[go: up one dir, main page]
More Web Proxy on the site http://driver.im/

EP1302723A1 - Lining for combustion chamber inside walls - Google Patents

Lining for combustion chamber inside walls Download PDF

Info

Publication number
EP1302723A1
EP1302723A1 EP01124603A EP01124603A EP1302723A1 EP 1302723 A1 EP1302723 A1 EP 1302723A1 EP 01124603 A EP01124603 A EP 01124603A EP 01124603 A EP01124603 A EP 01124603A EP 1302723 A1 EP1302723 A1 EP 1302723A1
Authority
EP
European Patent Office
Prior art keywords
elements
flow barrier
lining
shielding elements
lining according
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.)
Withdrawn
Application number
EP01124603A
Other languages
German (de)
French (fr)
Inventor
Milan Schmahl
Christine Dr. Taut
Marc Tertilt
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.)
Siemens AG
Original Assignee
Siemens 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 Siemens AG filed Critical Siemens AG
Priority to EP01124603A priority Critical patent/EP1302723A1/en
Priority to JP2002294861A priority patent/JP2003176915A/en
Priority to CNB021443556A priority patent/CN100498076C/en
Priority to US10/270,458 priority patent/US6840047B2/en
Publication of EP1302723A1 publication Critical patent/EP1302723A1/en
Withdrawn legal-status Critical Current

Links

Images

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/002—Wall structures
    • 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
    • F23M2900/00—Special features of, or arrangements for combustion chambers
    • F23M2900/05005—Sealing means between wall tiles or panels
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R2900/00—Special features of, or arrangements for continuous combustion chambers; Combustion processes therefor
    • F23R2900/00012—Details of sealing devices

Definitions

  • the present invention relates to a lining for interior walls of combustion chambers with gaps left on the inner wall to be arranged, essentially plate-shaped shielding elements.
  • the invention further relates to flow barriers for use in appropriate linings.
  • Linings for internal walls of combustion chambers in particular also those for gas turbines on which the present one relates Invention also relates are known per se.
  • the combustion chambers are with essentially plate-shaped shielding elements lined which are temperature resistant and where "Basic" describes the basic dimension.
  • the shielding elements can also be designed as hollow elements.
  • To absorb different or transient thermal expansions to be able to, are usually between neighboring Leave the shielding elements in the column. Because in this column from the Combustion chamber hot gas can enter, causing overheating on shielding elements, holding elements or the combustion chamber wall can lead, it is known, between the combustion chamber wall and shielding elements to introduce sealing air so that the Columns are blocked against hot gas intake.
  • Part of the sealing air is used to cool the shielding or Fasteners needed.
  • the minimum air consumption is due to the cooling of the shielding and fastening elements necessary air volume defined. Ideally, this should be The amount of air required for cooling is also sufficient to block the gaps.
  • the blocking of the technically necessary Column (thermal expansion stationary and unsteady, manufacturing tolerances, Assembly requirements) between the shielding elements however requires significantly higher air volumes. The air requirement is therefore directly dependent on the gap area.
  • the reduction in air consumption has a positive effect on stability the burner flames, the effectiveness of the machine and pollutant emissions and enables another Increased performance while maintaining maximum material temperatures.
  • the present invention has for its object to provide a lining for the inner walls of combustion chambers with substantially plate-shaped shielding elements to be arranged on the inner wall with gap leaving, which avoids the migration of hot gases by means of economically available means by efficient sealing.
  • the invention proposes that flow barriers that can be used be used in a gap between adjacent shielding elements.
  • the flow barrier is passed through flexible, temperature-resistant sealing elements formed, which in are advantageously porous. Due to the porosity the possibility of cooling the sealing elements.
  • the sealing elements are strip-shaped and thus for gap sealing are good to use.
  • the sealing elements made from a mixture of materials such as wire mesh, Wire mesh, wire mix, fiber mix, fabric, ceramic fabric and the like are formed.
  • tubular sealing elements It is also possible to form tubular sealing elements and fill them with the appropriate material as needed.
  • the sealing elements are advantageously made by means of holders positioned in the gap area and fixed there.
  • the side edges are of the shielding elements with grooves so that strip-shaped sealing elements in the grooves and thus the Allow the column to be hidden.
  • the invention also relates to novel flow barriers for use in gaps between shielding elements of combustion chamber inner walls.
  • Such flow barriers enable efficient and targeted cooling the sealing air requirement and affect a higher flame stability as well as the ability to reduce the combustion chamber To operate flame temperature.
  • Fig. 1 shows a basic structure of, for example, on the inner wall shielding elements 1 arranged in a combustion chamber, between which there are column 2, in which according to the Invention flow barriers 3 are used.
  • the flow barriers can be fixed baffles, nozzle plates, Batch of materials, composite structures and the like.
  • Fig. 2 are in the side edges of the shielding elements 1 formed according to one embodiment grooves 4, in which an essentially rod-shaped sealing element 3 is used to form a flow barrier.
  • the sealing element 3 has holder 5, which of the attachment the sealing elements 3 serve, for example, an arbitrary Avoid longitudinal displacement.
  • Fig. 3 shows a corresponding Side view.
  • Fig. 4 shows the representation of a corresponding sealing element.
  • the holder 5 by means of a holder anchor 6, with which they form a T-shaped cross section, inserted into the sealing element.
  • the sealing element can, for example from a fabric tube, ceramic or the like exist, which is filled with appropriate filling materials is. Also can be used for longitudinal reinforcement Struts may be provided. 9 shows possible design variants of the filled hose.
  • Sealing element base 7 and holder 8 comprises.
  • the sealing element base 7 can now be provided with material for sealing accordingly be covered, for example, with a textile tube and filled, with batches, with knitted fabric, knitted fabric, Foam or the like.
  • FIG. 6 shows a strand 9 from a material mixture, for example Steel wool or the like, in an elongated Shape, indicated by the envelope 10.
  • a material mixture for example Steel wool or the like
  • FIG. 7 can such a batch strand, knitted strand or the like 9 in a groove 4 of a shielding element 1 is inserted and fixed there be, for example, by pressing, gluing, hooking or similar.
  • shielding elements 1 When putting together shielding elements 1 then results in the gap 2, the seal through contiguous batch strands 9, as shown in Fig. 8.
  • This parallel arrangement for sealing the gap in each opposite grooves in shielding elements can all embodiments of the flow barriers (fabric hose, Material mixture, baffle, composite structures and the like) can be applied.

