EP1557611B1 - Joint d'étanchéité, revêtement et chambre de combustion - Google Patents

Joint d'étanchéité, revêtement et chambre de combustion Download PDF

Info

Publication number
EP1557611B1
EP1557611B1 EP20040001229 EP04001229A EP1557611B1 EP 1557611 B1 EP1557611 B1 EP 1557611B1 EP 20040001229 EP20040001229 EP 20040001229 EP 04001229 A EP04001229 A EP 04001229A EP 1557611 B1 EP1557611 B1 EP 1557611B1
Authority
EP
European Patent Office
Prior art keywords
flow
cladding
combustion chamber
flow barrier
barrier
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Lifetime
Application number
EP20040001229
Other languages
German (de)
English (en)
Other versions
EP1557611A1 (fr
Inventor
Olga Deiss
Holger Grote
Andreas Heilos
Marc Tertilt
Bernd Vonnemann
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 ES04001229.6T priority Critical patent/ES2528177T3/es
Priority to EP20040001229 priority patent/EP1557611B1/fr
Publication of EP1557611A1 publication Critical patent/EP1557611A1/fr
Application granted granted Critical
Publication of EP1557611B1 publication Critical patent/EP1557611B1/fr
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • 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
    • F23M5/04—Supports for linings
    • 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
    • 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
    • F23R3/007—Continuous combustion chambers using liquid or gaseous fuel constructed mainly of ceramic components
    • 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 invention relates to a flow barrier as an insert in a flow region between a first and a second cladding element of a lining of a combustion chamber.
  • the invention leads to a fairing and a combustion chamber.
  • a combustion chamber in particular the combustion chamber of a gas turbine combustion chamber of a gas turbine, is usually provided with a lining in order to insulate and protect the housing parts of the combustion chamber-carrying housing, also referred to as combustion chamber structure.
  • the combustion chamber conditions prevailing in the combustion chamber which are characterized in particular by strongly fluctuating and high temperatures, pressures and oxidizing effects of the hot gas, are kept away from the housing.
  • a region of the housing is to be protected, in which the holder of the panel is attached.
  • the thermal loads are usually in a temperature range of 1350 ° C or above and can also, for. B. subject to strong fluctuations in the context of a quick closure.
  • the metallic housing is usually not suspendable.
  • the housing and the holder are therefore also to protect against a progressing with time material fatigue, the material fatigue is higher, the more frequent and larger temperature and pressure fluctuations occur in the combustion chamber.
  • the cladding usually has a number of cladding elements. Particularly advantageous is a formed from a ceramic cladding element, as a heat shield (Ceramic Heat Shield, CHS) proven. Another possibility is to form a cladding element of a high temperature resistant metal alloy. On a metallic cladding element, a ceramic coating can be applied.
  • a gap is set in the assembly of a trim element on the entire circumference of the trim element.
  • the cladding elements of the panel are therefore mounted at a distance. This clearance provides a flow area between a first and a second trim element of the trim.
  • a cooling air flow running between the housing part and the lining is guided during operation of the combustion chamber. This serves in particular for cooling the holder, which holds a cladding element on the inside of the housing part facing a combustion chamber.
  • the cooling air can penetrate through the flow region into the combustion chamber.
  • the gaps are to be protected from the combustion chamber side penetrating hot gas intake.
  • the cooling air is guided from the housing part and the back of the panel forth in the direction of the combustion chamber, to block in this way a gap with the cooling air.
  • the flow barrier thus has to meet a wide variety of requirements.
  • the flow barrier should on the one hand take account of a width of the flow region which varies as a result of thermal changes and on the other hand should be heat-resistant.
  • porous ceramic gaskets are made of EP 1 302 723 A1 known. Although such a porous ceramic gasket is resistant to high temperatures, it must not come into direct contact with the hot gas. Since this contact in the combustion chamber is difficult to avoid, such a porous ceramic seal must be flowed through by cooling air in order to cool the seal itself and also to block the flow region from a hot gas intake. Nevertheless, in porous ceramic gaskets of the type mentioned overheating occurred. The essential reason is that a sufficient in each case a real operation of a combustion chamber flow through the porous ceramic seal with cooling air is difficult to guarantee.
  • a cladding element when using the usual concept explained here at its edge due to the cooling air outlet at a significantly lower temperature than at its center facing the combustion chamber.
  • a usually panel-shaped cladding element has a relatively high rigidity along its lateral extent. The high temperature gradient along the lateral extent and the stiffness along the lateral extent together lead to considerable stresses along the lateral extent of the cladding element.
  • the US 5333443 A discloses a flow barrier for use in a flow region between first and second trim members of a combustor of a gas turbine engine.
