EP2722486A1 - Seal holder for a stator assembly - Google Patents

Seal holder for a stator assembly Download PDF

Info

Publication number
EP2722486A1
EP2722486A1 EP12188822.6A EP12188822A EP2722486A1 EP 2722486 A1 EP2722486 A1 EP 2722486A1 EP 12188822 A EP12188822 A EP 12188822A EP 2722486 A1 EP2722486 A1 EP 2722486A1
Authority
EP
European Patent Office
Prior art keywords
axial
seal carrier
shell element
flange
radial
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.)
Granted
Application number
EP12188822.6A
Other languages
German (de)
French (fr)
Other versions
EP2722486B1 (en
Inventor
Frank Stiehler
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.)
MTU Aero Engines AG
Original Assignee
MTU Aero Engines 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 MTU Aero Engines AG filed Critical MTU Aero Engines AG
Priority to EP12188822.6A priority Critical patent/EP2722486B1/en
Priority to US14/056,876 priority patent/US9856736B2/en
Publication of EP2722486A1 publication Critical patent/EP2722486A1/en
Application granted granted Critical
Publication of EP2722486B1 publication Critical patent/EP2722486B1/en
Not-in-force legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/02Blade-carrying members, e.g. rotors
    • F01D5/08Heating, heat-insulating or cooling means
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D11/00Preventing or minimising internal leakage of working-fluid, e.g. between stages
    • F01D11/001Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between stator blade and rotor
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B21MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21JFORGING; HAMMERING; PRESSING METAL; RIVETING; FORGE FURNACES
    • B21J5/00Methods for forging, hammering, or pressing; Special equipment or accessories therefor
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D11/00Preventing or minimising internal leakage of working-fluid, e.g. between stages
    • F01D11/02Preventing or minimising internal leakage of working-fluid, e.g. between stages by non-contact sealings, e.g. of labyrinth type
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00Metal working
    • Y10T29/49Method of mechanical manufacture
    • Y10T29/49316Impeller making
    • Y10T29/4932Turbomachine making
    • Y10T29/49321Assembling individual fluid flow interacting members, e.g., blades, vanes, buckets, on rotary support member

Definitions

  • the present invention relates to a fish-mouth seal carrier for a guide vane assembly of a gas turbine, a vane assembly or gas turbine with such a fish-mouth seal carrier and a method for its production.
  • the fishmouth seal carrier is composed of a total of five sheet metal parts: an S-shaped sheet metal part to form a fishmouth gasket, an L-shaped sheet metal part to form an opposite fishmouth gasket, a U-shaped sheet metal part, a radial flange of the platform and a head between its radial legs a screw is arranged, a C-shaped sheet metal part in which a washer is received, which passes through the screw, and finally a G-shaped sheet metal part which carries the S-shaped sheet metal part, wherein the honeycomb seal on the L and the G is attached shaped sheet metal part.
  • An object of an embodiment of the present invention is to improve the manufacture and / or operation of a gas turbine.
  • a fishmouth seal carrier for a guide vane assembly of a gas turbine on a first half-shell member and a materially connected thereto, in particular welded, second half-shell element, which together a box section with two axial legs and form two radial legs.
  • a sealing element which in one embodiment has a honeycomb seal, in particular can be, is arranged on an outer side of a, in installation position radially inner, this axial leg of the box profile.
  • a box profile is understood in particular to mean a profile which has two, in particular at least substantially parallel, axial legs and two, in particular at least substantially parallel, radial legs, in particular thereof, which in a further embodiment is preferably at least substantially rectangular , Corners merge into each other.
  • the first and / or second half-shell element has in each case an axial flange for forming a fish mouth seal, which is formed integrally or integrally with the half-shell element, in particular, ur- or reshaped.
  • the Axialflansch acts in one embodiment as a so-called deflector of Fischmauldichtung. Opposite it radially in one embodiment is a radially inner platform of a vane assembly having one or more vanes to which the fishmouth seal carrier in one embodiment is suspended by means of a spoke centering. Radial between the platform and the axial flange, an axial flange of an adjacent blade assembly is arranged with one or more blades.
  • a Fischmauldichtung upstream and / or downstream of the vane assembly may be formed or have the first and / or second half-shell element of the fish-mouth seal carrier having a corresponding, designed as a deflector Axialflansch.
  • the axial flange of the first and / or second half-shell element extends in one embodiment, at least substantially, in the axial direction. He may have radial paragraphs or steps.
  • the first half-shell element has a U-profile for forming the box profile and a radial flange formed integrally therewith.
  • the radial flange can be followed by the axial flange on the side opposite the U-profile to form a fish gauge.
  • the second half-shell element can have a radial flange, to which the axial flange can connect in one embodiment to form a fish-measuring direction.
  • the radial flange together with the U-profile of the first half-shell element, can form the box profile, i. Completing the U-shaped profile lid-like and essentially form a radial leg of the U-profile.
  • a U-profile for forming the box profile also connects to the radial flange on the second half-shell element on the axial flange, so that both half-shell elements each form a radial leg and in each case a part of the two axial legs of the box profile.
  • a slider for suspending the fishmouth seal carrier on the vane assembly between the radial flange of the first half-shell member and the radial flange of the second half-shell member is mounted on both sides.
  • the fish-mouth seal carrier may for this purpose have a bolt which passes through passage openings in the radial flanges and the sliding body arranged between them and thus defines them.
  • the bolt can in particular be detachably or non-detachably fastened to the radial flanges, in particular screwed or riveted.
  • the sliding body can be accommodated in a passage opening, in particular a slot, of the guide blade arrangement, so that the fish-mouth seal carrier is suspended by means of spoke centering on the guide blade arrangement.
  • the sliding body can space and / or support the two radial flanges and thus improve the rigidity of the box profile.
  • an additional sheet may be fixed to the radial flange of the first or second half-shell element. It can be axially supported on the vane assembly and thus secure the fishmouth seal carrier axially.
  • the additional sheet may be arranged in an embodiment between the radial flange of the first half-shell element and the radial flange of the second half-shell element, in particular between the sliding body and a radial flange.
  • the additional sheet may be frictionally secured to the radial flange, in particular clamped between this and the slider, in particular by a bolt which connects the two radial flanges and / or superimposed on the slider.
  • a joint friction is impressed by the frictionally fixed additional sheet, which can advantageously damp vibrations.
  • the additional sheet can be firmly bonded to the radial flange, in particular welded to this.
  • the sealing element extends, at least substantially, axially from one to the other radial leg of the box section. In this way, a wide support surface can be provided and the box profile can be optimally used.
  • the sealing element has a honeycomb seal and a carrier, in particular a carrier plate, which is arranged on the outside of the axial leg, in particular cohesively, connected thereto, in particular soldered, welded or glued, and on whose axialschenkelabgewandten side the Honigwabendichtung, in particular cohesively, attached, in particular soldered, welded or glued.
  • the honeycomb seal can extend at least substantially axially from one to the other radial leg of the box profile and, in contrast, the carrier can project axially beyond one or both radial legs. This can protect the Honigwabendichtung especially with an axial rubbing.
  • At least one reinforcing element in particular a reinforcing plate, attached to one or both radial limbs of the box section, in particular cohesively, preferably by welding, soldering or gluing.
  • one or both radial legs may have an integral wall thickness thickening.
  • one or both half-shell elements are formed into a urine.
  • one or both half-shell elements in particular forging technology, can be reshaped.
  • one or both half shell elements are designed as sheet metal construction. In particular, they can have a wall thickness which is a maximum of 5 mm, in particular a maximum of 3 mm, preferably a maximum of 2 mm. Due to the box construction, high rigidity can thus be achieved in one embodiment, despite the low wall thickness and correspondingly low weight.
  • the two half-shell elements are firmly bonded together.
  • they can be welded together, preferably without additional material, in particular by laser or friction welding. This allows a light and reliable joint connection can be achieved.
  • they can also be glued or soldered together.
  • the two half-shell elements are connected to each other at impact, in particular with end faces of one axial leg of a U-profile of the half-shell elements. In this way, the weight can be reduced and / or the welding can be simplified.
  • half-shell elements can be connected to each other surface, in particular by welding of superimposed axial leg of the two half-shell elements.
  • the sealing element Before or after the cohesive bonding, the sealing element is arranged on an axial leg of the box profile. In particular, it may be made integral with one or both half-shell elements or connected to them prior to their connection. In a further development, the sealing element may be formed axially divided, wherein a part, in particular before the cohesive joining of the two half-shell elements together, with the first half-shell element and the other part is connected to the second half-shell element. Likewise, the sealing element can also be connected to the first and / or second half-shell element after the cohesive joining of the two half-shell elements.
  • the sealing element in particular a Honigwabendichtung or a connected thereto, preferably one-piece, carrier, a seam or joint of the cohesive joint connection of the two half-shell elements covers each other and thus secures the joint connection.
  • the sealing element can be connected to one or both half shell elements in a materially bonded manner, in particular welded, glued or soldered.
  • Fig. 1 shows in an axial section a part of a gas turbine with a vane arrangement with a plurality of vanes 10, at the radially inner (bottom in Fig. 1 ) Platform 11 a fishmouth seal carrier is suspended.
  • the fish-mouth seal carrier has a first half-shell element 1 and a second half-shell element 2 welded thereto, which together form a box profile with two substantially parallel axial limbs (1.1 + 2.1), (1.2 + 2.2) and two substantially parallel radial limbs 1.3, 2.3, which merge into each other in rounded corners.
  • a sealing element in the form of a stepped Honigwabendichtung 3 is disposed on an outer side of the radially inner axial leg (1.1 + 2.1).
  • the first and second half-shell elements each have an axial flange 1.4 and 2.4, respectively, for forming a fish mouth seal, which is formed integrally with the half-shell element and functions as a deflector of the fish-mouth seal. Opposite it radially lies the radially inner platform 11 of the vane arrangement. Radial between the platform 11 and the axial flange 1.4 and 2.4, respectively, an axial flange 20.1 and 21.1 of an adjacent blade assembly with blades 20 and 21 is arranged.
  • the axial flanges 1.4, 2.4 of the first and second half-shell elements extend substantially in the axial direction, wherein they have radial shoulders or steps.
  • the first half-shell element has a U-profile 1.1, 1.2, 1.3 to form the box profile and a thus formed integrally radial flange 1.5.
  • At the radial flange closes on the U-profile radially opposite side (above in Fig. 1 ) Axialflansch 1.4 to form the Fischmauldichtung.
  • the second half-shell element also has a radial flange 2.5 which is substantially parallel to the radial flange 1.5 of the first half-shell element and to which the axial flange 2.4 connects.
  • both half-shell elements joins on the axial flange 2.4 radially opposite side of the radial flange 2.5 a U-profile 2.1, 2.2, 2.3 to form the box profile, so that both half-shell elements each have a radial leg 1.3 and 2.3 and a part 1.1 or 2.1 of an axial leg (1.1 + 2.1) and a part 1.2 or 2.2 of the other axial leg (1.2 + 2.2) of the box profile form.
  • a slider 4 for suspending the fishmouth seal carrier on the vane arrangement is mounted on both sides between the radial flange 1.5 of the first half-shell element and the radial flange 2.5 of the second half-shell element.
  • the fish-mouth seal carrier on a bolt 5, which passes through openings in the radial flanges 1.5, 2.5 and arranged between these sliding body 4 and this determines.
  • the sliding body is received in a passage opening in the form of a slot 12 of the vane arrangement, so that the fish-mouth seal carrier is suspended by means of spoke centering on the vane arrangement.
  • the slider spaced the two radial flanges 1.5, 2.5 against each other and supports them against each other.
  • An additional plate 6 is fixed to the radial flange 1.5 of the first half-shell element. It is supported axially on the vane assembly and thus secures the fishmouth seal carrier axially.
  • the additional sheet is between the radial flange 1.5 of first half-shell element and the radial flange 2.5 of the second half-shell element, in particular the slider 4 and arranged by the bolt 5 frictionally fixed to the radial flange 1.5, in particular clamped between this and the slider 4.
  • the sealing element extends axially substantially from one radial leg 1.3 to the other radial leg 2.3 of the box section.
  • both half-shell elements 1.1-1.5, 2.1-2.5 are formed by casting molding or forging technology. Both half-shell elements are designed as sheet metal construction and have a wall thickness which is a maximum of 5 mm.
  • the two half-shell elements are then welded together without additional material, in particular by laser or friction welding. Both half-shell elements are connected to end faces of one axial limb 1.1, 2.1 of a U-profile of the half-shell elements in abutment with each other.
  • the sealing element 3 is arranged on the axial leg (1.1 + 2.1) of the box profile and welded thereto.
  • the sealing element 3 covers a seam or joint 7 of the cohesive joint connection of the two half-shell elements from each other and thus secures the joint connection.