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Gas Burners (AREA)
  • Gasket Seals (AREA)

Abstract

The lining has plate-like screen elements (1) set against the inside wall leaving a gap (2) inbetween so that flow barriers (3) can be inserted in the gap between adjoining screen elements. <??>The flow barriers are formed by flexible temperature-resistant sealing elements made of a porous material.

Description

Die vorliegende Erfindung betrifft eine Auskleidung für Innenwände von Brennkammern mit unter Spaltbelassung an der Innenwand anzuordnenden, im wesentlichen plattenförmigen Abschirmelementen. Weiterhin betrifft die Erfindung Strömungsbarrieren zum Einsatz in entsprechenden Auskleidungen.The present invention relates to a lining for interior walls of combustion chambers with gaps left on the inner wall to be arranged, essentially plate-shaped shielding elements. The invention further relates to flow barriers for use in appropriate linings.

Auskleidungen für Innenwände von Brennkammern, insbesondere auch solche für Gasturbinen, auf welche sich die vorliegende Erfindung auch bezieht, sind an sich bekannt. Die Brennkammern werden mit im wesentlichen plattenförmigen Abschirmelementen ausgekleidet, welche temperaturbeständig sind und wobei "plattenförmig" die Grunddimension beschreibt. Die Abschirmelemente können auch als Hohlelemente ausgebildet sein. Um unterschiedliche bzw. instationäre Wärmeausdehnungen aufnehmen zu können, werden üblicherweise zwischen benachbarten Abschirmelementen Spalte belassen. Da in diese Spalte aus der Brennkammer stammendes Heißgas eintreten kann, was zur Überhitzung an Abschirmelementen, Halteelementen oder der Brennkammerwand führen kann, ist es bekannt, zwischen Brennkammerwand und Abschirmelementen Sperrluft einzuführen, so daß die Spalte gegen Heißgaseinzug gesperrt sind.Linings for internal walls of combustion chambers, in particular also those for gas turbines on which the present one relates Invention also relates are known per se. The combustion chambers are with essentially plate-shaped shielding elements lined which are temperature resistant and where "Basic" describes the basic dimension. The shielding elements can also be designed as hollow elements. To absorb different or transient thermal expansions to be able to, are usually between neighboring Leave the shielding elements in the column. Because in this column from the Combustion chamber hot gas can enter, causing overheating on shielding elements, holding elements or the combustion chamber wall can lead, it is known, between the combustion chamber wall and shielding elements to introduce sealing air so that the Columns are blocked against hot gas intake.

Ein Teil der Sperrluft wird zur Kühlung der Abschirm- bzw. Befestigungselemente benötigt. Der Mindestluftverbrauch ist durch die zur Kühlung der Abschirm- und Befestigungselemente notwendige Luftmenge definiert. Im Idealfall sollte diese zur Kühlung benötigte Luftmenge auch zur Sperrung der Spalte ausreichen. Die Sperrung der technisch bedingt erforderlichen Spalte (Wärmedehnung stationär und instationär, Fertigungstoleranzen, Montageerfordernisse) zwischen den Abschirmelementen erfordert jedoch erheblich höhere Luftmengen. Der Luftbedarf ist somit direkt von der Spaltfläche abhängig. Part of the sealing air is used to cool the shielding or Fasteners needed. The minimum air consumption is due to the cooling of the shielding and fastening elements necessary air volume defined. Ideally, this should be The amount of air required for cooling is also sufficient to block the gaps. The blocking of the technically necessary Column (thermal expansion stationary and unsteady, manufacturing tolerances, Assembly requirements) between the shielding elements however requires significantly higher air volumes. The air requirement is therefore directly dependent on the gap area.

