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EP0081551B1 - Revetement d'un foyer de section au moins approximativement circulaire - Google Patents

Revetement d'un foyer de section au moins approximativement circulaire Download PDF

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Publication number
EP0081551B1
EP0081551B1 EP82901961A EP82901961A EP0081551B1 EP 0081551 B1 EP0081551 B1 EP 0081551B1 EP 82901961 A EP82901961 A EP 82901961A EP 82901961 A EP82901961 A EP 82901961A EP 0081551 B1 EP0081551 B1 EP 0081551B1
Authority
EP
European Patent Office
Prior art keywords
sealing
lining
lining according
layers
sealing portions
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
Application number
EP82901961A
Other languages
German (de)
English (en)
Other versions
EP0081551A1 (fr
Inventor
Wolfgang Hermann
Bernhard RÜTER
Rainer Gorris
Herbert Nowak
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.)
Karrena GmbH
Rheinbraun AG
Original Assignee
Karrena GmbH
Rheinische Braunkohlenwerke AG
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 Karrena GmbH, Rheinische Braunkohlenwerke AG filed Critical Karrena GmbH
Publication of EP0081551A1 publication Critical patent/EP0081551A1/fr
Application granted granted Critical
Publication of EP0081551B1 publication Critical patent/EP0081551B1/fr
Expired legal-status Critical Current

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Classifications

    • C—CHEMISTRY; METALLURGY
    • C10—PETROLEUM, GAS OR COKE INDUSTRIES; TECHNICAL GASES CONTAINING CARBON MONOXIDE; FUELS; LUBRICANTS; PEAT
    • C10J—PRODUCTION OF PRODUCER GAS, WATER-GAS, SYNTHESIS GAS FROM SOLID CARBONACEOUS MATERIAL, OR MIXTURES CONTAINING THESE GASES; CARBURETTING AIR OR OTHER GASES
    • C10J3/00—Production of combustible gases containing carbon monoxide from solid carbonaceous fuels
    • C10J3/72—Other features
    • C10J3/78—High-pressure apparatus
    • C—CHEMISTRY; METALLURGY
    • C10—PETROLEUM, GAS OR COKE INDUSTRIES; TECHNICAL GASES CONTAINING CARBON MONOXIDE; FUELS; LUBRICANTS; PEAT
    • C10J—PRODUCTION OF PRODUCER GAS, WATER-GAS, SYNTHESIS GAS FROM SOLID CARBONACEOUS MATERIAL, OR MIXTURES CONTAINING THESE GASES; CARBURETTING AIR OR OTHER GASES
    • C10J3/00—Production of combustible gases containing carbon monoxide from solid carbonaceous fuels
    • C10J3/72—Other features
    • C10J3/74—Construction of shells or jackets
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23M—CASINGS, LININGS, WALLS OR DOORS SPECIALLY ADAPTED FOR COMBUSTION CHAMBERS, e.g. FIREBRIDGES; DEVICES FOR DEFLECTING AIR, FLAMES OR COMBUSTION PRODUCTS IN COMBUSTION CHAMBERS; SAFETY ARRANGEMENTS SPECIALLY ADAPTED FOR COMBUSTION APPARATUS; DETAILS OF COMBUSTION CHAMBERS, NOT OTHERWISE PROVIDED FOR
    • F23M5/00—Casings; Linings; Walls
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F27—FURNACES; KILNS; OVENS; RETORTS
    • F27D—DETAILS OR ACCESSORIES OF FURNACES, KILNS, OVENS OR RETORTS, IN SO FAR AS THEY ARE OF KINDS OCCURRING IN MORE THAN ONE KIND OF FURNACE
    • F27D1/00—Casings; Linings; Walls; Roofs
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F27—FURNACES; KILNS; OVENS; RETORTS
    • F27D—DETAILS OR ACCESSORIES OF FURNACES, KILNS, OVENS OR RETORTS, IN SO FAR AS THEY ARE OF KINDS OCCURRING IN MORE THAN ONE KIND OF FURNACE
    • F27D1/00—Casings; Linings; Walls; Roofs
    • F27D1/0003—Linings or walls
    • F27D1/0023—Linings or walls comprising expansion joints or means to restrain expansion due to thermic flows
    • C—CHEMISTRY; METALLURGY
    • C10—PETROLEUM, GAS OR COKE INDUSTRIES; TECHNICAL GASES CONTAINING CARBON MONOXIDE; FUELS; LUBRICANTS; PEAT
    • C10J—PRODUCTION OF PRODUCER GAS, WATER-GAS, SYNTHESIS GAS FROM SOLID CARBONACEOUS MATERIAL, OR MIXTURES CONTAINING THESE GASES; CARBURETTING AIR OR OTHER GASES
    • C10J2200/00—Details of gasification apparatus
    • C10J2200/09—Mechanical details of gasifiers not otherwise provided for, e.g. sealing means
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F27—FURNACES; KILNS; OVENS; RETORTS
    • F27D—DETAILS OR ACCESSORIES OF FURNACES, KILNS, OVENS OR RETORTS, IN SO FAR AS THEY ARE OF KINDS OCCURRING IN MORE THAN ONE KIND OF FURNACE
    • F27D99/00—Subject matter not provided for in other groups of this subclass
    • F27D99/0073—Seals
    • F27D2099/0081—Joint