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)

Abstract

The fish mouth seal carrier includes a seal (3) mounted on the radial inner axial arm (1.1,2.1) of the box profile. Either the primary half shell segment (1) or the second half shell segment (2) includes an integrally formed axial flange (1.4,2.4). The axial flange together with the radial inner platform (11) of the guide vane (10) of the gas turbine forms a fish mouth seal for accommodating the axial flange extending from the adjoining moving blade radially between the radial inner platform and the axial flange. Independent claims are also included for the following: (1) a gas turbine; and (2) a producing method for fish mouth seal carrier for guide vane arrangement of gas turbine.

Description

Die vorliegende Erfindung betrifft einen Fischmaul-Dichtungsträger für eine Leitschaufelanordnung einer Gasturbine, eine Leitschaufelanordnung bzw. Gasturbine mit einem solchen Fischmaul-Dichtungsträger sowie ein Verfahren zu dessen Herstellung.The present invention relates to a fish-mouth seal carrier for a guide vane assembly of a gas turbine, a vane assembly or gas turbine with such a fish-mouth seal carrier and a method for its production.

Aus der US 5,215,435 A ist eine Gasturbine mit einer Leitschaufelanordnung mit einer Plattform bekannt, an der ein Fischmaul-Dichtungsträger mit einer Honigwabendichtung befestigt ist. Der Fischmaul-Dichtungsträger ist aus insgesamt fünf Blechteilen zusammengesetzt: einem S-förmigen Blechteil zur Bildung einer FischmaulDichtung, einem L-förmigen Blechteil zur Bildung einer gegenüberliegenden Fischmaul-Dichtung, einem U-förmigen Blechteil, zwischen dessen Radialschenkeln ein Radialflansch der Plattform und ein Kopf einer Schraube angeordnet ist, einem C-förmigen Blechteil, in dem eine Unterlegscheibe aufgenommen ist, die die Schraube durchgreift, und schließlich einem G-förmigen Blechteil, welches das S-förmige Blechteil trägt, wobei die Honigwabendichtung an dem L- und dem G-förmigen Blechteil befestigt ist.From the US 5,215,435 A For example, a gas turbine with a vane assembly having a platform to which a fishmouth seal carrier is secured with a honeycomb seal is known. The fishmouth seal carrier is composed of a total of five sheet metal parts: an S-shaped sheet metal part to form a fishmouth gasket, an L-shaped sheet metal part to form an opposite fishmouth gasket, a U-shaped sheet metal part, a radial flange of the platform and a head between its radial legs a screw is arranged, a C-shaped sheet metal part in which a washer is received, which passes through the screw, and finally a G-shaped sheet metal part which carries the S-shaped sheet metal part, wherein the honeycomb seal on the L and the G is attached shaped sheet metal part.

Eine Aufgabe einer Ausführung der vorliegenden Erfindung ist es, die Herstellung und/oder den Betrieb einer Gasturbine zu verbessern.An object of an embodiment of the present invention is to improve the manufacture and / or operation of a gas turbine.

Diese Aufgabe wird durch einen Fischmaul-Dichtungsträger mit den Merkmalen des Anspruchs 1 gelöst. Die Ansprüche 7, 8 und 9 stellen eine Leitschaufelanordnung bzw. Gasturbine mit einem solchen Fischmaul-Dichtungsträger bzw. ein Verfahren zu dessen Herstellung unter Schutz. Vorteilhafte Weiterbildungen sind Gegenstand der Unteransprüche.This object is achieved by a fish-mouth seal carrier with the features of claim 1. The claims 7, 8 and 9 provide a guide vane assembly or gas turbine with such a fish-mouth seal carrier or a method for its production under protection. Advantageous developments are the subject of the dependent claims.