Weiterhin bildet sich im Inneren der Brennkammer ein Druckund Temperaturfeld aus. Bei der Bemessung des Luftbedarfs muss dieses Druck- und Temperaturfeld berücksichtigt werden. Dadurch sind lokal höhere Luftmengen erforderlich. Die vorgeschlagene Strömungsbarriere verringert die Spaltfläche und ermöglicht somit eine erhebliche Reduktion des Luftbedarfs. Zudem wird der Luftbedarf von Druck- und Temperaturfeld weitgehend entkoppelt, was ein weiteres Einsparpotential erschließt.Furthermore, a pressure and builds up inside the combustion chamber Temperature field. When measuring the air requirement this pressure and temperature field must be taken into account. This means that locally higher air volumes are required. The proposed one Flow barrier reduces the gap area and thus enables a significant reduction in air consumption. In addition, the air requirement of the pressure and temperature field is largely decouples, which opens up further savings potential.

Die Senkung des Luftbedarfs wirkt sich positiv auf die Stabilität der Brennerflammen, die Effektivität der Maschine und die Schadstoffemissionen aus und ermöglicht eine weitere Leistungssteigerung unter Einhaltung maximal gegebener Materialtemperaturen.The reduction in air consumption has a positive effect on stability the burner flames, the effectiveness of the machine and pollutant emissions and enables another Increased performance while maintaining maximum material temperatures.

Ausgehend vom vorbeschriebenen Stand der Technik liegt der vorliegenden Erfindung die Aufgabe zugrunde, eine Auskleidung für Innenwände von Brennkammern mit unter Spaltbelassung an der Innenwand anzuordnenden, im wesentlichen plattenförmigen Abschirmelementen bereitzustellen, welche durch eine effiziente Abdichtung das Einwandern von Heißgasen unter Verwendung wirtschaftlich bereitstehender Mittel vermeidet.Starting from the above-described prior art, the present invention has for its object to provide a lining for the inner walls of combustion chambers with substantially plate-shaped shielding elements to be arranged on the inner wall with gap leaving, which avoids the migration of hot gases by means of economically available means by efficient sealing.

Zur technischen Lösung wird mit der Erfindung vorgeschlagen, daß in einen Spalt zwischen benachbarten Abschirmelementen einsetzbare Strömungsbarrieren verwendet werden.As a technical solution , the invention proposes that flow barriers that can be used be used in a gap between adjacent shielding elements.

Durch den erfindungsgemäßen Einsatz von Strömungsbarrieren kann einerseits ein Einwandern von Heißgas in den Bereich zwischen Abschirmelementen und Brennkammerwandung wirksam verhindert werden, zum anderen kann die in diesem Bereich geführte Kühlluft gezielt eingesetzt werden, da sie nun nicht mehr über offene Spalte austritt. Damit reduziert sich die Sperrwirkungs-Notwendigkeit nur noch auf solche Spaltbereiche, an welchen keine Strömungsbarrieren eingesetzt sind. Through the use of flow barriers according to the invention On the one hand, hot gas can migrate into the area effective between shielding elements and the combustion chamber wall can be prevented, on the other hand, the guided in this area Cooling air can be used specifically since it is not emerges more about open column. This reduces the The blocking effect is only necessary for such gap areas, where no flow barriers are used.

Insbesondere wird nur sehr wenig Luft für Sperrluft benötigt, wodurch sich ein erheblicher wirtschaftlicher Nutzen erschließt.In particular, very little air is required for sealing air, which opens up significant economic benefits.

In erfindungsgemäßer Weise wird die Strömungsbarriere durch flexible, temperaturbeständige Dichtelemente gebildet, die in vorteilhafter Weise porös sind. Durch die Porösität ergibt sich die Möglichkeit der Kühlung der Dichtelemente.In the manner according to the invention, the flow barrier is passed through flexible, temperature-resistant sealing elements formed, which in are advantageously porous. Due to the porosity the possibility of cooling the sealing elements.

Weiterhin wird mit Vorteil vorgeschlagen, daß die Dichtelemente streifenförmig ausgebildet sind und somit zur Spaltabdichtung gut einsetzbar sind. In vorteilhafter Weise können die Dichtelemente aus Materialgemenge wie Drahtgewirke, Drahtgestricke, Drahtgemenge, Fasergemenge, Gewebe, Keramikgewebe und dergleichen gebildet werden.Furthermore, it is advantageously proposed that the sealing elements are strip-shaped and thus for gap sealing are good to use. Can advantageously the sealing elements made from a mixture of materials such as wire mesh, Wire mesh, wire mix, fiber mix, fabric, ceramic fabric and the like are formed.

Auch ist es möglich, schlauchförmige Dichtelemente auszubilden und diese nach Bedarf mit entsprechendem Material zu verfüllen.It is also possible to form tubular sealing elements and fill them with the appropriate material as needed.

In vorteilhafter Weise werden die Dichtelemente mittels Haltern in den Spaltbereich positioniert und dort fixiert.The sealing elements are advantageously made by means of holders positioned in the gap area and fixed there.

Gemäß einem weiteren vorteilhaften Vorschlag sind die Seitenkanten der Abschirmelemente mit Nuten versehen, so daß sich streifenförmige Dichtelemente in den Nuten und damit die Spalte verdeckend positionieren lassen.According to a further advantageous proposal, the side edges are of the shielding elements with grooves so that strip-shaped sealing elements in the grooves and thus the Allow the column to be hidden.