Definitions

  • the invention relates to a lining for a combustion chamber which is at least approximately round in cross section and which is divided into at least two layers in the radial direction and at least two sections in the axial direction, with a gas seal made of metallic foil material which extends in the axial direction between two layers Sealing part and a sealing part bent at right angles from this in the boundary region between two layers and extending in the radial direction between two sections.
  • the gas seal is intended to prevent heat flow in the radial direction from the inside to the outside and should take into account the shrinking of the lining which is typical of fiber material.
  • a gas seal that extends continuously from the inside to the outside over at least two layers is not provided, since in the region of the joints between two adjacent layers the essentially horizontally running sealing sections collide with one another at best. A tight connection cannot be achieved in this way.
  • the same also applies to the bent areas which engage in a joint between two adjacent layers, since a bent area of a possibly existing adjacent section is not provided in the same joint.
  • the object of the invention is to design a lining of the type described in the introduction in such a way that it adapts well to different thermal expansions in the individual layers and also enables or simplifies repairs in partial areas of the lining.
  • the invention proposes that the sealing parts, which extend in the radial and axial direction, are connected to a gas seal, which is known per se and extends continuously from the inside to the outside of the lining, in such a way that adjacent sealing parts which extend in the radial direction are in the region between overlap two layers of the lining and are releasably connected in the manner of a plug connection in the axial direction.
  • This configuration takes into account in a very particularly advantageous manner not only the possible removal of an inner sealing part and the connection of a new sealing part to the sealing part of the next outer layer. Rather, this configuration also ensures that the adjacent layers are able to absorb different thermal expansions, without the seal being adversely affected, in particular being damaged. This is achieved in that the overlapping, axially extending sealing parts can slide against one another without the sealing effect being impaired.
  • the overlapping, axially extending sealing parts can be arranged laterally next to each other and adjacent to each other between two layers.
  • an embodiment is also possible in which at least one of the overlapping, axially extending sealing parts is bent back and the other cooperating sealing part can be inserted into the fold formed in this way. In this case, the two sealing parts are pushed into one another in the manner of a plug connection, as a result of which the sealing effect is further improved.
  • the sealing parts extending in the radial direction can be arranged in the axial direction at different heights and the overlapping sealing parts extending in the axial direction bridge the height difference between two adjacent sealing parts extending in the radial direction.
  • Such a step-like arrangement of the sealing parts extending in the radial direction favors the sealing effect in the radial direction since there is no continuous joint from the inside to the outside.
  • the arrangement is expediently such that the fold is open at the bottom.
  • the fold can be attached to that of two adjacent such sealing parts which is arranged higher in the axial direction than the other sealing part which can be inserted into the fold.
  • the free edge of the sealing part which can be inserted into the fold can be folded back by 180 ° to form a sealing lip.
  • An additional improvement of the sealing effect is also the possibility of folding over the free edge of the section forming the fold of the sealing part extending in the axial direction towards the outside of the fold.
  • the folded areas also increase the strength of the free edge.
  • a sealing part is composed of a ring segment extending in the radial direction and a strip extending in the axial direction, which acts as a connecting part, which are connected to one another by folding .
  • the outer most sealing part can be arranged with its outer edge between a support ring and a retaining ring, the two rings being screwed together and connected to one another in another way.