Nach einem Aspekt der vorliegenden Erfindung weist ein Fischmaul-Dichtungsträger für eine Leitschaufelanordnung einer Gasturbine ein erstes Halbschalenelement und ein damit stoffschlüssig verbundenes, insbesondere verschweißtes, zweites Halbschalenelement auf, welche zusammen ein Kastenprofil mit zwei Axialschenkeln und zwei Radialschenkeln bilden. Ein Dichtungselement, welches in einer Ausführung eine Honigwabendichtung aufweist, insbesondere sein kann, ist an einer Außenseite eines, in Einbaulage radial inneren, dieser Axialschenkel des Kastenprofils angeordnet.According to one aspect of the present invention, a fishmouth seal carrier for a guide vane assembly of a gas turbine on a first half-shell member and a materially connected thereto, in particular welded, second half-shell element, which together a box section with two axial legs and form two radial legs. A sealing element, which in one embodiment has a honeycomb seal, in particular can be, is arranged on an outer side of a, in installation position radially inner, this axial leg of the box profile.

Durch diese Kastenbauweise kann in einer Ausführung, insbesondere verglichen mit dem offenen Profil der US 5,215,435 A , das Betriebsverhalten, insbesondere eine Steifigkeit, des Fischmaul-Dichtungsträgers bzw. der Lagerung seines Dichtungselements verbessert werden. Unter einem Kastenprofil im Sinne der vorliegenden Erfindung wird insbesondere ein Profil verstanden, welches zwei, insbesondere wenigstens im Wesentlichen parallele, Axialschenkel und zwei, insbesondere wenigstens im Wesentlichen parallele, Radialschenkel aufweist, insbesondere hieraus besteht, die in einer Weiterbildung in vorzugsweise wenigstens im Wesentlichen rechtwinkligen, Ecken ineinander übergehen.Through this box construction, in one embodiment, in particular compared with the open profile of US 5,215,435 A , the operating behavior, in particular a rigidity of the fish mouth seal carrier or the storage of its sealing element can be improved. In the context of the present invention, a box profile is understood in particular to mean a profile which has two, in particular at least substantially parallel, axial legs and two, in particular at least substantially parallel, radial legs, in particular thereof, which in a further embodiment is preferably at least substantially rectangular , Corners merge into each other.

Das erste und/oder zweite Halbschalenelement weist jeweils einen Axialflansch zur Bildung einer Fischmauldichtung auf, der integral bzw. einteilig mit dem Halbschalenelement ausgebildet, insbesondere ur- oder umgeformt ist.The first and / or second half-shell element has in each case an axial flange for forming a fish mouth seal, which is formed integrally or integrally with the half-shell element, in particular, ur- or reshaped.

Durch diese integrale Bauweise kann in einer Ausführung, insbesondere verglichen mit den vielen Blechteilen der US 5,215,435 A , die Herstellung und/oder das Betriebsverhalten des Fischmaul-Dichtungsträgers verbessert werden.Due to this integral design can in one embodiment, in particular compared with the many sheet metal parts of US 5,215,435 A , the production and / or the performance of the fish mouth seal carrier are improved.

Der Axialflansch fungiert in einer Ausführung als sogenannter Deflektor der Fischmauldichtung. Ihm radial gegenüber liegt in einer Ausführung eine radial innere Plattform einer Leitschaufelanordnung mit einer oder mehreren Leitschaufeln, an der der Fischmaul-Dichtungsträger in einer Ausführung mittels einer Speichenzentrierung aufgehängt ist. Radial zwischen der Plattform und dem Axialflansch ist ein Axialflansch einer benachbarten Laufschaufelanordnung mit einer oder mehreren Laufschaufeln angeordnet. Wie vorstehend ausgeführt, kann eine Fischmauldichtung stromauf- und/oder abwärts der Leitschaufelanordnung ausgebildet sein bzw. das erste und/oder zweite Halbschalenelement des Fischmaul-Dichtungsträgers einen entsprechenden, als Deflektor ausgebildeten Axialflansch aufweisen. Der Axialflansch des ersten und/oder zweiten Halbschalenelements erstreckt sich in einer Ausführung, wenigstens im Wesentlichen, in axialer Richtung. Dabei kann er radiale Absätze bzw. Stufen aufweisen.The Axialflansch acts in one embodiment as a so-called deflector of Fischmauldichtung. Opposite it radially in one embodiment is a radially inner platform of a vane assembly having one or more vanes to which the fishmouth seal carrier in one embodiment is suspended by means of a spoke centering. Radial between the platform and the axial flange, an axial flange of an adjacent blade assembly is arranged with one or more blades. As stated above, a Fischmauldichtung upstream and / or downstream of the vane assembly may be formed or have the first and / or second half-shell element of the fish-mouth seal carrier having a corresponding, designed as a deflector Axialflansch. The axial flange of the first and / or second half-shell element extends in one embodiment, at least substantially, in the axial direction. He may have radial paragraphs or steps.

In einer Ausführung weist das erste Halbschalenelement ein U-Profil zur Bildung des Kastenprofils und einen damit integral ausgebildeten Radialflansch auf. An den Radialflansch kann sich in einer Ausführung auf der dem U-Profil radial gegenüberliegenden Seite der Axialflansch zur Bildung einer Fischmauldichtung anschließen.In one embodiment, the first half-shell element has a U-profile for forming the box profile and a radial flange formed integrally therewith. In one embodiment, the radial flange can be followed by the axial flange on the side opposite the U-profile to form a fish gauge.

Das zweite Halbschalenelement kann einen Radialflansch aufweisen, an den sich in einer Ausführung der Axialflansch zur Bildung einer Fischmauldichtung anschließen kann. Auf der diesem Axialflansch radial gegenüberliegenden Seite kann der Radialflansch zusammen mit dem U-Profil des ersten Halbschalenelements das Kastenprofil bilden, d.h. das U-Profil deckelartig abschließen und im Wesentlichen einen Radialschenkel des U-Profils bilden. In einer alternativen Ausführung schließt sich auch bei dem zweiten Halbschalenelement auf der dem Axialflansch radial gegenüberliegenden Seite an den Radialflansch ein U-Profil zur Bildung des Kastenprofils an, so dass beide Halbschalenelemente jeweils einen Radialschenkel und jeweils einen Teil der beiden Axialschenkel des Kastenprofils bilden.The second half-shell element can have a radial flange, to which the axial flange can connect in one embodiment to form a fish-measuring direction. On the radially opposite side of this axial flange, the radial flange, together with the U-profile of the first half-shell element, can form the box profile, i. Completing the U-shaped profile lid-like and essentially form a radial leg of the U-profile. In an alternative embodiment, a U-profile for forming the box profile also connects to the radial flange on the second half-shell element on the axial flange, so that both half-shell elements each form a radial leg and in each case a part of the two axial legs of the box profile.

In einer Ausführung ist ein Gleitkörper zur Aufhängung des Fischmaul-Dichtungsträgers an der Leitschaufelanordnung zwischen dem Radialflansch des ersten Halbschalenelements und dem Radialflansch des zweiten Halbschalenelements beidseitig gelagert. Insbesondere kann der Fischmaul-Dichtungsträger hierzu einen Bolzen aufweisen, der Durchgangsöffnungen in den Radialflanschen und dem zwischen diesen angeordneten Gleitkörper durchgreift und diesen so festlegt. Der Bolzen kann insbesondere lösbar oder unlösbar an den Radialflanschen befestigt, insbesondere verschraubt oder vernietet, sein. Der Gleitkörper kann in einer Ausführung in einer Durchgangsöffnung, insbesondere einem Langloch, der Leitschaufelanordnung aufgenommen sein, so dass der Fischmaul-Dichtungsträger mittels Speichenzentrierung an der Leitschaufelanordnung aufgehängt ist. Der Gleitkörper kann insbesondere die beiden Radialflansche gegeneinander beabstanden und/oder abstützen und so die Steifigkeit des Kastenprofils verbessern.In one embodiment, a slider for suspending the fishmouth seal carrier on the vane assembly between the radial flange of the first half-shell member and the radial flange of the second half-shell member is mounted on both sides. In particular, the fish-mouth seal carrier may for this purpose have a bolt which passes through passage openings in the radial flanges and the sliding body arranged between them and thus defines them. The bolt can in particular be detachably or non-detachably fastened to the radial flanges, in particular screwed or riveted. In one embodiment, the sliding body can be accommodated in a passage opening, in particular a slot, of the guide blade arrangement, so that the fish-mouth seal carrier is suspended by means of spoke centering on the guide blade arrangement. In particular, the sliding body can space and / or support the two radial flanges and thus improve the rigidity of the box profile.

