EP2898269A2 - Élément de retenue destiné à maintenir une tuile de protection thermique et procédé de refroidissement de la structure support d'un bouclier thermique - Google Patents

Élément de retenue destiné à maintenir une tuile de protection thermique et procédé de refroidissement de la structure support d'un bouclier thermique

Info

Publication number
EP2898269A2
EP2898269A2 EP13762847.5A EP13762847A EP2898269A2 EP 2898269 A2 EP2898269 A2 EP 2898269A2 EP 13762847 A EP13762847 A EP 13762847A EP 2898269 A2 EP2898269 A2 EP 2898269A2
Authority
EP
European Patent Office
Prior art keywords
cooling air
heat shield
support structure
air passage
cooling
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
EP13762847.5A
Other languages
German (de)
English (en)
Other versions
EP2898269B1 (fr
Inventor
Daniel Vogtmann
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 EP13762847.5A priority Critical patent/EP2898269B1/fr
Publication of EP2898269A2 publication Critical patent/EP2898269A2/fr
Application granted granted Critical
Publication of EP2898269B1 publication Critical patent/EP2898269B1/fr
Not-in-force legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/005—Combined with pressure or heat exchangers
    • 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
    • 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
    • F23M5/08—Cooling thereof; Tube walls
    • F23M5/085—Cooling thereof; Tube walls using air or other gas as the cooling medium
    • 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
    • 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
    • F23R3/42—Continuous combustion chambers using liquid or gaseous fuel characterised by the arrangement or form of the flame tubes or combustion chambers
    • F23R3/60—Support structures; Attaching or mounting means
    • 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
    • F23M5/08—Cooling thereof; Tube walls