  • the flow barrier is secured to a support structure carrying the trim elements and includes a screw and a stack of rectangular stacked sheet-like seals which are urged by the screw and a coil spring surrounding the screw to seal against the trim elements.
  • the seals are offset from each other and arranged several times, so that there is a seal of the flow area.
  • the US 6145452 A discloses hexagonal cladding elements of a combustor which are attached to a support structure at a central bore by means of a helical fastener made of ceramic.
  • the invention is whose task is to provide a flow barrier, which is resistant to heat and at the same time can be used in a variable-shape, varying in size flow area and which is as simple as possible.
  • a further object of the present invention in terms of the lining and the combustion chamber with such a flow barrier is to take into account the problems explained in connection with the cooling air.
  • a flow barrier for use in a flow region between a first and a second cladding element of a lining of a combustion chamber, wherein the flow barrier has a high temperature resistant ceramic body and a spring element and the high temperature resistant ceramic body and the spring element have an elongated extent, wherein the ceramic body rests along a bearing surface on the spring element, and the bearing surface is aligned along the elongate extent.
  • the invention has recognized that a hitherto customary porous ceramic flow barrier leads to a number of consequential problems which are avoided according to the concept of an overall high-temperature-resistant flow barrier explained here.
  • the use of a high temperature resistant ceramic body as part of the flow barrier ensures that the flow barrier has sufficient hot gas resistance, which is independent of a cooling air flow.
  • an alumina ceramic has been found. It can also be used depending on the usefulness of another high-temperature resistant ceramic.
  • the sufficient hot gas resistance of the high-temperature resistant ceramic body has, in particular, the particularly reliable and reliable effect of the flow barrier in comparison to conventional porous ceramic flow barriers.
  • the combination of the high-temperature resistant ceramic body with a spring element to a flow barrier also has the effect according to the finding of the invention that the barrier effect of the flow barrier achieved by the spring force acting on the ceramic body proves to be particularly effective.
  • the combination of the high-temperature resistant ceramic body and the spring element to a flow barrier proves to be particularly adaptable when used in a highly variable shape and distance flow region between the first and the second cladding element as a result of temperature fluctuations.
  • the parts, d. H. the high-temperature resistant ceramic body and the spring element, the flow barrier can be easily manufactured and thus produced inexpensively.
  • the invention is thus, in departure from the known porous ceramic flow barrier, from the new and surprising in its effect consideration that compared to a porous ceramic flow barrier the flow barrier explained here with a relatively rigid high-temperature resistant ceramic body yet to a reliable sealing of the flow area leads.
  • the flow barrier according to the new concept namely as sufficiently variable within the variable-shape flow area.
  • the high temperature resistant ceramic body and the spring element have an elongated extent, wherein the ceramic body rests along a bearing surface on the spring element and the bearing surface is aligned along the elongate extent.
  • elongated spring elements can be assembled particularly easily and mounted in a flow region of a lining of a combustion chamber. Its elongated extent accounts for the elongate extent of the flow area between a first and a second trim element of the fairing.
  • the support surface is curved towards the spring element.
  • the spring element on its side facing the support surface on a trough and the high-temperature resistant ceramic body on its side facing the support surface on a bulge are suitably adapted to each other, so that the ceramic body in the spring element comes to rest securely and is secured against lateral slipping in the trough.
  • the spring element expediently has retaining means which ensure the position of the high-temperature-resistant ceramic body along the elongate extension.
  • the ceramic body is also in an axial direction, ie in a direction of elongated extent, against a Secured slipping.
  • a stop or a sufficiently rough design of the bearing surface between the spring element and the ceramic body is particularly suitable.
  • the spring element is formed at least along a fraction of the elongated extent in the form of a spring subjected to compression according to the operating principle of a disc spring. That is, the spring element is, except for its elongated extension (instead of a round in a plate spring), formed in principle like a plate spring and is based in principle on the same mechanism of action as a plate spring.
  • the spring element is formed along a further fraction of the elongated extension in the form of a bare support. It has proved to be particularly useful to form the spring element along a central part of the elongated extension in the form of a compression spring, clip-like, after the operating principle of a disc spring and form along its lateral parts of the elongated extension in the form of a bare support.
  • the supports support the high-temperature resistant ceramic body in its edition while in the middle part of the spring force is generated.