Zusätzlich oder alternativ kann ein Zusatzblech an dem Radialflansch des ersten oder zweiten Halbschalenelements festgelegt sein. Es kann sich axial an der Leitschaufelanordnung abstützen und so den Fischmaul-Dichtungsträger axial sichern. Das Zusatzblech kann in einer Ausführung zwischen dem Radialflansch des ersten Halbschalenelements und dem Radialflansch des zweiten Halbschalenelements angeordnet sein, insbesondere zwischen dem Gleitkörper und einem Radialflansch. In einer Ausführung kann das Zusatzblech reibschlüssig an dem Radialflansch festgelegt, insbesondere zwischen diesem und dem Gleitkörper geklemmt sein, insbesondere durch einen Bolzen, der die beiden Radialflansche verbindet und/oder den Gleitkörper lagert. In einer Ausführung wird durch das reibschlüssig festgelegte Zusatzblech eine Fügereibung eingeprägt, die vorteilhaft Schwingungen dämpfen kann. Gleichermaßen kann das Zusatzblech stoffschlüssig an dem Radialflansch festgelegt, insbesondere mit diesem verschweißt sein.Additionally or alternatively, an additional sheet may be fixed to the radial flange of the first or second half-shell element. It can be axially supported on the vane assembly and thus secure the fishmouth seal carrier axially. The additional sheet may be arranged in an embodiment between the radial flange of the first half-shell element and the radial flange of the second half-shell element, in particular between the sliding body and a radial flange. In one embodiment, the additional sheet may be frictionally secured to the radial flange, in particular clamped between this and the slider, in particular by a bolt which connects the two radial flanges and / or superimposed on the slider. In one embodiment, a joint friction is impressed by the frictionally fixed additional sheet, which can advantageously damp vibrations. Similarly, the additional sheet can be firmly bonded to the radial flange, in particular welded to this.

In einer Ausführung erstreckt sich das Dichtungselement, wenigstens im Wesentlichen, axial von dem einen zu dem anderen Radialschenkel des Kastenprofils. Auf diese Weise kann eine breite Abstützfläche bereitgestellt und das Kastenprofil optimal genutzt werden. In einer Ausführung weist das Dichtungselement eine Honigwabendichtung und einen Träger, insbesondere ein Trägerblech, auf, der bzw. das an der Außenseite des Axialschenkels angeordnet, insbesondere stoffschlüssig, mit diesem verbunden, insbesondere verlötet, verschweißt oder verklebt ist, und an dessen axialschenkelabgewandten Seite die Honigwabendichtung, insbesondere stoffschlüssig, befestigt, insbesondere verlötet, verschweißt oder verklebt ist. In einer Weiterbildung kann sich die Honigwabendichtung wenigstens im Wesentlichen axial von dem einen zu dem anderen Radialschenkel des Kastenprofils erstrecken und der Träger demgegenüber axial über einen oder beide Radialschenkel überstehen. Dies kann insbesondere bei einem axialen Anstreifen die Honigwabendichtung schützen.In one embodiment, the sealing element extends, at least substantially, axially from one to the other radial leg of the box section. In this way, a wide support surface can be provided and the box profile can be optimally used. In one embodiment, the sealing element has a honeycomb seal and a carrier, in particular a carrier plate, which is arranged on the outside of the axial leg, in particular cohesively, connected thereto, in particular soldered, welded or glued, and on whose axialschenkelabgewandten side the Honigwabendichtung, in particular cohesively, attached, in particular soldered, welded or glued. In a further development, the honeycomb seal can extend at least substantially axially from one to the other radial leg of the box profile and, in contrast, the carrier can project axially beyond one or both radial legs. This can protect the Honigwabendichtung especially with an axial rubbing.

In einer Ausführung ist an einem oder beiden Radialschenkeln des Kastenprofils wenigstens ein Verstärkungselement, insbesondere ein Verstärkungsblech, befestigt, insbesondere stoffschlüssig, vorzugsweise durch Verschweißen, Verlöten oder Verkleben. Zusätzlich oder alternativ können ein oder beide Radialschenkel eine integrale Wandstärkenaufdickung aufweisen. Durch diese separat angebrachte und/oder integral ausgeführte Verstärkung des bzw. der Radialschenkel kann in einer Ausführung die Robustheit gegen ein axiales Anstreifen erhöht werden.In one embodiment, at least one reinforcing element, in particular a reinforcing plate, attached to one or both radial limbs of the box section, in particular cohesively, preferably by welding, soldering or gluing. Additionally or alternatively, one or both radial legs may have an integral wall thickness thickening. Through these separately attached and / or integral Running reinforcement of the radial leg or in one embodiment, the robustness against axial rubbing be increased.

Zur Herstellung eines Fischmaul-Dichtungsträgers nach einem Aspekt der vorliegenden Erfindung werden ein oder beide Halbschalenelemente, insbesondere gusstechnisch, urgeformt. Gleichermaßen können ein oder beide Halbschalenelemente, insbesondere schmiedetechnisch, umgeformt werden. In einer Ausführung sind ein oder beide Halbschalenelemente als Blechkonstruktion ausgebildet. Insbesondere können sie eine Wandstärke aufweisen, die maximal 5 mm, insbesondere maximal 3 mm, vorzugsweise maximal 2 mm beträgt. Durch die Kastenbauweise kann in einer Ausführung so trotz geringer Wandstärke und entsprechend geringem Gewicht eine hohe Steifigkeit erreicht werden.For producing a fish-mouth seal carrier according to one aspect of the present invention, one or both half-shell elements, in particular casting technology, are formed into a urine. Similarly, one or both half-shell elements, in particular forging technology, can be reshaped. In one embodiment, one or both half shell elements are designed as sheet metal construction. In particular, they can have a wall thickness which is a maximum of 5 mm, in particular a maximum of 3 mm, preferably a maximum of 2 mm. Due to the box construction, high rigidity can thus be achieved in one embodiment, despite the low wall thickness and correspondingly low weight.

Die beiden Halbschalenelemente werden stoffschlüssig miteinander verbunden. Sie können insbesondere miteinander verschweißt werden, vorzugsweise ohne Zusatzwerkstoff, insbesondere durch Laser- oder Reibschweißen. Hierdurch kann eine leichte und prozesssichere Fügeverbindung erreicht werden. Gleichermaßen können sie auch miteinander verklebt oder gelötet werden.The two half-shell elements are firmly bonded together. In particular, they can be welded together, preferably without additional material, in particular by laser or friction welding. This allows a light and reliable joint connection can be achieved. Likewise, they can also be glued or soldered together.

In einer Ausführung werden die beiden Halbschalenelemente auf Stoß, insbesondere mit Stirnseiten von je einem Axialschenkel eines U-Profils der Halbschalenelemente, miteinander verbunden. Auf diese Weise kann das Gewicht reduziert und/oder das Schweißen vereinfacht werden. Gleichermaßen können Halbschalenelemente flächig miteinander verbunden werden, insbesondere durch Verschweißen von einander überlagemder Axialschenkel der beiden Halbschalenelemente.In one embodiment, the two half-shell elements are connected to each other at impact, in particular with end faces of one axial leg of a U-profile of the half-shell elements. In this way, the weight can be reduced and / or the welding can be simplified. Similarly, half-shell elements can be connected to each other surface, in particular by welding of superimposed axial leg of the two half-shell elements.

Vor oder nach dem stoffschlüssigen Verbinden wird das Dichtungselement an einem Axialschenkel des Kastenprofils angeordnet. Insbesondere kann es integral mit einem oder beiden Halbschalenelementen hergestellt oder vor deren Verbindung mit diesen verbunden werden. In einer Weiterbildung kann das Dichtungselement axial geteilt ausgebildet sein, wobei ein Teil, insbesondere vor dem stoffschlüssigen Verbinden der beiden Halbschalenelemente miteinander, mit dem ersten Halbschalenelement und der andere Teil mit dem zweiten Halbschalenelement verbunden wird. Gleichermaßen kann das Dichtungselement auch nach dem stoffschlüssigen Verbinden der beiden Halbschalenelemente miteinander mit dem ersten und/oder zweiten Halbschalenelement verbunden werden. In einer Ausführung deckt das Dichtungselement, insbesondere eine Honigwabendichtung oder ein mit dieser verbundener, vorzugsweise einstückiger, Träger, eine Naht- bzw. Stoßstelle der stoffschlüssigen Fügeverbindung der beiden Halbschalenelemente miteinander ab und sichert so die Fügeverbindung. Das Dichtungselement kann insbesondere stoffschlüssig mit einem oder beiden Halbschalenelementen verbunden werden, insbesondere verschweißt, - klebt oder -lötet.Before or after the cohesive bonding, the sealing element is arranged on an axial leg of the box profile. In particular, it may be made integral with one or both half-shell elements or connected to them prior to their connection. In a further development, the sealing element may be formed axially divided, wherein a part, in particular before the cohesive joining of the two half-shell elements together, with the first half-shell element and the other part is connected to the second half-shell element. Likewise, the sealing element can also be connected to the first and / or second half-shell element after the cohesive joining of the two half-shell elements. In one embodiment, the sealing element, in particular a Honigwabendichtung or a connected thereto, preferably one-piece, carrier, a seam or joint of the cohesive joint connection of the two half-shell elements covers each other and thus secures the joint connection. In particular, the sealing element can be connected to one or both half shell elements in a materially bonded manner, in particular welded, glued or soldered.