Die Erfindung bezieht sich auch auf neuartige Strömungsbarrieren für den Einsatz in Spalten zwischen Abschirmelementen von Brennkammerinnenwänden. Derartige Strömungsbarrieren ermöglichen eine effiziente und gezielte Kühlung, reduzieren den Sperrluftbedarf und wirken sich auf eine höhere Flammenstabilität sowie die Möglichkeit, die Brennkammer mit verringerter Flammentemperatur zu betreiben, aus. The invention also relates to novel flow barriers for use in gaps between shielding elements of combustion chamber inner walls. Such flow barriers enable efficient and targeted cooling the sealing air requirement and affect a higher flame stability as well as the ability to reduce the combustion chamber To operate flame temperature.

Die Erfindung läßt sich mit geringem wirtschaftlichen Aufwand unter Verwendung geeigneter Materialien realisieren. Weitere Vorteile und Merkmale der Erfindung ergeben sich aus der folgenden Beschreibung anhand der Figuren. Dabei zeigen:

Fig. 1
eine Draufsicht auf eine Abschirmelementanordnung mit schematisch dargestellten Strömungsbarrieren;
Fig. 2
eine Schnittansicht entlang Linie II-II gemäß Fig. 1;
Fig. 3
eine Schnittansicht gemäß III-III gemäß Fig. 1;
Fig. 4
eine perspektivische Ansicht eines Ausführungsbeispiels für ein Dichtelement;
Fig. 5
eine perspektivische Ansicht für eine alternative Ausführungsform eines Dichtelement-Trägers;
Fig. 6
eine schematische Ansicht einer weiteren Ausführungsform für ein Dichtelement;
Fig. 7
eine perspektivische Ansicht eines eingesetzten Dichtelementes gemäß Fig. 6;
Fig. 8
eine Schnittansicht mit Dichtelementen gemäß Fig. 6 und
Fig. 9
Schnittansichten durch mögliche Ausführungsvarianten von Dichtelementen gemäß Fig. 6
The invention can be implemented with little economic effort using suitable materials. Further advantages and features of the invention result from the following description with reference to the figures. Show:
Fig. 1
a plan view of a shielding element arrangement with schematically illustrated flow barriers;
Fig. 2
a sectional view taken along line II-II of FIG. 1;
Fig. 3
a sectional view according to III-III of FIG. 1;
Fig. 4
a perspective view of an embodiment of a sealing element;
Fig. 5
a perspective view of an alternative embodiment of a sealing element carrier;
Fig. 6
a schematic view of a further embodiment for a sealing element;
Fig. 7
a perspective view of an inserted sealing element according to FIG. 6;
Fig. 8
a sectional view with sealing elements according to FIG. 6 and
Fig. 9
Section views through possible design variants of sealing elements according to FIG. 6

In den Fig. werden für gleiche Elemente gleiche Bezugszeichen verwendet.In the figures, the same reference numerals are used for the same elements used.

Fig. 1 zeigt einen Grundaufbau von beispielsweise an der Innenwand einer Brennkammer angeordneten Abschirmelementen 1, zwischen denen sich Spalte 2 befinden, in welche gemäß der Erfindung Strömungsbarrieren 3 eingesetzt sind. Die Strömungsbarrieren können fest montierte Leitbleche, Düsenbleche, Materialgemenge, Kompositaufbauten und dergleichen sein.Fig. 1 shows a basic structure of, for example, on the inner wall shielding elements 1 arranged in a combustion chamber, between which there are column 2, in which according to the Invention flow barriers 3 are used. The flow barriers can be fixed baffles, nozzle plates, Batch of materials, composite structures and the like.

Wie aus Fig. 2 erkennbar, sind in den Seitenkanten der Abschirmelemente 1 gemäß einer Ausführungsform Nuten 4 ausgebildet, in welche ein im wesentlichen stabförmiges Dichtelement 3 zur Bildung einer Strömungsbarriere eingesetzt ist. Das Dichtelement 3 weist Halter 5 auf, welche der Befestigung der Dichtelemente 3 dienen, beispielsweise um ein willkürliches Längsverschieben zu vermeiden. Fig. 3 zeigt eine entsprechende Seitenansicht.As can be seen from Fig. 2, are in the side edges of the shielding elements 1 formed according to one embodiment grooves 4, in which an essentially rod-shaped sealing element 3 is used to form a flow barrier. The sealing element 3 has holder 5, which of the attachment the sealing elements 3 serve, for example, an arbitrary Avoid longitudinal displacement. Fig. 3 shows a corresponding Side view.