  • the spring element is formed at least along a fraction of the elongated extent in the form of a pressure-loaded, resiliently yielding solid body.
  • any type of material comes into consideration, which gives the solid body a pressure-loaded resilient effect. It can be a uniform solid material or a composition or a conglomerate of different materials.
  • a cross section through the solid body advantageously has a shape that is similar to the shape of a horizontal figure eight.
  • the object with regard to the cladding is achieved by a cladding for a combustion chamber with a number of cladding elements, wherein between a first and second cladding element, a flow region is formed, in which a flow barrier of the above type is used.
  • one or more flow barriers are inserted into the flow region in such a way that the flow region is completely sealed by the one or more flow barriers. In this way, namely a hot gas intake into the flow area is completely prevented.
  • One or more of the flow barriers are particularly advantageously used in all flow regions extending along a circumference of a cladding element. To this In this way, a hot gas intake is avoided in all flow areas that run circumferentially around a cladding element.
  • the object is achieved in terms of the combustion chamber according to the invention by a combustion chamber with a lining, which has a number of cladding elements, wherein between a first and a second cladding element, a flow region is formed, in which a flow barrier of the type mentioned above is used.
  • This concept guarantees a reliable cooling of the holder and thus a secure and permanently stable mounting of the cladding elements.
  • a hot gas intake into the flow area is avoided.
  • Corrosion problems due to hot gas intake or other material loads in the vicinity of the flow region and behind the lining, in particular in the holder, are thus - in contrast to known flow barriers - eliminated.
  • the aforementioned flow barrier design also has the advantage that larger tolerances in adjusting the column, i. the flow area between a first and a second cladding element are possible. In this way, the assembly time of the cladding elements is considerably reduced.
  • the cooling air flowing out of a flow region between the lining elements is reduced or completely suppressed.
  • the temperature gradients that form from the edges of a cladding element towards the cladding element center and the stresses associated therewith along the lateral extent of the cladding element are significantly reduced. Due to the reduced stresses, fewer and, if any, shorter cracks will form in a cladding element during operation.
  • porous ceramic flow barriers are known.
  • Such a known flow barrier is in the form of a double tube formed with an outer shell of high temperature resistant, ceramic Nextelgewebe and an inner shell of an Inconellgestrick, which is flexible in the composite and has sufficient length stability as well as the flow barrier on the spring force of the fabric holds in its axial position.
  • the ends of the flow barrier are sewn with a multifilament thread.
  • FIG. 1 shows a lining 1 for a combustion chamber with a number of cladding elements in the region of a first cladding element 3 and a second cladding element 5.
  • a flow region 7 is formed in the form of a gap.
  • the risk of hot gas intake exists from the side of the combustion chamber 11.
  • the flow region 7 is a first variant of a flow barrier 9, which completely seals the flow region against hot gas intake, used.
  • the flow region has a holder 12.
  • a first part 13 of the holder 12 holds the first cladding element 3.
  • a second part 15 of the holder 12 holds the second cladding element 5.
  • Both the flow barrier 9 and the holder 12 engage in a cavity 17 into which the flow area 7 approximately the height of the center of the panel 1 and a cladding element 3, 5, expands.
  • the cavity 17 is formed by a first groove 23 of the first cladding element 3 and by a second groove 25 of the second cladding element 5.
  • the flow barrier 9 is formed by a high-temperature-resistant ceramic body 19 and a first variant of a spring element 21, wherein the first variant of the spring element 21 is formed in the form of a plate spring like spring-loaded.
  • the flow barrier 9 according to this first variant in the form of a metal seal with ceramic insert combines the temperature resistance of a ceramic with the spring properties of a metal.
  • the resilient metal clip as spring plate-like design and pressure-loaded spring of the first variant of the spring element 21 is mounted between the outlet ends of the holder 12 in the region of the cavity 17 and the high temperature resistant ceramic body 19.
  • the illustrated here first variant of the spring element 21 in the form of a metal clip presses the high temperature resistant ceramic body 19 firmly against the hot bar 33 of the first cladding element 3 and the hot bar 35 of the second cladding element 5.
  • the ceramic body 19 grinds on its top optimally on the bars 33, 35, so that the sealing effect of the flow barrier increases after a short period of operation and finally a complete sealing effect can be achieved.
  • the high-temperature-resistant ceramic body 19 protects the first variation of the spring element 21 formed as a metal clamp and the holder 12 from the side of the combustion chamber 11 before a hot gas intake through the flow region 7.
  • FIGS. 2 to 4 the assembly of the in the FIG. 1 shown first variant of the flow barrier 9.
  • a first cladding element 3 is mounted with a first part 13 of a holder 12 and a second part 15 of the holder 12.