  • the layers of the lining of at least one section can also be supported on an annular support bracket, the outer edge of the outer sealing part being held in a clamping manner between the lining and the support bracket.
  • the gas seal is also advantageously divided into a plurality of sealing parts in the circumferential direction, the end regions of which face one another in the circumferential direction overlap one another.
  • This enables good adaptability of the seal to the thermal expansion occurring in the circumferential direction.
  • one of the two end regions of a sealing part lies above and one below the end region of an adjacent sealing part, with at least one of the sealing parts overlapping the adjacent sealing parts with both end regions. This makes it easy to mount the seal over the circumference of the lining.
  • a furnace which here has the form of a pressure reactor and is used to gasify carbon-containing material, will be described with reference to FIG. 1.
  • Average temperatures up to 1100 ° C occur here, which can reach peak values of up to 1500 ° C.
  • the operating pressure will generally be between 10 and 30 bar, although maximum values up to over 100 bar are possible.
  • such a pressure reactor can have an outside diameter of up to 4 m and a length of up to 10 m or more.
  • the pressure reactor has an outer steel jacket 10 and a lining which is made of refractory building materials and forms three layers 11, 12 and 13. Each of these layers 11, 12 and 13 is along the length of the pressure reactor, i.e. in the axial direction, divided into two sections, one above and the other below a gas seal generally designated by reference numeral 14. Since the gas seal 14 has the task of preventing the penetration of gas into the outer part of the lining due to pressure differences that can occur between the lower and the upper part of the interior 15 during a reaction process, further gas seals 14 are also used as required be arranged in the higher area of the pressure reactor if such pressure differences are also to be expected there.
  • the gas seal is formed in the radial direction by three sealing parts 16, 17 and 18, of which the sealing part 16 between the two sections of the layer 11 adjoining one another in the axial direction and the part 17 between the two adjoining one another in the axial direction Portions of the layer 12 and the Teit 18 between the two axially adjacent portions of the layer 13 of the lining is arranged.
  • the sealing part 16 can, as shown for example below in connection with FIGS. 3 and 4, be divided over the circumference into individual sector-shaped parts which overlap accordingly. Since the lining cross section is circular, the strip 16a of the sealing part 16 runs in a correspondingly circular arc, which also applies to the other strips of the sealing parts which extend in the axial direction and which are described in connection with the later exemplary embodiments.
  • the sealing part 16 like the sealing parts 17 and 18 and the sealing parts to be described in connection with the other exemplary embodiments, consists of a metal foil, the thickness of which is between 0.01 and 1 mm. In general, thicknesses between 0.05 and 0.3 mm will be used, although different foils can of course also be selected within a gas seal. As a material for the film, it is advisable to use high-temperature steels with relatively high alloy proportions or another high-temperature alloy.
  • the sealing part 17 which adjoins the sealing part 16 towards the outside has on it Both ends have a strip 17a bent over in the axial direction, one of which is bent downwards and overlaps with the strip 16a of the sealing part 16.
  • An annular seal 20 is inserted between the sealing part 18 and the support ring 19.
  • On the top of the sealing part 18 is a retaining ring 21 which is screwed to the support ring 19.
  • the overlap between the sealing parts 16, 17 and 18 is designed such that the sealing parts can be separated from one another by pulling them off in the axial direction. If, for example, you only want to replace the lower section of the inner layer 11 of the lining, the sealing part 16 can be removed after the upper section has been temporarily intercepted and the lower section of the layer 11 has been removed and, if necessary, replaced by a new sealing side 16.
  • the overlapping strips 16a and 17a or 17a and 18a also allow compensation for different thermal expansions in the axial direction.