Fig. 4 zeigt die Darstellung eines entsprechenden Dichtelementes. Bei diesem sind die Halter 5 mittels eines Halterankers 6, mit welchem sie einen T-förmigen Querschnitt bilden, in das Dichtelement eingesetzt. Das Dichtelement kann beispielsweise aus einem Gewebeschlauch, Keramik oder dergleichen bestehen, welches mit entsprechenden Füllmaterialien gefüllt ist. Auch können für die Verstärkung in Längsrichtung Streben vorgesehen sein. Fig. 9 zeigt mögliche Ausführungsvarianten des gefüllten Schlauches.Fig. 4 shows the representation of a corresponding sealing element. In this, the holder 5 by means of a holder anchor 6, with which they form a T-shaped cross section, inserted into the sealing element. The sealing element can, for example from a fabric tube, ceramic or the like exist, which is filled with appropriate filling materials is. Also can be used for longitudinal reinforcement Struts may be provided. 9 shows possible design variants of the filled hose.

Gemäß Fig. 5 ist ein alternativer Halter gezeigt, welcher eine Dichtelementbasis 7 und Halter 8 umfaßt. Die Dichtelementbasis 7 kann nun entsprechend mit Material zum Abdichten versehen sein, beispielsweise mit einem Textilschlauch überzogen und befüllt, mit Gemenge versehen, mit Gewirk, Gestrick, Schaum oder dergleichen.5, an alternative holder is shown, which one Sealing element base 7 and holder 8 comprises. The sealing element base 7 can now be provided with material for sealing accordingly be covered, for example, with a textile tube and filled, with batches, with knitted fabric, knitted fabric, Foam or the like.

Fig. 6 zeigt einen Strang 9 aus einem Materialgemenge, beispielsweise Stahlwolle oder dergleichen, in einer länglichen Form, angedeutet durch die Hüllkurve 10. Gemäß Fig. 7 kann ein solcher Gemengestrang, Gewirkstrang oder dergleichen 9 in eine Nut 4 eines Abschirmelementes 1 eingesetzt und dort fixiert werden, beispielsweise durch Einpressen, Kleben, Verhaken oder dergleichen. Beim Aneinandersetzen von Abschirmelementen 1 ergibt sich dann im Spalt 2 die Abdichtung durch die aneinanderliegenden Gemengestränge 9, wie in Fig. 8 gezeigt. Diese parallele Anordnung zur Abdichtung des Spaltes in jeweils gegenüberliegenden Nuten in Abschirmelementen kann auf alle Ausführungsformen der Strömungsbarrieren (Gewebe-schlauch, Materialgemenge, Leitblech, Kompositaufbauten und dergleichen) angewendet werden.6 shows a strand 9 from a material mixture, for example Steel wool or the like, in an elongated Shape, indicated by the envelope 10. According to FIG. 7 can such a batch strand, knitted strand or the like 9 in a groove 4 of a shielding element 1 is inserted and fixed there be, for example, by pressing, gluing, hooking or similar. When putting together shielding elements 1 then results in the gap 2, the seal through contiguous batch strands 9, as shown in Fig. 8. This parallel arrangement for sealing the gap in each opposite grooves in shielding elements can all embodiments of the flow barriers (fabric hose, Material mixture, baffle, composite structures and the like) can be applied.

Die gezeigten Ausführungsbeispiele dienen der Erläuterung und sind nicht beschränkend.The exemplary embodiments shown serve for explanation and are not restrictive.

Claims (11)