  • the first variant of a flow barrier 9 in the form of a composite seal of a first variant of a spring element 21 in the form of a metal clip on the one hand and with a high temperature resistant ceramic body 19 on the other hand into the cavity 17 forming groove 23 of the first cladding element 3 is inserted.
  • the second cladding element 5 is pushed and mounted with its groove 17 forming the groove 25 via the holder 12 and the flow barrier 9.
  • first variant of a spring element 21 has a trough 41, which forms the bearing surface between the first variant of the spring element 21 and the ceramic solid body 19.
  • the in FIG. 2 shown solid ceramic body has a bulge 43, which comes to rest in the trough 41.
  • the bearing surface formed between the spring element 21 and the solid ceramic body 19 is thus arched towards the spring element 21.
  • the in FIG. 3 shown spring element 21 at its axial ends along its elongated extension 45 each have a stop 47, which secures the position of the ceramic body 19 in a direction of elongated extent 45, ie in the axial direction.
  • the spring element 21 also has, along its middle part 49 of the elongated extension 45, the shape of a spring under pressure, which is designed in accordance with the principle of action of a disc spring.
  • the spring 51 in the middle part 49 is at its sides 53 downwards, curved in an annular shape, the ends 55 facing slightly upwards, but are free.
  • the spring 51 thus has the form of a metal clip. In this way, it works much like a diaphragm spring.
  • the spring element 21 is designed in the form of a mere support, which also continues the trough 41.
  • the mere support has no spring action as the spring 51 in the middle part 49.
  • the trough 41 protects and reinforces the high temperature resistant ceramic body 19 along the entire elongated extension 45 of the ceramic body 19, in particular against breakage, and presses it against the hot gas side 33, 35 a Cladding element 3, 5 of in FIG. 1 ,
  • FIG. 5 shows a second variant of a flow barrier 10 with a high temperature resistant ceramic body 20 and a second variant of a spring element 22.
  • the second variant of the spring element 22 along the entire elongated extension 46 in the form of a pressure-loaded resiliently yielding solid body is formed.
  • the solid body is formed in the present embodiment of an Inconellgestrick or may in a further embodiment of this second variant of a similar material as the ceramic seal in the EP 1 302 723 A1 , namely in particular in the form of a ceramic seal with a Nextelhülle be formed.
  • the shape of the second variant of the Spring element 22 is similar to the shape of the first variant of the spring element 21 made of metal, namely in cross-section similar to the shape of a lying eight.
  • FIG. 6 is a perspective view of the second variant of the spring element 22 consisting of the solid ceramic body 20 and the pressure-loaded resiliently yielding solid body of the second variant of the spring element 22 shown.
  • This second variant of the flow barrier 10 in turn rests on a holder 12 and is located in a cavity 17 of a flow region 7 between a first cladding element 3 and a second cladding element 5.
  • the other elements of FIG. 6 correspond to those of FIG. 1 and are provided with the same reference numerals.
  • FIG. 7 shows a first cladding element 3 and a second cladding element 5 with the second variant of in FIG. 6 shown flow barrier 10 in a larger section of the panel 2 for a selected in this embodiment annular combustion chamber.
  • the second variant of the flow barrier 10 could in the present case optionally also by the in FIG. 1 shown first variant of the flow barrier 9 to be replaced.
  • FIG. 7 illustrates the effect of such a first variant of the flow barrier 9 or a second variant of a flow barrier 10 shown here in the combustion chamber.
  • the flow barrier 9, 10 with high-temperature resistant ceramic body 19, 20 and spring element 21, 22 is virtually impermeable to air due to their above-described training after a short period of operation.
  • lining elements 3, 5 are attached to the combustion chamber 11 facing inside of a housing part 4 by means of one or more brackets for fastening the cladding elements 3, 5.
  • the brackets 12 have cooling air holes 14.
  • the flow barrier 9, 10 is in fact inserted into a flow region 7 in such a way that the flow region 7 is completely sealed by the flow barrier 9, 10, since it is impermeable to air.
  • a running between the housing part 4 and the cover 3, 5 cooling air flow 6 does not get through the flow area 7 into the combustion chamber 11, but rather for the benefit of the combustion chamber, along an orientation 48 of the flow region for cooling the holder 12 deflected.
  • the extent of the flow region 48 suitably agrees with the in FIGS. 2 to 5 shown elongated expansions 45, 46 of a flow barrier 9, 10 match.
  • the distance between a first 3 and a second 5 cladding element is formed by a gap which provides a flow region 7 between the first 3 and the second cladding element and in the combustion chamber side hot gas and in the opposite direction cooling air can penetrate, the flow region 7 due to temperature changes may have varying dimensions.
  • a flow barrier 9, 10 is disclosed herein which has a high-temperature resistant ceramic body 19, 20 and a spring element 21, 22.
  • the proposed flow barrier 9, 10 has improved heat resistance, greater cooling-air saving potential and reduces thermally-induced stresses in a trim element 3, 5.
  • the invention leads to a lining of a combustion chamber and a combustion chamber.