Weitere Vorteile und Merkmale ergeben sich aus den Unteransprüchen und dem Ausführungsbeispiel. Hierzu zeigt, teilweise schematisiert, die einzige

Fig. 1:
einen Fischmaul-Dichtungsträger einer Leitschaufelanordnung einer Gasturbine nach einer Ausführung der vorliegenden Erfindung in einem Axialschnitt.
Further advantages and features emerge from the subclaims and the exemplary embodiment. This shows, partially schematized, the only one
Fig. 1:
a fishmouth seal carrier a guide vane assembly of a gas turbine according to an embodiment of the present invention in an axial section.

Fig. 1 zeigt in einem Axialschnitt einen Teil einer Gasturbine mit einer Leitschaufelanordnung mit mehreren Leitschaufeln 10, an deren radial innerer (unten in Fig. 1) Plattform 11 ein Fischmaul-Dichtungsträger aufgehängt ist. Fig. 1 shows in an axial section a part of a gas turbine with a vane arrangement with a plurality of vanes 10, at the radially inner (bottom in Fig. 1 ) Platform 11 a fishmouth seal carrier is suspended.

Der Fischmaul-Dichtungsträger weist ein erstes Halbschalenelement 1 und ein damit verschweißtes zweites Halbschalenelement 2 auf, welche zusammen ein Kastenprofil mit zwei im Wesentlichen parallelen Axialschenkeln (1.1 + 2.1), (1.2 + 2.2) und zwei im Wesentlichen parallelen Radialschenkeln 1.3, 2.3 bilden, die in abgerundeten Ecken ineinander übergehen. Ein Dichtungselement in Form einer gestuften Honigwabendichtung 3 ist an einer Außenseite des radial inneren Axialschenkels (1.1 + 2.1) angeordnet.The fish-mouth seal carrier has a first half-shell element 1 and a second half-shell element 2 welded thereto, which together form a box profile with two substantially parallel axial limbs (1.1 + 2.1), (1.2 + 2.2) and two substantially parallel radial limbs 1.3, 2.3, which merge into each other in rounded corners. A sealing element in the form of a stepped Honigwabendichtung 3 is disposed on an outer side of the radially inner axial leg (1.1 + 2.1).

Das erste und zweite Halbschalenelement weist jeweils einen Axialflansch 1.4 bzw. 2.4 zur Bildung einer Fischmauldichtung auf, der integral bzw. einteilig mit dem Halbschalenelement ausgebildet ist und als Deflektor der Fischmauldichtung fungiert. Ihm radial gegenüber liegt die radial innere Plattform 11 der Leitschaufelanordnung. Radial zwischen der Plattform 11 und dem Axialflansch 1.4 bzw. 2.4 ist jeweils ein Axialflansch 20.1 bzw. 21.1 einer benachbarten Laufschaufelanordnung mit Laufschaufeln 20 bzw. 21 angeordnet. Die Axialflansche 1.4, 2.4 des ersten und zweiten Halbschalenelements erstrecken sich im Wesentlichen in axialer Richtung, wobei sie radiale Absätze bzw. Stufen aufweisen.The first and second half-shell elements each have an axial flange 1.4 and 2.4, respectively, for forming a fish mouth seal, which is formed integrally with the half-shell element and functions as a deflector of the fish-mouth seal. Opposite it radially lies the radially inner platform 11 of the vane arrangement. Radial between the platform 11 and the axial flange 1.4 and 2.4, respectively, an axial flange 20.1 and 21.1 of an adjacent blade assembly with blades 20 and 21 is arranged. The axial flanges 1.4, 2.4 of the first and second half-shell elements extend substantially in the axial direction, wherein they have radial shoulders or steps.

Das erste Halbschalenelement weist ein U-Profil 1.1, 1.2, 1.3 zur Bildung des Kastenprofils und einen damit integral ausgebildeten Radialflansch 1.5 auf. An den Radialflansch schließt sich auf der dem U-Profil radial gegenüberliegenden Seite (oben in Fig. 1) der Axialflansch 1.4 zur Bildung der Fischmauldichtung an. Das zweite Halbschalenelement weist ebenfalls einen Radialflansch 2.5 auf, der zu dem Radialflansch 1.5 des ersten Halbschalenelements im Wesentlichen parallel ist und an den sich der Axialflansch 2.4 anschließt. Auch bei dem zweiten Halbschalenelement schließt sich auf der dem Axialflansch 2.4 radial gegenüberliegenden Seite an den Radialflansch 2.5 ein U-Profil 2.1, 2.2, 2.3 zur Bildung des Kastenprofils an, so dass beide Halbschalenelemente jeweils einen Radialschenkel 1.3 bzw. 2.3 und jeweils einen Teil 1.1 bzw. 2.1 des einen Axialschenkels (1.1 + 2.1) und einen Teil 1.2 bzw. 2.2 des anderen Axialschenkels (1.2 + 2.2) des Kastenprofils bilden.The first half-shell element has a U-profile 1.1, 1.2, 1.3 to form the box profile and a thus formed integrally radial flange 1.5. At the radial flange closes on the U-profile radially opposite side (above in Fig. 1 ) Axialflansch 1.4 to form the Fischmauldichtung. The second half-shell element also has a radial flange 2.5 which is substantially parallel to the radial flange 1.5 of the first half-shell element and to which the axial flange 2.4 connects. Also in the second half-shell element joins on the axial flange 2.4 radially opposite side of the radial flange 2.5 a U-profile 2.1, 2.2, 2.3 to form the box profile, so that both half-shell elements each have a radial leg 1.3 and 2.3 and a part 1.1 or 2.1 of an axial leg (1.1 + 2.1) and a part 1.2 or 2.2 of the other axial leg (1.2 + 2.2) of the box profile form.

Ein Gleitkörper 4 zur Aufhängung des Fischmaul-Dichtungsträgers an der Leitschaufelanordnung ist zwischen dem Radialflansch 1.5 des ersten Halbschalenelements und dem Radialflansch 2.5 des zweiten Halbschalenelements beidseitig gelagert. Hierzu weist der Fischmaul-Dichtungsträger einen Bolzen 5 auf, der Durchgangsöffnungen in den Radialflanschen 1.5, 2.5 und dem zwischen diesen angeordneten Gleitkörper 4 durchgreift und diesen so festlegt. Der Gleitkörper ist in einer Durchgangsöffnung in Form eines Langlochs 12 der Leitschaufelanordnung aufgenommen, so dass der Fischmaul-Dichtungsträger mittels Speichenzentrierung an der Leitschaufelanordnung aufgehängt ist. Der Gleitkörper beabstandet die beiden Radialflansche 1.5, 2.5 gegeneinander und stützt sie gegeneinander ab.A slider 4 for suspending the fishmouth seal carrier on the vane arrangement is mounted on both sides between the radial flange 1.5 of the first half-shell element and the radial flange 2.5 of the second half-shell element. For this purpose, the fish-mouth seal carrier on a bolt 5, which passes through openings in the radial flanges 1.5, 2.5 and arranged between these sliding body 4 and this determines. The sliding body is received in a passage opening in the form of a slot 12 of the vane arrangement, so that the fish-mouth seal carrier is suspended by means of spoke centering on the vane arrangement. The slider spaced the two radial flanges 1.5, 2.5 against each other and supports them against each other.

Ein Zusatzblech 6 ist an dem Radialflansch 1.5 des ersten Halbschalenelements festgelegt. Es stützt sich axial an der Leitschaufelanordnung ab und sichert so den Fischmaul-Dichtungsträger axial. Das Zusatzblech ist zwischen dem Radialflansch 1.5 des ersten Halbschalenelements und dem Radialflansch 2.5 des zweiten Halbschalenelements, insbesondere dem Gleitkörper 4 angeordnet und durch den Bolzen 5 reibschlüssig an dem Radialflansch 1.5 festgelegt, insbesondere zwischen diesem und dem Gleitkörper 4 geklemmt.An additional plate 6 is fixed to the radial flange 1.5 of the first half-shell element. It is supported axially on the vane assembly and thus secures the fishmouth seal carrier axially. The additional sheet is between the radial flange 1.5 of first half-shell element and the radial flange 2.5 of the second half-shell element, in particular the slider 4 and arranged by the bolt 5 frictionally fixed to the radial flange 1.5, in particular clamped between this and the slider 4.