Auskleidung für Innenwände von Brennkammern mit unter Spaltbelassung an der Innenwand anzuordnenden, im wesentlichen plattenförmigen Abschirmelementen (1),
gekennzeichnet durch in einen Spalt (2) zwischen benachbarten Abschirmelementen (1) einsetzbare Strömungsbarrieren (3).Lining for inner walls of combustion chambers with essentially plate-shaped shielding elements (1) to be arranged on the inner wall while leaving gaps,
characterized by flow barriers (3) which can be inserted into a gap (2) between adjacent shielding elements (1). Auskleidung nach Anspruch 1,
dadurch gekennzeichnet, daß die Strömungsbarriere (3) durch flexible, temperaturbeständige Dichtelemente (3) gebildet wird.Lining according to claim 1,
characterized in that the flow barrier (3) is formed by flexible, temperature-resistant sealing elements (3). Auskleidung nach einem der vorhergehenden Ansprüche,
dadurch gekennzeichnet, daß die Strömungsbarriere (3) aus einem porösen Material gebildet ist.Lining according to one of the preceding claims,
characterized in that the flow barrier (3) is formed from a porous material. Auskleidung nach einem der vorhergehenden Ansprüche,
dadurch gekennzeichnet, daß die Strömungsbarriere durch streifenförmige Elemente (3) gebildet ist.Lining according to one of the preceding claims,
characterized in that the flow barrier is formed by strip-shaped elements (3). Auskleidung nach einem der vorhergehenden Ansprüche,
dadurch gekennzeichnet, daß die Strömungsbarriere wenigstens teilweise aus einem Materialgemenge (9) gebildet ist.Lining according to one of the preceding claims,
characterized in that the flow barrier is at least partially formed from a mixture of materials (9). Vorrichtung nach einem der vorhergehenden Ansprüche,
dadurch gekennzeichnet, daß die Strömungsbarriere (3) wenigstens teilweise aus einem Gewebe gebildet ist.Device according to one of the preceding claims,
characterized in that the flow barrier (3) is at least partially formed from a fabric. Auskleidung nach einem der vorhergehenden Ansprüche,
dadurch gekennzeichnet, daß die Strömungsbarriere (3) wenigstens teilweise aus Keramik gebildet ist. Lining according to one of the preceding claims,
characterized in that the flow barrier (3) is at least partially made of ceramic. Auskleidung nach einem der vorhergehenden Ansprüche,
dadurch gekennzeichnet, daß die Strömungsbarriere (3) ein schlauchförmiges Element umfaßt.Lining according to one of the preceding claims,
characterized in that the flow barrier (3) comprises a tubular element. Auskleidung aus einem der vorhergehenden Ansprüche,
dadurch gekennzeichnet, daß die Strömungsbarriere (3) mittels Halteelementen (5) ortsfest positionierbar ist.Lining from one of the preceding claims,
characterized in that the flow barrier (3) can be positioned in a stationary manner by means of holding elements (5). Auskleidung nach einem der vorhergehenden Ansprüche,
dadurch gekennzeichnet, daß die Abschirmelemente (1) in Seitenkanten Nuten (4) zur Aufnahme von Strömungsbarrieren (3) aufweisen.Lining according to one of the preceding claims,
characterized in that the shielding elements (1) have grooves (4) in side edges for receiving flow barriers (3). Strömungsbarriere (3, 9) für Auskleidungen für Innenwände von Brennkammern, bei welchen unter Spaltbelassung an der Innenwand der Brennkammer im wesentlichen plattenförmige Abschirmelemente (1) angeordnet werden,
dadurch gekennzeichnet, daß die Strömungsbarriere (3) zum Einsetzen in einen Spalt (2) zwischen benachbarten Abschirmelementen (1) ausgebildet ist.Flow barrier (3, 9) for linings for inner walls of combustion chambers, in which essentially plate-shaped shielding elements (1) are arranged on the inner wall of the combustion chamber while leaving gaps,
characterized in that the flow barrier (3) is designed for insertion into a gap (2) between adjacent shielding elements (1).
EP01124603A 2001-10-15 2001-10-15 Lining for combustion chamber inside walls Withdrawn EP1302723A1 (en)

Priority Applications (4)

Application Number Priority Date Filing Date Title
EP01124603A EP1302723A1 (en) 2001-10-15 2001-10-15 Lining for combustion chamber inside walls
JP2002294861A JP2003176915A (en) 2001-10-15 2002-10-08 Lining for inner wall of combustor
CNB021443556A CN100498076C (en) 2001-10-15 2002-10-10 Lining for combustion chamber internal wall
US10/270,458 US6840047B2 (en) 2001-10-15 2002-10-15 Lining for inner walls of combustion chambers

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
EP01124603A EP1302723A1 (en) 2001-10-15 2001-10-15 Lining for combustion chamber inside walls

Publications (1)

Publication Number Publication Date
EP1302723A1 true EP1302723A1 (en) 2003-04-16

Family

ID=8178974

Family Applications (1)

Application Number Title Priority Date Filing Date
EP01124603A Withdrawn EP1302723A1 (en) 2001-10-15 2001-10-15 Lining for combustion chamber inside walls

Country Status (4)

Country Link
US (1) US6840047B2 (en)
EP (1) EP1302723A1 (en)
JP (1) JP2003176915A (en)
CN (1) CN100498076C (en)

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1557611A1 (en) 2004-01-21 2005-07-27 Siemens Aktiengesellschaft Flow barrier, lining and combustion chamber
WO2005071320A1 (en) 2004-01-27 2005-08-04 Siemens Aktiengesellschaft Thermal shield
EP1591724A1 (en) 2004-04-30 2005-11-02 Siemens Aktiengesellschaft Gap sealing element for a heat shield
EP1591725A2 (en) * 2004-04-30 2005-11-02 Siemens Aktiengesellschaft Hot gas seal
EP1666797A1 (en) * 2004-12-01 2006-06-07 Siemens Aktiengesellschaft Heat shield element, method for manufacturing the same, heat shield and combustor
EP2168935A1 (en) 2008-09-29 2010-03-31 Siemens Aktiengesellschaft Material compound for producing a fire-retardant material and its application and fire-retardant moulding body and method for its manufacture
EP2169311A1 (en) 2008-09-29 2010-03-31 Siemens Aktiengesellschaft Material mixture for producing a fire-retardant material, fire-retardant moulding body and method for its manufacture
DE102018200926A1 (en) * 2018-01-22 2019-07-25 Siemens Aktiengesellschaft Component for positioning a heat shield element