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Ceramic Engineering (AREA)
  • Gasket Seals (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)

Claims (12)

  1. Barrière ( 9, 10 ) à l'écoulement à utiliser dans une zone ( 7 ) d'écoulement entre un premier ( 3 ) et un deuxième ( 5 ) éléments d'un habillage ( 1 ) d'une chambre de combustion, les barrières ( 9, 10 ) à l'écoulement ayant un corps ( 19, 20 ) en céramique résistant aux températures hautes et un élément ( 21, 22 ) à ressort et
    le corps ( 19, 20 ) en céramique résistant aux températures hautes et l'élément ( 21, 22 ) à ressort ont une étendue ( 45 ) longitudinale, le corps ( 19, 20 ) en céramique s'appliquant à l'élément ( 21, 22 ) à ressort le long d'une surface d'application et la surface d'application étant dirigée le long de l'étendue ( 45 ) longitudinale.
  2. Barrière ( 9, 10 ) à l'écoulement suivant la revendication 1, caractérisée en ce que
    la barrière ( 9, 10 ) à l'écoulement peut être fixée entre le premier ( 3 ) et le deuxième ( 5 ) éléments d'habillage, de manière à ce que la barrière ( 9, 10 ) à l'écoulement pénètre dans un élargissement de la zone ( 7 ) d'écoulement, l'élargissement de la zone d'écoulement étant formé par une première rainure dans le premier élément d'habillage et par une deuxième rainure dans le deuxième élément d'habillage.
  3. Barrière ( 9, 10 ) à l'écoulement suivant la revendication 1 ou 2,
    caractérisée en ce que
    la surface d'application est courbée en allant vers l'élément ( 21, 22 ) à ressort.
  4. Barrière ( 9, 10 ) à l'écoulement suivant l'une des revendications 1 à 3,
    caractérisée en ce que
    l'élément ( 21, 22 ) à ressort a un moyen ( 47 ) de maintien, qui maintient la position du corps ( 19, 20 ) en céramique résistant aux températures hautes le long de l'étendue ( 45 ) longitudinale.
  5. Barrière ( 9 ) à l'écoulement suivant l'une des revendications 1 à 4,
    caractérisée en ce que
    l'élément ( 21 ) à ressort est constitué au moins le long d'une fraction de l'étendue ( 45 ) longitudinale sous la forme d'un ressort sollicité à la compression suivant le principe d'action d'un ressort à disque.
  6. Barrière ( 9 ) à l'écoulement suivant la revendication 5,
    caractérisée en ce que
    l'élément ( 21 ) à ressort est constitué le long d'une autre fraction de l'étendue ( 45 ) longitudinale sous la forme d'un simple appui.
  7. Barrière ( 10 ) à l'écoulement suivant l'une des revendications 1 à 4,
    caractérisée en ce que
    l'élément ( 22 ) à ressort est constitué au moins le long d'une fraction de l'étendue ( 45 ) longitudinale sous la forme d'un corps plein sollicité à la compression et cédant élastiquement.