  • the film, from which the sealing parts 16, 17 and 18 are made, is shown both in Fig. 2 and in the following figures in relation to the thickness of the layers 11, 12 and 13 on a disproportionately large scale in order to better show the overlap can. In practice, these overlap areas lie in a relatively narrow gap between two adjacent layers 11, 12 or 13 of the lining or between sections of the respective lining layers lying one above the other.
  • FIG. 3 and 4 show which structure a gas seal can have in the circumferential direction.
  • FIG. 4 is shown in the manner of a processing for FIG. 3.
  • the circumferentially overlapping sealing parts 22 have strips 22a bent upwards in the axial direction and overlap in such a way that of the two circumferential edges of each sealing part 22, one edge lies above and one edge below the edge of an adjacent part . Only two of the sealing parts 22 overlap both edges of the adjacent sealing parts 22. These sealing parts are installed as the first and last part of the gas seal.
  • the gas seal in the radial direction is also divided into three sealing parts 23, 24 and 25.
  • the inner sealing part 23 assigned to the layer 11 has a strip 23a bent upwards.
  • the adjacent sealing part 24 has, on its side facing the sealing part 23, an approximately V-shaped strip 24a, which overlaps the strip 23a of the sealing part 23 or into which the strip 23a can be inserted.
  • the sealing part 24 has on its outer edge a strip 24b which is first bent downwards and then outwards, the horizontal part of which overlaps the horizontal part of a strip 25a of the sealing part 25 which is shaped in the same way.
  • This overlap area is located in a groove-shaped recess 26 of approximately square cross-section, which is formed in the middle layer 12 of the lining and is filled with a sealing or filling compound in the form of mortar, fiber material or the like.
  • the outer sealing part 25 is fastened in the same way as in the exemplary embodiment according to FIG. 2 by means of a support ring 19, a seal 20 and a retaining ring 21.
  • the sealing part 27 has a strip 27a bent in the axial direction, the free edge of which in turn is bent through 180 ° to form a sealing lip 27b.
  • the edge of the sealing part 27 can better adapt to the shape of a strip 28a of the sealing part 28 which is bent into a V-shaped pocket.
  • the free edge of the strip 28a is in turn bent back outwards by 180 ° in order to achieve greater strength in this area.
  • the connection is also established here simply by plugging the sealing parts 27 and 28 into one another.
  • two sealing parts 29 and 30 are not in direct contact with one another, but are connected to one another by a connecting part 31.
  • the sealing part 29 has a strip 29a bent upwards in the axial direction.
  • the connecting part 31 is connected to the sealing part 30 by two folds 30a and 31a. Following the fold 31 a, the connecting part 31 forms a second, likewise U-shaped part 31 b, which runs at approximately a right angle to the fold 31 a and surrounds the strip 29 a of the sealing part 29.
  • the connecting part 31 is also designed and shaped here in such a way that the sealing part 29 can be inserted or removed in the axial direction.
  • a seal 32 can additionally be placed between the strips 29a and the surrounding U-shaped part 31b of the connecting part 31.
  • a layer 33 is assigned to the layer 11, which has a strip 33a which is bent upward approximately in the axial direction. The latter, in turn, is bent outwards at its free edge by 180 °.
  • this embodiment of the gas seal is similar to the embodiment according to FIG. 2. However, the overlap area in the axial direction is now even greater.
  • the layer 11 of the lining is divided in the axial direction above and below the gas seal.
  • the upper lining section is supported on console stones 35 which are enclosed in a support ring 36 of L-shaped cross section.
  • a concrete ring that is continuous over the circumference or formed from segment-shaped parts can also be used.
  • the support ring 36 lies over two seals 37 on a support bracket 38, which in turn is welded to the steel jacket 19.
  • a sealing part 39 assigned to the inner layer 11 and a sealing part 40 assigned to the other two layers 12 and 13 are connected to one another in the same way as, for example — the sealing parts 23 and 24 in the embodiment according to FIG. 5.
  • the outer sealing part 40 is between the two seals 37 held clamped.