Families Citing this family (19)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE10003728A1 (en) * 2000-01-28 2001-08-09 Siemens Ag Heat shield arrangement for a component carrying hot gas, in particular for structural parts of gas turbines
EP1191285A1 (en) * 2000-09-22 2002-03-27 Siemens Aktiengesellschaft Heat shield panel, combustion chamber with inner lining and a gas turbine
US7152864B2 (en) * 2003-10-02 2006-12-26 Alstom Technology Ltd. Seal assembly
US20050242526A1 (en) * 2004-04-30 2005-11-03 Stefan Dahlke Hot gas seal
EP1715271A1 (en) * 2005-04-19 2006-10-25 Siemens Aktiengesellschaft Heat shield element, combustion chamber and gas turbine
GB2453946B (en) * 2007-10-23 2010-07-14 Rolls Royce Plc A Wall Element for use in Combustion Apparatus
GB0800294D0 (en) * 2008-01-09 2008-02-20 Rolls Royce Plc Gas heater
GB0801839D0 (en) * 2008-02-01 2008-03-05 Rolls Royce Plc combustion apparatus
GB2457281B (en) * 2008-02-11 2010-09-08 Rolls Royce Plc A Combustor Wall Arrangement with Parts Joined by Mechanical Fasteners
GB2460634B (en) * 2008-06-02 2010-07-07 Rolls Royce Plc Combustion apparatus
US20100095679A1 (en) * 2008-10-22 2010-04-22 Honeywell International Inc. Dual wall structure for use in a combustor of a gas turbine engine
US20100095680A1 (en) * 2008-10-22 2010-04-22 Honeywell International Inc. Dual wall structure for use in a combustor of a gas turbine engine
US9341118B2 (en) * 2009-12-29 2016-05-17 Rolls-Royce Corporation Various layered gas turbine engine component constructions
DE112014001160T5 (en) 2013-03-06 2015-12-17 Mitsubishi Heavy Industries, Ltd. exhaust duct
JP6104646B2 (en) * 2013-03-06 2017-03-29 三菱重工業株式会社 Exhaust duct
EP3044444B1 (en) * 2013-09-13 2019-11-06 United Technologies Corporation Combustor for a gas turbine engine with a sealed liner panel
EP2851514A1 (en) * 2013-09-20 2015-03-25 Alstom Technology Ltd Method for applying heat resistant protection components onto a surface of a heat exposed component
EP3299720B1 (en) * 2016-09-22 2020-11-04 Ansaldo Energia IP UK Limited Combustor front assembly for a gas turbine
CN116792200A (en) * 2022-03-16 2023-09-22 通用电气公司 Combustion liner assembly

Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CH392359A (en) 1960-09-23 1965-05-15 Oil Therm Ag Firebox lining made of refractory bricks
US4725567A (en) * 1985-12-02 1988-02-16 General Electric Company Composite by infiltration
EP0417734A1 (en) * 1989-09-12 1991-03-20 Praxair Technology, Inc. Protective lining for aluminum refining vessel
DE19643715A1 (en) * 1996-10-23 1998-04-30 Asea Brown Boveri Cooled flame tube for gas turbine combustion chamber
EP1064510A1 (en) 1998-03-19 2001-01-03 Siemens Aktiengesellschaft Wall segment for a combustion chamber and combustion chamber
EP1130219A1 (en) 2000-03-02 2001-09-05 Siemens Aktiengesellschaft Turbine engine with sealing means between panels
EP1191285A1 (en) 2000-09-22 2002-03-27 Siemens Aktiengesellschaft Heat shield panel, combustion chamber with inner lining and a gas turbine

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
NL69245C (en) * 1946-01-09
GB758213A (en) * 1954-03-03 1956-10-03 Parsons & Marine Eng Turbine Improvements in and relating to cylindrical combustion chambers or furnaces
FR2657675B1 (en) * 1990-01-31 1992-07-03 Dassault Avions THERMAL PROTECTION SYSTEM, ESPECIALLY FOR SPACE VEHICLES.
US5363643A (en) * 1993-02-08 1994-11-15 General Electric Company Segmented combustor
FR2703323B1 (en) * 1993-04-01 1995-06-30 Europ Propulsion THERMAL PROTECTION DEVICE, ESPECIALLY FOR AN AEROSPATIAL MACHINE.

Patent Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CH392359A (en) 1960-09-23 1965-05-15 Oil Therm Ag Firebox lining made of refractory bricks
US4725567A (en) * 1985-12-02 1988-02-16 General Electric Company Composite by infiltration
EP0417734A1 (en) * 1989-09-12 1991-03-20 Praxair Technology, Inc. Protective lining for aluminum refining vessel
DE19643715A1 (en) * 1996-10-23 1998-04-30 Asea Brown Boveri Cooled flame tube for gas turbine combustion chamber
EP1064510A1 (en) 1998-03-19 2001-01-03 Siemens Aktiengesellschaft Wall segment for a combustion chamber and combustion chamber
EP1130219A1 (en) 2000-03-02 2001-09-05 Siemens Aktiengesellschaft Turbine engine with sealing means between panels
EP1191285A1 (en) 2000-09-22 2002-03-27 Siemens Aktiengesellschaft Heat shield panel, combustion chamber with inner lining and a gas turbine