  8. Habillage ( 1 ) d'une chambre de combustion ayant un certain nombre d'éléments d'habillage, dans lequel il est formé, entre un premier ( 3 ) et un deuxième ( 5 ) éléments d'habillage, une zone ( 7 ) d'écoulement, dans laquelle est mise une barrière ( 9, 10 ) à l'écoulement suivant l'une des revendications 1 à 7.
  9. Habillage ( 1 ) suivant la revendication 8,
    caractérisé en ce que
    une ou plusieurs barrières ( 9, 10 ) à l'écoulement sont mises dans la zone ( 7 ) d'écoulement, de manière à ce que la zone ( 7 ) d'écoulement soit rendue étanche complètement par la ou par les plusieurs barrières ( 9, 10 ) à l'écoulement.
  10. Habillage ( 1 ) suivant la revendication 8 ou 9,
    caractérisé en ce que
    une ou plusieurs barrières ( 9, 10 ) à l'écoulement sont mises dans l'ensemble des zones ( 7 ) d'écoulement s'étendant le long d'un pourtour d'un élément ( 3, 5 ) d'habillage.
  11. Chambre de combustion ayant un habillage ( 1 ), qui a un certain nombre d'éléments ( 3, 5 ) d'habillage, dans laquelle il est formé, entre un premier ( 3 ) et un deuxième ( 5 ) éléments d'habillage, une zone ( 7 ) d'écoulement, dans laquelle est mise une barrière ( 9, 10 ) à l'écoulement suivant l'une des revendications 1 à 7.
  12. Chambre de combustion suivant la revendication 11, caractérisée en ce que
    - un élément ( 3, 5 ) d'habillage est mis au moyen d'une fixation ( 12 ) sur le côté intérieur, tourné vers l'espace ( 11 ) de combustion, d'une partie ( 4 ) d'enveloppe, et
    - une ou plusieurs barrières ( 9, 10 ) à l'écoulement sont mises dans la zone ( 7 ) d'écoulement, de manière à rendre étanche complètement la zone ( 7 ) d'écoulement par la ou les plusieurs barrières ( 9, 10 ) à l'écoulement, et
    - un courant ( 6 ) d'air de refroidissement s'étendant entre la partie ( 4 ) d'enveloppe et l'habillage ( 1 ), qui est dévié par une ou par plusieurs barrières ( 9, 10 ) à l'écoulement le long d'une étendue ( 48 ) de la zone ( 7 ) d'écoulement pour le refroidissement de la fixation ( 12 ).
EP20040001229 2004-01-21 2004-01-21 Joint d'étanchéité, revêtement et chambre de combustion Expired - Lifetime EP1557611B1 (fr)

Priority Applications (2)

Application Number Priority Date Filing Date Title
ES04001229.6T ES2528177T3 (es) 2004-01-21 2004-01-21 Barrera de flujo, revestimiento y cámara de combustión
EP20040001229 EP1557611B1 (fr) 2004-01-21 2004-01-21 Joint d'étanchéité, revêtement et chambre de combustion

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
EP20040001229 EP1557611B1 (fr) 2004-01-21 2004-01-21 Joint d'étanchéité, revêtement et chambre de combustion

Publications (2)

Publication Number Publication Date
EP1557611A1 EP1557611A1 (fr) 2005-07-27
EP1557611B1 true EP1557611B1 (fr) 2014-12-31

Family

ID=34626476

Family Applications (1)

Application Number Title Priority Date Filing Date
EP20040001229 Expired - Lifetime EP1557611B1 (fr) 2004-01-21 2004-01-21 Joint d'étanchéité, revêtement et chambre de combustion

Country Status (2)