Das Dichtungselement erstreckt sich axial im Wesentlichen von dem einen Radialschenkel 1.3 zu dem anderen Radialschenkel 2.3 des Kastenprofils.The sealing element extends axially substantially from one radial leg 1.3 to the other radial leg 2.3 of the box section.

Zur Herstellung des Fischmaul-Dichtungsträgers werden beide Halbschalenelemente 1.1-1.5, 2.1-2.5 gusstechnisch urgeformt oder schmiedetechnisch umgeformt. Beide Halbschalenelemente sind als Blechkonstruktion ausgebildet und weisen eine Wandstärke auf, die maximal 5 mm beträgt.To produce the fish-mouth seal carrier, both half-shell elements 1.1-1.5, 2.1-2.5 are formed by casting molding or forging technology. Both half-shell elements are designed as sheet metal construction and have a wall thickness which is a maximum of 5 mm.

Die beiden Halbschalenelemente werden anschließend miteinander ohne Zusatzwerkstoff verschweißt, insbesondere durch Laser- oder Reibschweißen. Beide Halbschalenelemente werden mit Stirnseiten von je einem Axialschenkel 1.1, 2.1 eines U-Profils der Halbschalenelemente auf Stoß miteinander verbunden.The two half-shell elements are then welded together without additional material, in particular by laser or friction welding. Both half-shell elements are connected to end faces of one axial limb 1.1, 2.1 of a U-profile of the half-shell elements in abutment with each other.

Nach dem stoffschlüssigen Verbinden wird das Dichtungselement 3 an dem Axialschenkel (1.1 + 2.1) des Kastenprofils angeordnet und mit diesem verschweißt. Dabei deckt das Dichtungselement 3 eine Naht- bzw. Stoßstelle 7 der stoffschlüssigen Fügeverbindung der beiden Halbschalenelemente miteinander ab und sichert so die Fügeverbindung.After the integral connection, the sealing element 3 is arranged on the axial leg (1.1 + 2.1) of the box profile and welded thereto. Here, the sealing element 3 covers a seam or joint 7 of the cohesive joint connection of the two half-shell elements from each other and thus secures the joint connection.

BezugszeichenlisteLIST OF REFERENCE NUMBERS

1/21.2
erstes/zweites Halbschalenelementfirst / second half-shell element
1.1/2.11.1 / 2.1
Axialschenkel des U-Profils des ersten/zweiten HalbschalenelementsAxial leg of the U-profile of the first / second half-shell element
1.2/2.21.2 / 2.2
Axialschenkel des U-Profils des ersten/zweiten HalbschalenelementsAxial leg of the U-profile of the first / second half-shell element
1.3/2.31.3 / 2.3
Radialschenkel des U-Profils des ersten/zweiten HalbschalenelementsRadial leg of the U-profile of the first / second half-shell element
1.4/2.41.4 / 2.4
Axialflansch des ersten/zweiten HalbschalenelementsAxial flange of the first / second half-shell element
1.5/2.51.5 / 2.5
Radialflansch des ersten/zweiten HalbschalenelementsRadial flange of the first / second half-shell element
33
Honigwabendichtung (Dichtungselement)Honeycomb seal (sealing element)
44
Gleitkörpersliding
55
Bolzenbolt
66
Zusatzblechadditional sheet
77
Naht- bzw. Stoßstelle (Fügestelle)Seam or joint (joint)
1010
Leitschaufel(anordnung)Vane (arrangement)
1111
radial innere Plattformradially inner platform
1212
LanglochLong hole
20/2120/21
Laufschaufel(anordnung)Blade (arrangement)
20.1/21.120.1 / 21.1
Axialflansch der Laufschaufel(anordnung) 20/21Blade axial flange (arrangement) 20/21

Claims (10)

Fischmaul-Dichtungsträger für eine Leitschaufelanordnung (10) einer Gasturbine, mit einem ersten Halbschalenelement (1) und einem damit stoffschlüssig (7) verbundenen zweiten Halbschalenelement (2), welche zusammen ein Kastenprofil mit zwei Axialschenkeln (1.1 + 2.1, 1.2 + 2.2) und zwei Radialschenkeln (1.3, 2.3) bilden, und einem Dichtungselement (3), welches an einem Axialschenkel (1.1 + 2.1) des Kastenprofils angeordnet ist, wobei wenigstens eines von den beiden Halbschalenelementen einen integral ausgebildeten Axialflansch (1.4, 2.4) zur Bildung einer Fischmauldichtung aufweist.Fishmouth seal carrier for a stator blade assembly (10) of a gas turbine, with a first half-shell element (1) and a cohesively connected (7) second half-shell element (2), which together a box section with two axial limbs (1.1 + 2.1, 1.2 + 2.2) and two radial arms (1.3, 2.3) form, and a sealing element (3) which is arranged on an axial leg (1.1 + 2.1) of the box profile, wherein at least one of the two half-shell elements has an integrally formed Axialflansch (1.4, 2.4) for forming a Fischmauldichtung having. Fischmaul-Dichtungsträger nach dem vorhergehenden Anspruch, dadurch gekennzeichnet, dass das erste und/oder zweite Halbschalenelement ein U-Profil (1.1 - 1.3, 2.1 - 2.3) zur Bildung des Kastenprofils und einen damit integral ausgebildeten Radialflansch (1.5, 2.5) aufweisen.Fish-mouth seal carrier according to the preceding claim, characterized in that the first and / or second half-shell element have a U-profile (1.1 - 1.3, 2.1 - 2.3) for forming the box profile and a thus integrally formed radial flange (1.5, 2.5). Fischmaul-Dichtungsträger nach dem vorhergehenden Anspruch, gekennzeichnet durch einen Gleitkörper (4) zur Aufhängung des Fischmaul-Dichtungsträgers an der Leitschaufelanordnung, welcher zwischen dem Radialflansch des ersten Halbschalenelements und dem Radialflansch des zweiten Halbschalenelements beidseitig gelagert ist, und/oder durch ein Zusatzblech (6), welches an dem Radialflansch des ersten oder zweiten Halbschalenelements reib- oder stoffschlüssig festgelegt ist.Fish-mouth seal carrier according to the preceding claim, characterized by a sliding body (4) for suspending the fish-mouth seal carrier on the vane arrangement, which is mounted on both sides between the radial flange of the first half-shell element and the radial flange of the second half-shell element, and / or by an additional sheet (6 ), which is frictionally or cohesively fixed to the radial flange of the first or second half-shell element. Fischmaul-Dichtungsträger nach einem der vorhergehenden Ansprüche, dadurch gekennzeichnet, dass das Dichtungselement eine Honigwabendichtung (3) aufweist und/oder sich, wenigstens im Wesentlichen, axial von dem einen zu dem anderen Radialschenkel des Kastenprofils erstreckt.Fish-mouth seal carrier according to one of the preceding claims, characterized in that the sealing element has a Honigwabendichtung (3) and / or extends, at least substantially, axially from one to the other radial leg of the box section. Fischmaul-Dichtungsträger nach einem der vorhergehenden Ansprüche, dadurch gekennzeichnet, dass der Axialflansch des ersten und/oder zweiten Halbschalenelements sich, wenigstens im Wesentlichen, in axialer Richtung erstreckt.Fish-mouth seal carrier according to one of the preceding claims, characterized in that the axial flange of the first and / or second half-shell element extends, at least substantially, in the axial direction. Fischmaul-Dichtungsträger nach einem der vorhergehenden Ansprüche, dadurch gekennzeichnet, dass es nach einem Verfahren nach Anspruch 9 oder einem darauf rückbezogenen Anspruch hergestellt ist.Fishmouth seal carrier according to one of the preceding claims, characterized in that it is produced by a method according to claim 9 or a claim relating thereto. Leitschaufelanordnung (10) für eine Gasturbine, mit einem Fischmaul-Dichtungsträger nach einem der vorhergehenden Ansprüche und einer radial inneren Plattform (11), die zusammen mit wenigstens einem Axialflansch (1.4, 2.4) des Fischmaul-Dichtungsträgers eine Fischmauldichtung zur Aufnahme eines Axialflansches (20.1, 21.1) einer benachbarten Laufschaufelanordnung (20, 21) radial zwischen der Plattform und dem Axialflansch bildet.A guide vane assembly (10) for a gas turbine having a fishmouth seal carrier according to any one of the preceding claims and a radially inner platform (11) which together with at least one axial flange (1.4, 2.4) of the fishmouth seal carrier comprises a fishmouth seal for receiving an axial flange (20.1 , 21.1) of an adjacent blade assembly (20, 21) forms radially between the platform and the axial flange. Gasturbine, insbesondere Gasturbinen-Triebwerk, mit einer Leitschaufelanordnung (10) nach dem vorhergehenden Anspruch und wenigstens einer benachbarten Laufschaufelanordnung (20, 21) mit einem Axialflansch (20.1, 21.1), der radial zwischen der Plattform (11) und einem Axialflansch (1.4, 2.4) eines Halbschalenelements (1, 2) des Fischmaul-Dichtungsträgers angeordnet ist.A gas turbine, in particular a gas turbine engine, with a vane arrangement (10) according to the preceding claim and at least one adjacent rotor blade arrangement (20, 21) with an axial flange (20.1, 21.1), which is arranged radially between the platform (11) and an axial flange (1.4, 2.4) of a half-shell element (1, 2) of the fish-mouth seal carrier is arranged. Verfahren zur Herstellung eines Fischmaul-Dichtungsträgers nach einem der vorhergehenden Ansprüche, mit den Schritten: - Urformen, insbesondere Gießen, und/oder Umformen, insbesondere Schmieden, wenigstens eines Halbschalenelements (1, 2); - stoffschlüssiges Verbinden dieses Halbschalenelements mit dem anderen Halbschalenelement; und - Anordnen des Dichtungselements (3) an einem Axialschenkel (1.1 + 2.1) des Kastenprofils. A method of making a fishmouth seal carrier according to any one of the preceding claims, comprising the steps of: - primary molds, in particular casting, and / or forming, in particular forging, at least one half-shell element (1, 2); - integral connection of this half-shell element with the other half-shell element; and - Arranging the sealing element (3) on an axial leg (1.1 + 2.1) of the box profile. Verfahren nach dem vorhergehenden Anspruch, wobei die beiden Halbschalenelemente auf Stoß (7) an Stirnseiten ihrer Axialschenkel miteinander stoffschlüssig verbunden, insbesondere verschweißt werden.Method according to the preceding claim, wherein the two half-shell elements are integrally connected, in particular welded, to each other at the ends (7) of end faces of their axial limbs.
EP12188822.6A 2012-10-17 2012-10-17 Seal holder for a stator assembly Not-in-force EP2722486B1 (en)