Definitions

  • the invention relates to a holding element for holding a heat shield brick held on a support structure and to a method for cooling the support structure of a heat shield.
  • the invention also relates to such a heat shield and a combustion chamber lined by the heat shield and a gas turbine.
  • heat shields are used, which must withstand hot gases of 1000 to 1600 degrees Celsius.
  • gas turbines such as those used in power-generating power plants and in aircraft engines, have correspondingly large surfaces to be shielded by heat shields in the interior of the combustion chambers.
  • the heat shield must be composed of a plurality of individual, generally ceramic heat shield bricks, spaced apart from each other with a sufficient gap to a support structure. This gap offers the heat shield elements sufficient space for the thermal expansion.
  • cooling air is introduced as a countermeasure by the gaps in the direction of the combustion chamber
  • a generic heat shield thus comprises a support structure and a number of heat shields, which are releasably secured to the support structure by means of holding elements, each heat shield brick having a support structure facing cold side and the cold side opposite, acted upon by a hot medium hot side.
  • at least one cooling air passage is provided in the support structure.
  • the generic holding element has a fastening portion attachable to the support structure and a holding portion with a holding head, which is designed to engage in an existing on the heat shield stone engaging device.
  • EP 1 701 095 A1 discloses an initially mentioned heat shield of a combustion chamber of a gas turbine having a support structure and a number of heat shield bricks arranged detachably on the support structure.
  • the heat shield bricks are arranged across the surface, leaving expansion gaps on the support structure, wherein each heat shield brick has a cold-side facing the support structure and a hot side which is opposite to the cold side and can be charged with a hot medium.
  • the heat shield bricks are resiliently fastened to the support structure with two metallic holding elements each.
  • each retaining element comprises a holding portion with a gripping portion and a fixing portion.
  • each heat shield brick retaining grooves are introduced on two opposite circumferential sides, so that for holding the heat shield brick, the gripping portions of the holding elements opposite can engage in the retaining grooves.
  • the holding elements which are fastened on the heat shield block in opposite directions are guided with their attachment section in a fastening groove extending below the heat shield block in the support structure.
  • the gripping sections of the metallic stone holders are cooled.
  • openings are made in the stone holder in the region of the holding section and in the retaining bolts of the heat shield bricks, which are aligned with a cooling air hole arranged in the support structure, so that cooling air from the cooling air bore flows in a direct line against a cold side of the gripping section.
  • Another object of the invention is to provide a combustion chamber and a gas turbine, with which a scaling of the support structure of a heat shield covered by the combustion chamber can be particularly effectively avoided.
  • the object is achieved in a holding element of the type mentioned above in that at least one cooling air passage is arranged in the attachment portion.
  • the cooling air passage comprises an inlet opening and at least one outlet opening arranged in a side surface and / or on the top side of the fastening section.
  • Cooling air entering from the inlet opening exits from the at least one outlet opening, whereby an outflow direction can be imposed on the cooling air by means of the cooling air passage, which comprises a velocity component parallel to the cold side and avoids impact cooling of the heat shield brick held by the holding section.
  • the attachment section can be arranged on the support structure such that the cooling air passage corresponds to at least one cooling air passage arranged in the support structure.
  • the configuration of the retaining element according to the invention allows cooling air in the region of the fastening section to be removed. to feed below a heat shield of a heat shield. Because of this cooling air flowing in substantially centrally under the heat shield brick, the support structure can be effectively cooled in the areas which serve to secure the heat shield stones.
  • the resilient retaining elements which are also referred to with stone holders, are mounted substantially centrally below the heat shield bricks. With the invention, this area is effectively cooled, with a direct flow of the heat shield bricks is prevented by means of the inventively designed stone holder. Damage to the heat shield stones is thus safely avoided.
  • the heat shield bricks are generally made of a ceramic material and are in operation on your hot side directly in contact with the hot gases in the combustion chamber.
  • the cooling air passage integrated in the attachment section can be fed by at least one cooling air channel in the support structure with suitable positioning of the stone support on the support structure. That the cooling air passage corresponds to the cooling air passage is to be understood such that the stone holder on the support structure in such a way
  • the inlet opening of the cooling air passage and the outlet opening of the cooling air passage can be aligned with each other, for example. There is thus no need for a physically fixed connection between the cooling air duct in the supporting structure and the cooling air passage in the brick holder.
  • the stone holder is only to be positioned at a suitable location on the support structure, whereby a simple installation or removal of the heat shield bricks is made possible for maintenance purposes.
  • the retaining elements may be guided in fastening grooves, wherein the cooling air channels arranged in the supporting structure are arranged in a groove bottom of the fastening Groove are arranged.
  • the stone holders can be pushed over the cooling air channels for maintenance purposes.
  • the cooling air passage can be arranged, for example, in the end region of the fastening section facing away from the holding section.
  • the flow direction of the cooling air when leaving an outlet opening of the cooling air passage can be directed by appropriate design of the cooling air passage on a region to be cooled of the support structure.
  • the direction of the total momentum of a cooling air flow emerging from an outlet opening of the cooling air passage is not directed to the heat shield.
  • the cooling air passage corresponds to a survey formed on the top of the mounting portion survey.
  • This embodiment of the invention makes it possible to arrange the at least one outlet opening of the cooling air passage laterally in the survey. It can also be considered advantageous that the attachment portion is thickened in the region of the survey.
  • the cooling air passage can be arranged, for example, within the fastening section.
  • a cooling air hole arranged in the fastening section which comprises at least one outlet opening arranged in a side surface of the elevation.
  • the cooling air bore may, for example, have a T-shaped profile.
  • the attachment portion is stepped in the region of the survey.