Country Link
EP (1) EP1557611B1 (fr)
ES (1) ES2528177T3 (fr)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105324611A (zh) 2013-05-21 2016-02-10 西门子股份公司 用于燃烧室的隔热件的隔热瓦
DE102015202570A1 (de) * 2015-02-12 2016-08-18 Rolls-Royce Deutschland Ltd & Co Kg Abdichtung eines Randspalts zwischen Effusionsschindeln einer Gasturbinenbrennkammer
EP3104077B1 (fr) * 2015-06-08 2021-05-12 ANSALDO ENERGIA S.p.A. Carreau céramique thermo-isolant présentant une faible épaisseur pour une chambre de combustion d'une turbine à gaz
EP3845810B1 (fr) * 2019-12-31 2023-11-22 ANSALDO ENERGIA S.p.A. Dispositif de support pour des tuiles d'isolation thermique d'une chambre de combustion d'un ensemble turbine à gaz pour centrales électriques et ensemble turbine à gaz

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5333443A (en) * 1993-02-08 1994-08-02 General Electric Company Seal assembly
DE19730751A1 (de) * 1996-07-24 1998-01-29 Siemens Ag Keramisches Bauteil für eine Wärmeschutzschicht sowie Wärmeschutzschicht
EP0895028B1 (fr) * 1997-07-28 2002-03-06 Alstom Garniture céramique
EP1260767A1 (fr) * 2001-05-25 2002-11-27 Siemens Aktiengesellschaft Ensemble bouclier thermique pour un composant acheminant un gaz chaud, notamment pour des pièces de structure de turbines à gaz, ainsi que le procédé de fabrication d'un tel ensemble
EP1302723A1 (fr) 2001-10-15 2003-04-16 Siemens Aktiengesellschaft Revêtement pour parois intérieures de chambre de combustion

Also Published As

Publication number Publication date
EP1557611A1 (fr) 2005-07-27
ES2528177T3 (es) 2015-02-05

Similar Documents

Publication Publication Date Title
EP2363643B1 (fr) Elément de bouclier thermique
EP1872058B1 (fr) Chambre de combustion munie d'un bouclier thermique
DE102012105402B4 (de) Verstellvorrichtung für einen Abgasturbolader
DE60032440T2 (de) Halterung für die Brennkammer einer Gasturbine
DE10155420A1 (de) Hitzeschildanordnung mit Dichtungselement
WO1992009850A1 (fr) Ecran thermique en ceramique monte sur une structure portante
EP0904512B1 (fr) Systeme de bouclier thermique, notamment pour elements structuraux d'installations a turbine a gaz
DE4343658A1 (de) Gleitverbindungsvorrichtung zwischen zwei Teilen, die starken mechanischen und thermischen Belastungen unterliegen
WO2009124824A1 (fr) Élément de fixation et turbocompresseur à géométrie de turbine variable
DE60119674T2 (de) Verfahren und Vorrichtung für die Abdichtung verstellbarer Düsen in Gasturbinen
EP1429058A2 (fr) Joint plat, en particulier joint pour collecteur d'échappement
EP2881691A1 (fr) Échangeur de chaleur avec une plaque tubulaire et un manchon inséré
DE102005032980A1 (de) Brennkammerbaugruppe für einen Verdampferbrenner
DE4414961A1 (de) Zylinderkopfdichtung
EP3091188B1 (fr) Turbomachine dotée d'un dispositif d'étanchéité
DE102005046731A1 (de) Hitzeschildanordnung
DE60300423T2 (de) Kühlsystem für eine Nachbrennerdüse in einer Turbomaschine
EP1557611B1 (fr) Joint d'étanchéité, revêtement et chambre de combustion
DE102008020870A1 (de) Klappenventil
EP1591724B1 (fr) Elément d'étanchéité d'une fente pour un bouclier thermique
EP1128131A1 (fr) Bouclier thermique, chambre de combustion et turbine à gaz
DE2909467A1 (de) Absperrschieber fuer rohrleitungen grosser nennweiten
DE2937788A1 (de) Leichtmetallzylinderkopf fuer brennkraftmaschinen
WO2005008053A1 (fr) Moteur, notamment moteur diesel deux temps, important
DE4322526A1 (de) Brennkraftmaschine mit Katalysator im Auslaßkanal

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

Kind code of ref document: A1

Designated state(s): AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HU IE IT LI LU MC NL PT RO SE SI SK TR

AX Request for extension of the european patent

Extension state: AL LT LV MK

17P Request for examination filed

Effective date: 20050822

AKX Designation fees paid

Designated state(s): AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HU IE IT LI LU MC NL PT RO SE SI SK TR