Priority Applications (2)

Application Number Priority Date Filing Date Title
EP12188822.6A EP2722486B1 (en) 2012-10-17 2012-10-17 Seal holder for a stator assembly
US14/056,876 US9856736B2 (en) 2012-10-17 2013-10-17 Fish mouth seal carrier

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
EP12188822.6A EP2722486B1 (en) 2012-10-17 2012-10-17 Seal holder for a stator assembly

Publications (2)

Publication Number Publication Date
EP2722486A1 true EP2722486A1 (en) 2014-04-23
EP2722486B1 EP2722486B1 (en) 2016-12-07

Family

ID=47071165

Family Applications (1)

Application Number Title Priority Date Filing Date
EP12188822.6A Not-in-force EP2722486B1 (en) 2012-10-17 2012-10-17 Seal holder for a stator assembly

Country Status (2)

Country Link
US (1) US9856736B2 (en)
EP (1) EP2722486B1 (en)

Cited By (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP2960555A1 (en) * 2014-06-25 2015-12-30 MTU Aero Engines GmbH Brush seal system for sealing a gap between components of a turbomachine which can be moved relative to each other
FR3039589A1 (en) * 2015-07-28 2017-02-03 Snecma STAGE OF TURBOMACHINE, ESPECIALLY LOW-PRESSURE TURBINE
EP3208426A1 (en) 2016-02-18 2017-08-23 MTU Aero Engines GmbH Guide blade formation for a flow machine
EP3409897A1 (en) * 2017-05-29 2018-12-05 MTU Aero Engines GmbH Seal assembly for a turbomachine, method for producing a seal assembly and turbomachine
EP3483399A1 (en) * 2017-11-09 2019-05-15 MTU Aero Engines GmbH Seal assembly for a turbomachine, method for producing a seal assembly and turbomachine
EP3517734A1 (en) * 2018-01-29 2019-07-31 MTU Aero Engines GmbH Sealing module for a turbomachine
IT201900013218A1 (en) * 2019-07-29 2021-01-29 Ge Avio Srl INTERNAL BAND FOR TURBINE ENGINE.
WO2021186135A1 (en) * 2020-03-19 2021-09-23 Safran Aircraft Engines Turbomachine rotary assembly comprising an annular clamping part
FR3113298A1 (en) * 2020-08-10 2022-02-11 Safran Aircraft Engines Abradable holder of a low pressure distributor comprising a single sheet
EP4345251A1 (en) * 2022-09-22 2024-04-03 MTU Aero Engines AG Module for a fluid flow machine

Families Citing this family (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102013212465B4 (en) * 2013-06-27 2015-03-12 MTU Aero Engines AG Sealing arrangement for a turbomachine, a vane assembly and a turbomachine with such a sealing arrangement
EP2818643B1 (en) * 2013-06-27 2018-08-08 MTU Aero Engines GmbH Sealing device and turbo-machine
DE102016222608A1 (en) * 2016-11-17 2018-05-17 MTU Aero Engines AG Sealing arrangement for a guide vane arrangement of a gas turbine
DE102017209420A1 (en) 2017-06-02 2018-12-06 MTU Aero Engines AG Sealing arrangement with welded sealing plate, turbomachine and manufacturing process
DE102018210513A1 (en) * 2018-06-27 2020-01-02 MTU Aero Engines AG Rotor for a turbomachine and turbomachine with such a rotor
FR3120649A1 (en) * 2021-03-12 2022-09-16 Safran Aircraft Engines TURBINE STATOR ASSEMBLY
FR3126014B1 (en) * 2021-08-05 2024-06-14 Safran Aircraft Engines Distributor for turbomachine

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5215435A (en) * 1991-10-28 1993-06-01 General Electric Company Angled cooling air bypass slots in honeycomb seals
EP1614862A1 (en) * 2004-07-07 2006-01-11 Hitachi, Ltd. Gas turbine and gas turbine cooling and sealing method
FR2928963A1 (en) * 2008-03-19 2009-09-25 Snecma Sa TURBINE DISPENSER FOR A TURBOMACHINE.
US20110052380A1 (en) * 2008-03-19 2011-03-03 Snecma Sectored distributor for turbomachine
DE102010055435A1 (en) * 2010-12-21 2012-06-21 Rolls-Royce Deutschland Ltd & Co Kg Inner shroud for holding blade roots of e.g. stator blade of high-pressure compressor in aircraft gas turbine, has U-profile provided with flat middle portion, where value defining geometry of blade roots is smaller than reference value

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3603599A (en) * 1970-05-06 1971-09-07 Gen Motors Corp Cooled seal
JP2004202544A (en) * 2002-12-25 2004-07-22 Daido Steel Co Ltd Method for producing polygonal annular member having deformed cross section
DE102004034312A1 (en) * 2004-07-15 2006-02-02 Mtu Aero Engines Gmbh Sealing arrangement and method for producing a sealing body for a sealing arrangement
US9080449B2 (en) * 2011-08-16 2015-07-14 United Technologies Corporation Gas turbine engine seal assembly having flow-through tube

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5215435A (en) * 1991-10-28 1993-06-01 General Electric Company Angled cooling air bypass slots in honeycomb seals
EP1614862A1 (en) * 2004-07-07 2006-01-11 Hitachi, Ltd. Gas turbine and gas turbine cooling and sealing method
FR2928963A1 (en) * 2008-03-19 2009-09-25 Snecma Sa TURBINE DISPENSER FOR A TURBOMACHINE.
US20110052380A1 (en) * 2008-03-19 2011-03-03 Snecma Sectored distributor for turbomachine
DE102010055435A1 (en) * 2010-12-21 2012-06-21 Rolls-Royce Deutschland Ltd & Co Kg Inner shroud for holding blade roots of e.g. stator blade of high-pressure compressor in aircraft gas turbine, has U-profile provided with flat middle portion, where value defining geometry of blade roots is smaller than reference value