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  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Oil, Petroleum & Natural Gas (AREA)
  • Organic Chemistry (AREA)
  • Gasket Seals (AREA)
  • Furnace Housings, Linings, Walls, And Ceilings (AREA)

Claims (13)

1. Revêtement pour un foyer ayant une section au moins approximativement circulaire, ledit revêtement étant divisé en direction radiale en au moins deux couches (11, 12, 13) et en direction axiale en au moins deux sections, comprenant un joint étanche au gaz en une matière métallique en forme de feuille, ledit joint comprenant une partie de joint (16a, 17a; 23a, 24a; 27a, 28a; 29a, 31 b; 33a, 34a) s'étendant entre deux couches (11,12, 13} en direction axiale et une partie de joint (16, 17, 18; 23, 24, 25; 27, 28; 29, 30; 33, 34; 39, 40) pliée dans la zone limite entre deux couches (11, 12,13) sous angle droit et s'étendant en direction radiale entre deux sections, caractérisé en ce que les parties de joint s'étendant en direction radiale et axiale sont jointes l'une à l'autre pour former un joint étanche au gaz connu en soi s'étendant du côté intérieur vers le côté extérieur du revêtement d'une façon continue, cette fonction étant de telle sorte que des parties de joint adjacentes s'étendant en direction radiale dans la zone entre deux couches (11,12,13) du revêtement se recouvrent et sont unies de façon amovible en direction axiale de la façon d'un système de couplage.
2. Revêtement selon la revendication 1, caractérisé en ce que les parties de joint (16a, 17a; 17a, 18a; 33a, 34a) axial se recouvrant sont disposées de façon à être en contact l'une avec l'autre et à se trouver latéralement l'une à côté de l'autre entre deux couches (11, 12, 13).
3. Revêtement selon l'une des revendications 1 ou 2, caractérisé en ce que les parties de joint (16, 17, 18) s'étendant en direction radiale sont disposées dans différentes hauteurs par rapport à l'axe et que les parties de joint (16a, 17a;17a, 18a) se recouvrant et s'étendant en direction axiale remplissent la différence de hauteur existant entre deux parties de joint adjacentes s'étendant en direction radiale.
4. Revêtement selon la revendication 1, caractérisé en ce qu'au moins une des parties de joint (23a, 24a, 27a, 28a) se recouvrant est pliée en arrière et que l'autre partie de joint (23a, 27a) peut être introduite dans le pli ainsi formé.
5. Revêtement selon la revendication 3, caractérisé en ce que le pli est ouvert vers le bas.
6. Revêtement selon l'une des revendications 4 ou 5, caractérisé en ce que le pli est formé sur celle (28) de deux parties de joint (27, 28) adjacentes s'étendant en direction radiale qui est arrangée en direction axiale plus haut que l'autre partie de joint (27) qui peut être introduite dans la fente.
7. Revêtement selon l'une des revendications 4 à 6, caractérisé en ce que le bord libre de la partie de joint (27a) pouvant être introduite dans la fente est pliée en arrière de 180° pour former une lèvre d'étanchéité (27b, 27a).
8. Revêtement selon l'une des revendications 4 à 7, caractérisé en ce que le bord libre de la section de la partie de joint (28a) s'étendant en direction axiale formant le joint est plié vers le côté extérieur du pli.
9. Revêtement selon l'une des revendications précédentes, caractérisé en ce qu'une partie de joint (30) respective est composée d'un segment annulaire s'étendant en direction radiale et d'une bande (partie de connexion 31) s'étendant en direction axiale, ledit segment et ladite bande étant unis par pliage (fig. 7).
10. Revêtement selon l'une des revendications précédentes, caractérisé en ce que la partie de joint (18) se trouvant le plus vers l'extérieur est disposée avec son bord extérieur entre un anneau de support (19) et un anneau de maintien (21 ) et en ce que les anneaux sont serrés à vis.
11. Revêtement selon l'une des revendications précédentes, caractérisé en ce que les couches (12, 13) du revêtement d'au moins une section reposent sur une console de support (38) annulaire et que le bord extérieur de la partie de joint (40) extérieure est maintenu par pincement entre le revêtement et la colonne de support (38).
12. Revêtement selon l'une des revendications précédentes, caractérisé en ce que le joint étanche au gaz (14) est également divisé en direction circonférentielle en plusieurs parties de joint (22) dont les zones terminales opposées en direction circonférentielle se recouvrent.
13. Revêtement selon la revendication 12, caractérisé en ce que des deux zones terminales d'une partie de joint (22) une zone respective se trouve au-dessus et l'autre au-dessous de la zone terminale d'une partie de joint adjacente et qu'au moins une des parties de joint (22) recouvre avec les deux zones terminales les parties de joint adjacentes.
EP82901961A 1981-06-19 1982-06-16 Revetement d'un foyer de section au moins approximativement circulaire Expired EP0081551B1 (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE19813124263 DE3124263A1 (de) 1981-06-19 1981-06-19 Auskleidung fuer einen im querscchnitt zumindest angenaehert runden feuerungsraum
DE3124263 1981-06-19

Publications (2)

