separating gaseous media therein
HK09107562.4A HK1128191A1 (en) 2007-07-24 2009-08-18 A regenerative heat exchanger and its radial seal and method for separating gaseous media

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
EP07014528A EP2023070B1 (de) 2007-07-24 2007-07-24 Regenerativ-Wärmeaustauscher und Radialdichtung zur Verwendung für einen solchen sowie Verfahren zum Trennen von gasförmigen Medien in einem regenerativ-Wärmeaustauscher

Publications (2)

Publication Number Publication Date
EP2023070A1 EP2023070A1 (de) 2009-02-11
EP2023070B1 true EP2023070B1 (de) 2011-05-04

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EP07014528A Active EP2023070B1 (de) 2007-07-24 2007-07-24 Regenerativ-Wärmeaustauscher und Radialdichtung zur Verwendung für einen solchen sowie Verfahren zum Trennen von gasförmigen Medien in einem regenerativ-Wärmeaustauscher

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US (1) US8561672B2 (xx)
EP (1) EP2023070B1 (xx)
CN (1) CN101373122B (xx)
AT (1) ATE508337T1 (xx)
DE (1) DE502007007132D1 (xx)
DK (1) DK2023070T3 (xx)
HK (1) HK1128191A1 (xx)
PL (1) PL2023070T3 (xx)
PT (1) PT2023070E (xx)
RU (1) RU2395051C2 (xx)
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US8505923B2 (en) * 2009-08-31 2013-08-13 Sealeze, A Unit of Jason, Inc. Brush seal with stress and deflection accommodating membrane
CN102200407B (zh) * 2011-07-09 2012-12-05 程爱平 回转式气气换热器无泄漏密封系统轴向隔离密封舱
CN102645116B (zh) * 2012-04-27 2014-04-23 中南大学 一种连续蓄热式热交换器
KR102343408B1 (ko) 2017-11-17 2021-12-27 주식회사 엘지화학 열 교환기

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CN101373122B (zh) 2012-07-18
PL2023070T3 (pl) 2011-10-31
SI2023070T1 (sl) 2011-09-30
RU2395051C2 (ru) 2010-07-20
RU2008130532A (ru) 2010-01-27
ATE508337T1 (de) 2011-05-15
CN101373122A (zh) 2009-02-25
DE502007007132D1 (de) 2011-06-16
HK1128191A1 (en) 2009-10-16
US20090056908A1 (en) 2009-03-05
US8561672B2 (en) 2013-10-22
PT2023070E (pt) 2011-06-30
EP2023070A1 (de) 2009-02-11
ZA200806464B (en) 2010-07-28

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