Cited By (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1557611A1 (en) 2004-01-21 2005-07-27 Siemens Aktiengesellschaft Flow barrier, lining and combustion chamber
WO2005071320A1 (en) 2004-01-27 2005-08-04 Siemens Aktiengesellschaft Thermal shield
EP1561997A1 (en) 2004-01-27 2005-08-10 Siemens Aktiengesellschaft Heat Shield
US7677044B2 (en) 2004-01-27 2010-03-16 Siemens Aktiengesellschaft Heat shield
EP2363643A1 (en) 2004-01-27 2011-09-07 Siemens Aktiengesellschaft Heat shield element
EP1591725A3 (en) * 2004-04-30 2014-03-05 Siemens Aktiengesellschaft Hot gas seal
EP1591724A1 (en) 2004-04-30 2005-11-02 Siemens Aktiengesellschaft Gap sealing element for a heat shield
EP1591725A2 (en) * 2004-04-30 2005-11-02 Siemens Aktiengesellschaft Hot gas seal
US8695989B2 (en) 2004-04-30 2014-04-15 Siemens Aktiengesellschaft Hot gas seal
EP1666797A1 (en) * 2004-12-01 2006-06-07 Siemens Aktiengesellschaft Heat shield element, method for manufacturing the same, heat shield and combustor
WO2006058851A1 (en) * 2004-12-01 2006-06-08 Siemens Aktiengesellschaft Thermal shield element, method for the production thereof, hot gas lining, and combustion chamber
EP2168935A1 (en) 2008-09-29 2010-03-31 Siemens Aktiengesellschaft Material compound for producing a fire-retardant material and its application and fire-retardant moulding body and method for its manufacture
US8609019B2 (en) 2008-09-29 2013-12-17 Siemens Aktiengesellschaft Material composition for producing a fireproof material and the use thereof, and fireproof molded body and method for the production thereof
US8530364B2 (en) 2008-09-29 2013-09-10 Siemens Aktiengesellschaft Material mixture for producing a fireproof material, fireproof molded body and method for the manufacturing thereof
EP2169311A1 (en) 2008-09-29 2010-03-31 Siemens Aktiengesellschaft Material mixture for producing a fire-retardant material, fire-retardant moulding body and method for its manufacture
US9108886B2 (en) 2008-09-29 2015-08-18 Siemens Aktiengesellschaft Material composition for producing a fireproof material and the use thereof, and fireproof molded body and method for the production thereof
DE102018200926A1 (en) * 2018-01-22 2019-07-25 Siemens Aktiengesellschaft Component for positioning a heat shield element

Also Published As

Publication number Publication date
CN100498076C (en) 2009-06-10
US6840047B2 (en) 2005-01-11
JP2003176915A (en) 2003-06-27
US20030079475A1 (en) 2003-05-01
CN1412476A (en) 2003-04-23

Similar Documents

Publication Publication Date Title
EP1302723A1 (en) Lining for combustion chamber inside walls
EP2423597B1 (en) Premix burner for a gas turbine
DE10140435C1 (en) Exhaust gas system for a motor vehicle has a tail pipe device running adjacent to a wall part of a motor vehicle construction
DE1529168B1 (en) Burner plate for gas-heated heat radiation devices
DE3806114C2 (en)
DE3828093C2 (en)
EP2066878B1 (en) Filter element, in particular for filtering exhaust gases of an internal combustion engine
DE1905148C3 (en) Radiant burner
DE1291554B (en) Combustion chamber for gas turbines
DE4343319A1 (en) Combustion chamber with a ceramic lining
EP0483743B1 (en) Fiber burner brick and burner with such a fiber burner brick
DE3031606A1 (en) RECUPERATOR.
DE4132235C1 (en)
DE19713407B4 (en) Atmospheric gas burner
EP1422479B1 (en) Chamber for the combustion of a fluid combustible mixture
EP1136777A1 (en) Firing tunnel furnace
EP0107243A1 (en) Horizontal checkerwork for chambers of a regeneratively heated furnace
DE2713414A1 (en) COMBUSTION CHAMBER FOR GAS TURBINE ENGINES
DE102008019532B3 (en) Oil premix burner, has cylindrical fuel element with auxiliary fuel upper surface for heating flame on front side turned towards oil nozzle, where fuel upper surface acts on air heat exchanger for preheating of combustion air
DE4402390C1 (en) Ceramic honeycomb body, for lining furnace walls
DE19706883C2 (en) Exhaust silencers for vehicles with internal combustion engines
DE19718885A1 (en) Gas burner
DE10212050B4 (en) silencer
DE1529168C (en) Burner plate for gas-heated radiant heaters
DE10032190C2 (en) Gas burner with a porous material burner

Legal Events

Date Code Title Description
PUAI Public reference made under article 153(3) epc to a published international application that has entered the european phase

Free format text: ORIGINAL CODE: 0009012

AK Designated contracting states

Designated state(s): AT BE CH CY DE DK ES FI FR GB GR IE IT LI LU MC NL PT SE TR

AX Request for extension of the european patent

Extension state: AL LT LV MK RO SI

17P Request for examination filed

Effective date: 20030519

AKX Designation fees paid

Designated state(s): DE FR GB IT

RAP1 Party data changed (applicant data changed or rights of an application transferred)

Owner name: SIEMENS AKTIENGESELLSCHAFT

RAP1 Party data changed (applicant data changed or rights of an application transferred)

Owner name: SIEMENS AKTIENGESELLSCHAFT

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: THE APPLICATION IS DEEMED TO BE WITHDRAWN

18D Application deemed to be withdrawn

Effective date: 20160408