Publication Number Publication Date
EP0081551A1 EP0081551A1 (fr) 1983-06-22
EP0081551B1 true EP0081551B1 (fr) 1985-02-06

Family

ID=6135000

Family Applications (1)

Application Number Title Priority Date Filing Date
EP82901961A Expired EP0081551B1 (fr) 1981-06-19 1982-06-16 Revetement d'un foyer de section au moins approximativement circulaire

Country Status (11)

Country Link
US (1) US4463690A (fr)
EP (1) EP0081551B1 (fr)
JP (1) JPS58500958A (fr)
AU (1) AU554508B2 (fr)
BR (1) BR8207755A (fr)
CA (1) CA1194365A (fr)
DD (1) DD210341A1 (fr)
DE (2) DE3124263A1 (fr)
SU (1) SU1269749A3 (fr)
WO (1) WO1982004473A1 (fr)
ZA (1) ZA824072B (fr)

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Publication number Priority date Publication date Assignee Title
US4918894A (en) * 1988-11-21 1990-04-24 Conoco Inc. Refractory supporting anchoring system
DE4343319A1 (de) * 1993-12-18 1995-06-22 Abb Patent Gmbh Brennkammer mit keramischer Auskleidung
DE19533912C2 (de) * 1995-09-13 1998-09-24 Gutehoffnungshuette Man Feuerfestauskleidung für eine Synthesegasanlage
SE9904284L (sv) * 1999-11-26 2001-05-27 Kvaerner Chemrec Ab Keramisk isolering i reaktorer för understökiometrisk förgasning av restprodukter från framställning av kemisk massa
WO2013002746A2 (fr) * 2011-06-15 2013-01-03 Emsa Enerji Madencilik Sanayi Ve Ticaret Anonim Sirketi Unité à eau chaude et à vapeur à commande automatique réalisant la combustion de schiste bitumineux et de charbon avec de l'hydrogène et/ou de l'air
US20140287170A1 (en) * 2013-03-22 2014-09-25 Applied Materials, Inc. Reflective liners

Citations (1)

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Publication number Priority date Publication date Assignee Title
DE2948385A1 (de) * 1979-12-01 1981-06-04 Karrena GmbH, 4000 Düsseldorf Feuerungsraum

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DE698685C (de) * 1936-03-11 1940-11-15 Oesterreichische Magnesit Akt Ausmauerung von Feuerungen und OEfen
US2763321A (en) * 1949-08-26 1956-09-18 Custom Metal Products Inc Double-walled metal combustion chamber
DE1174934B (de) * 1959-08-19 1964-07-30 Steinmueller Gmbh L & C Abdichtung der Aussenwand fuer Dampfkessel mit UEberdruckfeuerung
US3503111A (en) * 1966-12-07 1970-03-31 Mahon Technology Group Industrial oven wall construction
DE1558568A1 (de) * 1967-07-25 1970-04-09 Inst Za Bakar Mauerwerk fuer metallurgische OEfen
DE2425962C3 (de) * 1974-05-30 1979-04-05 Shell Internationale Research Maatschappij B.V., Den Haag (Niederlande) Gasgenerator für die Vergasung feinzerteilter Brennstoffe
US4001996A (en) * 1974-06-03 1977-01-11 J. T. Thorpe Company Prefabricated insulating blocks for furnace lining
US4096681A (en) * 1975-05-02 1978-06-27 Rostfria Tak Aktiebolag Fastener for retaining sheet cladding
US4333292A (en) * 1980-07-28 1982-06-08 Owens-Corning Fiberglas Corporation Insulated roof structure

Patent Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2948385A1 (de) * 1979-12-01 1981-06-04 Karrena GmbH, 4000 Düsseldorf Feuerungsraum

Also Published As

Publication number Publication date
AU554508B2 (en) 1986-08-21
DE3262211D1 (en) 1985-03-21
EP0081551A1 (fr) 1983-06-22
DE3124263A1 (de) 1983-01-05
DD210341A1 (de) 1984-06-06
JPS58500958A (ja) 1983-06-09
SU1269749A3 (ru) 1986-11-07
CA1194365A (fr) 1985-10-01
US4463690A (en) 1984-08-07
WO1982004473A1 (fr) 1982-12-23
AU8587582A (en) 1983-01-04
ZA824072B (en) 1983-04-27
BR8207755A (pt) 1983-05-31

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