17Q First examination report despatched

Effective date: 20110428

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

GRAP Despatch of communication of intention to grant a patent

Free format text: ORIGINAL CODE: EPIDOSNIGR1

INTG Intention to grant announced

Effective date: 20140804

GRAS Grant fee paid

Free format text: ORIGINAL CODE: EPIDOSNIGR3

GRAA (expected) grant

Free format text: ORIGINAL CODE: 0009210

AK Designated contracting states

Kind code of ref document: B1

Designated state(s): AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HU IE IT LI LU MC NL PT RO SE SI SK TR

REG Reference to a national code

Ref country code: GB

Ref legal event code: FG4D

Free format text: NOT ENGLISH

Ref country code: CH

Ref legal event code: EP

Ref country code: CH

Ref legal event code: NV

Representative=s name: SIEMENS SCHWEIZ AG, CH

REG Reference to a national code

Ref country code: IE

Ref legal event code: FG4D

Free format text: LANGUAGE OF EP DOCUMENT: GERMAN

REG Reference to a national code

Ref country code: ES

Ref legal event code: FG2A

Ref document number: 2528177

Country of ref document: ES

Kind code of ref document: T3

Effective date: 20150205

REG Reference to a national code

Ref country code: AT

Ref legal event code: REF

Ref document number: 704647

Country of ref document: AT

Kind code of ref document: T

Effective date: 20150215

REG Reference to a national code

Ref country code: DE

Ref legal event code: R096

Ref document number: 502004014797

Country of ref document: DE

Effective date: 20150219

REG Reference to a national code

Ref country code: NL

Ref legal event code: T3

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: FI

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20141231

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: SE

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20141231

Ref country code: GR

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20150401

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: SK

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20141231

Ref country code: CZ

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20141231

Ref country code: RO

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20141231

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: LU

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20150121

REG Reference to a national code

Ref country code: DE

Ref legal event code: R097

Ref document number: 502004014797

Country of ref document: DE

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: EE

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20141231

Ref country code: DK

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20141231

Ref country code: MC

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20141231

REG Reference to a national code

Ref country code: IE

Ref legal event code: MM4A

PLBE No opposition filed within time limit

Free format text: ORIGINAL CODE: 0009261

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

Free format text: STATUS: NO OPPOSITION FILED WITHIN TIME LIMIT

26N No opposition filed

Effective date: 20151001

REG Reference to a national code

Ref country code: FR

Ref legal event code: PLFP

Year of fee payment: 13

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: IE

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20150121

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: SI

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20141231

REG Reference to a national code

Ref country code: AT

Ref legal event code: MM01

Ref document number: 704647

Country of ref document: AT

Kind code of ref document: T

Effective date: 20150121

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: NL

Payment date: 20160120

Year of fee payment: 13

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: DE

Payment date: 20160321

Year of fee payment: 13

Ref country code: IT

Payment date: 20160127

Year of fee payment: 13

Ref country code: ES

Payment date: 20160223

Year of fee payment: 13

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: AT

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20150121

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: FR

Payment date: 20160115

Year of fee payment: 13

Ref country code: GB

Payment date: 20160111

Year of fee payment: 13

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: CH

Payment date: 20160404

Year of fee payment: 13

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: HU

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT; INVALID AB INITIO

Effective date: 20040121

Ref country code: BG

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20141231

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: CY

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20141231

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: BE

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20150131

Ref country code: PT

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20150501

REG Reference to a national code

Ref country code: DE

Ref legal event code: R119

Ref document number: 502004014797

Country of ref document: DE

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: TR

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20141231

REG Reference to a national code

Ref country code: CH

Ref legal event code: PL

REG Reference to a national code

Ref country code: NL

Ref legal event code: MM

Effective date: 20170201

GBPC Gb: european patent ceased through non-payment of renewal fee

Effective date: 20170121

REG Reference to a national code

Ref country code: FR

Ref legal event code: ST

Effective date: 20170929

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: FR

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20170131

Ref country code: LI

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20170131

Ref country code: CH

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20170131

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: NL

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20170201

Ref country code: GB

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20170121

Ref country code: DE

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20170801

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: IT

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20170121

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: ES

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20170122

REG Reference to a national code

Ref country code: ES

Ref legal event code: FD2A

Effective date: 20180627