Cited By (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP2960555A1 (en) * 2014-06-25 2015-12-30 MTU Aero Engines GmbH Brush seal system for sealing a gap between components of a turbomachine which can be moved relative to each other
US10094230B2 (en) 2014-06-25 2018-10-09 MTU Aero Engines AG Brush seal system for sealing a clearance between components of a turbo engine that are movable in relation to one another
FR3039589A1 (en) * 2015-07-28 2017-02-03 Snecma STAGE OF TURBOMACHINE, ESPECIALLY LOW-PRESSURE TURBINE
EP3208426A1 (en) 2016-02-18 2017-08-23 MTU Aero Engines GmbH Guide blade formation for a flow machine
DE102016202519A1 (en) 2016-02-18 2017-08-24 MTU Aero Engines AG Guide vane segment for a turbomachine
US10895162B2 (en) 2016-02-18 2021-01-19 MTU Aero Engines AG Guide vane segment for a turbomachine
US10808561B2 (en) 2017-05-29 2020-10-20 MTU Aero Engines AG Seal arrangement for a turbomachine, method for manufacturing a seal arrangement and turbomachine
EP3409897A1 (en) * 2017-05-29 2018-12-05 MTU Aero Engines GmbH Seal assembly for a turbomachine, method for producing a seal assembly and turbomachine
EP3483399A1 (en) * 2017-11-09 2019-05-15 MTU Aero Engines GmbH Seal assembly for a turbomachine, method for producing a seal assembly and turbomachine
US10865651B2 (en) 2017-11-09 2020-12-15 MTU Aero Engines AG Sealing assembly for a fluid kinetic machine, method for producing a sealing assembly as well as fluid kinetic machine
EP3517734A1 (en) * 2018-01-29 2019-07-31 MTU Aero Engines GmbH Sealing module for a turbomachine
US10844737B2 (en) 2018-01-29 2020-11-24 MTU Aero Engines AG Additively manufactured module for a turbomachine
IT201900013218A1 (en) * 2019-07-29 2021-01-29 Ge Avio Srl INTERNAL BAND FOR TURBINE ENGINE.
WO2021186135A1 (en) * 2020-03-19 2021-09-23 Safran Aircraft Engines Turbomachine rotary assembly comprising an annular clamping part
FR3108358A1 (en) * 2020-03-19 2021-09-24 Safran Aircraft Engines Rotary assembly for a turbomachine comprising an annular clamping part.
FR3113298A1 (en) * 2020-08-10 2022-02-11 Safran Aircraft Engines Abradable holder of a low pressure distributor comprising a single sheet
EP4345251A1 (en) * 2022-09-22 2024-04-03 MTU Aero Engines AG Module for a fluid flow machine

Also Published As

Publication number Publication date
EP2722486B1 (en) 2016-12-07
US20140105725A1 (en) 2014-04-17
US9856736B2 (en) 2018-01-02

Similar Documents

Publication Publication Date Title
EP2722486B1 (en) Seal holder for a stator assembly
DE102010041808B4 (en) Blade segment, turbomachinery and process for their preparation
DE102007002326A1 (en) Turbine blade and vane construction
EP2960555B1 (en) Brush seal system for sealing a gap between components of a turbomachine which can be moved relative to each other
EP3020922A1 (en) Blade assembly of a turbomachine with tuning mass
EP2851518B1 (en) Component system of a turbo engine
EP2873807A1 (en) Cover plate, rotor blade, wheel disc, bolt and gas turbine
EP3409899A1 (en) Sealing arrangement with a welded seal sheet, turbo-machine and production method
EP2356319A1 (en) Guide blade arrangement for an axial turbo-machine
DE102008008856A1 (en) Turbine housing and method of manufacturing a turbine housing
DE102016205995A1 (en) vane segment
EP1862640B1 (en) Turbine blade
DE19957718C1 (en) Bucket with optimized vibration behavior
DE102011055942B4 (en) Steam turbine singlet connection for nozzles of a limit stage with pinned or bolted inner ring
EP2696039B1 (en) Gas turbine stage
DE102016215807A1 (en) Inner ring for a vane ring of a turbomachine
DE102009013408A1 (en) Torque converter shovel
EP3483399A1 (en) Seal assembly for a turbomachine, method for producing a seal assembly and turbomachine
DE102009007664A1 (en) Sealing device on the blade shank of a rotor stage of an axial flow machine
DE102011084125A1 (en) Blade segment for turbomachine e.g. gas turbine for aircraft engine, has upper shroud which interconnects blades to each other, and lower shroud is divided into several portions which are firmly connected to the blades
EP2860352A1 (en) Rotor, corresponding manufacturing method and blade
EP3477048B1 (en) Arrangement for sealing a gap between turbomachine blades and for reducing vibrations of the turbomachine blades
EP2455587B1 (en) Rotor for a turbomachine, corrresponding turbomachine and method for manufacturing, repairing or upgrading
DE2609702C1 (en) Jet guide vane for a gas turbine engine
EP3999718B1 (en) Integrally bladed turbomachine rotor

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

17P Request for examination filed

Effective date: 20130725

AK Designated contracting states

Kind code of ref document: A1

Designated state(s): AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR

AX Request for extension of the european patent

Extension state: BA ME

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

Owner name: MTU AERO ENGINES GMBH

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

Owner name: MTU AERO ENGINES AG

17Q First examination report despatched

Effective date: 20160506

GRAP Despatch of communication of intention to grant a patent

Free format text: ORIGINAL CODE: EPIDOSNIGR1

INTG Intention to grant announced

Effective date: 20160915

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): AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR

REG Reference to a national code

Ref country code: GB

Ref legal event code: FG4D

Free format text: NOT ENGLISH

REG Reference to a national code

Ref country code: CH

Ref legal event code: EP

Ref country code: AT

Ref legal event code: REF

Ref document number: 851919

Country of ref document: AT

Kind code of ref document: T

Effective date: 20161215

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: DE

Ref legal event code: R096

Ref document number: 502012008963

Country of ref document: DE

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

Ref country code: LV

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: 20161207

REG Reference to a national code

Ref country code: LT

Ref legal event code: MG4D

REG Reference to a national code

Ref country code: NL

Ref legal event code: MP

Effective date: 20161207

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

Ref country code: LT

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: 20161207

Ref country code: NO

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: 20170307

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: 20170308

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: 20161207

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 FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20161207

Ref country code: RS

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: 20161207

Ref country code: HR

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: 20161207

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: 20161207

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 FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20161207

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

Ref country code: IS

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: 20170407

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: 20161207

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: 20161207

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: 20161207

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: 20161207

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

Ref country code: PL

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: 20161207

Ref country code: IT

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: 20161207

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: 20170307

Ref country code: SM

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: 20161207

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: 20170407

REG Reference to a national code

Ref country code: DE

Ref legal event code: R097

Ref document number: 502012008963

Country of ref document: DE

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

REG Reference to a national code

Ref country code: FR

Ref legal event code: PLFP

Year of fee payment: 6

26N No opposition filed

Effective date: 20170908

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

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: 20161207

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: 20161207

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

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: 20161207

REG Reference to a national code

Ref country code: CH

Ref legal event code: PL

REG Reference to a national code

Ref country code: IE

Ref legal event code: MM4A

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

Ref country code: LI

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

Effective date: 20171031

Ref country code: LU

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

Effective date: 20171017

Ref country code: CH

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

Effective date: 20171031

REG Reference to a national code

Ref country code: BE

Ref legal event code: MM

Effective date: 20171031

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: 20171031

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

Ref country code: MT

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: 20161207

REG Reference to a national code

Ref country code: FR

Ref legal event code: PLFP

Year of fee payment: 7

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: 20171017

REG Reference to a national code

Ref country code: AT

Ref legal event code: MM01

Ref document number: 851919

Country of ref document: AT

Kind code of ref document: T

Effective date: 20171017

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: 20171017

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: 20121017

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 NON-PAYMENT OF DUE FEES

Effective date: 20161207

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

Ref country code: MK

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: 20161207

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: 20161207

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

Ref country code: AL

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: 20161207

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

Ref country code: GB

Payment date: 20201022

Year of fee payment: 9

Ref country code: FR

Payment date: 20201020

Year of fee payment: 9

Ref country code: DE

Payment date: 20201022

Year of fee payment: 9

REG Reference to a national code

Ref country code: DE

Ref legal event code: R119

Ref document number: 502012008963

Country of ref document: DE

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

Effective date: 20211017

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

Ref country code: GB

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

Effective date: 20211017

Ref country code: DE

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

Effective date: 20220503

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: 20211031