  • the cooling air passage may be formed as arranged below the step groove.
  • the groove may have two opposite side surfaces.
  • the groove could also include only one side surface.
  • the cooling air passage thus comprises two outlet openings, which are arranged in a side surface of the fastening portion.
  • the cooling air passage may include further outlet openings arranged in the elevation.
  • the elevation is step-shaped and comprises at least one side surface pointing in the direction of the holding section. According to this embodiment of the invention, at least one outlet opening of the cooling air passage is arranged in this side surface.
  • the flow direction of the cooling air emerging from the cooling air passage can be directed towards the side edges of the fastening section.
  • the fastening section comprises an elongate base plate, at one end face of which the holding section adjoins and at the other end face of which the base plate is offset in the direction of heat shield block a blocking plate is arranged.
  • a step-shaped elevation is formed in the top of the mounting portion by means of the blocking plate.
  • the cooling air passage is bounded at least by the underside of the blockade plate and the portion of the end face of the base plate running below the blocking plate.
  • a further object of the invention is to specify a heat shield mentioned at the beginning, with which a scaling of the support structure due to hot gas infeed can be avoided particularly effectively.
  • At least one retaining element encompassed by the heat shield is designed according to one of claims 1 to 7.
  • At least one cooling air channel arranged in the supporting structure corresponds to the retaining element, so that cooling air flowing from the cooling air channel at the heat structure blocks attached to the supporting structure at least partially enters the inlet opening of the cooling air passage.
  • a cooling air channel arranged in the support structure corresponds to the retaining element is to be understood such that the retaining element with its fastening section can be positioned on the support structure such that the cooling air flowing out of the cooling air channel at least partially enters the inlet opening of the cooling air passage.
  • the heat shield according to claim 8 is formed or formed at least one combustion chamber according to claim 9.
  • the heat shield used in the method comprises a number of heat shield bricks releasably attachable to the support structure.
  • the heat shield bricks are fastened by means of retaining elements on the support structure.
  • cooling air is conducted from the supporting structure along at least one upper side and / or side surface of the fastening section along a cooling air passage formed by the fastening section of a retaining element.
  • the cooling air is hereby impressed by means of the cooling air passage a flow direction, which avoids an impact cooling of the heat shield brick.
  • cooling air is impressed on a flow direction is to be understood such that the cooling air exits from one or more outlet openings of the cooling air passage.
  • Each of these cooling air flows at the exit on an optionally pointing in different directions total pulse.
  • an impingement cooling of the heat shield is avoided.
  • Such a total pulse thus always has a velocity component parallel to the cold side of the heat shield brick and is not directed directly to this.
  • Cooling air passage directed to at least a portion of the support structure to which a mounting portion of a holding element is attached.
  • the cooling air flowing along the cooling air passage is directed to a groove edge of a fastening groove.
  • FIG. 5 shows the holding element shown in Figure 4 arranged on a
  • FIG. 1 shows a schematic sectional view of a gas turbine 1 according to the prior art.
  • the gas turbine 1 has inside a rotatably mounted about a rotation axis 2 rotor 3 with a shaft 4, which is also referred to as a turbine runner.
  • a turbine runner which is also referred to as a turbine runner.
  • the rotor 3 successively follow an intake housing 6, a compressor 8, a combustion system 9 with a number of combustion chambers 10, each comprising a burner assembly 11 and a housing 12, a turbine 14 and an exhaust housing 15.
  • the housing 12 is for protection Hot gases lined with a heat shield (not shown).
  • the combustion system 9 communicates with an annular hot gas duct, for example.
  • a plurality of successively connected turbine stages form the turbine 14.
  • Each turbine stage is formed of blade rings.
  • a row formed of rotor blades 18 follows in the hot runner of a row formed by vanes 17.
  • the guide vanes 17 are fastened to an inner housing of a stator 19, whereas the rotor blades 18 of a row are attached to the rotor 3, for example by means of a turbine disk.
  • Coupled to the rotor 3 is, for example, a generator (not shown).
  • FIG. 2 shows a holding element 22 according to the invention in a perspective view according to a first exemplary embodiment.
  • the exemplary embodiment of the retaining element 22 comprises a rectangular, plate-shaped fastening section 23, at one end face of which a retaining section 24 connects at right angles.
  • the holding portion 24 comprises a holding head 25, which is designed to engage in an engagement device (not shown) on a heat shield brick.
  • the attachment portion 23 has a
  • the attachment portion 23 is widened in sections. This broadening the attachment portion 23 is also referred to as shoe 29.
  • the shoe 29 is adjoined by an elevation 30 arranged on the upper side 28 of the fastening section 23, so that the fastening section is thickened in the region of the elevation 30.
  • the term "side surface of the fastening portion 23" also includes the side surface 32.
  • the fastening portion 23 shown comprises a cooling air passage through the thickened region
  • the cooling air passage 34 thus corresponds to the elevation 30 formed on the upper side of the attachment section.
  • the cooling air passage 34 comprises an inlet opening 35 and two outlet openings 37 and 38.
  • the outlet openings 37, 38 are arranged in opposite side surfaces 32, 39 of the fastening section
  • the illustrated cooling air passage 34 is a cooling air bore which has an outlet opening 38 arranged in the side face 32 of the elevation 30 which points in the direction of the holding section 24.
  • a cooling air flow which enters the cooling air passage 34 through the inlet opening 35, is divided into two streams by the course of the T-shaped cooling air passage 34 and exits the cooling air passage 34 through the outlet openings 37 and 38.
  • an outflow direction is imparted to the cooling air, which runs parallel to the upper side of the fastening section 23. An impingement cooling of structures arranged above the holding element 22 (not shown) is thereby avoided.
  • FIG. 3 shows a section of a heat shield 42 according to the invention with a support structure 43 and a holding element 22 fastened to the support structure, which is designed in accordance with FIG.
  • the holding element 22 rests with its attachment section 23 on the support structure 43 and has a holding section 24 for holding a heat shield block (not shown). In this position is the upper side 28 of the attachment portion 23 faces a cold side of a heat shield block held by the holding portion 24 (not shown).
  • the cooling air passage 34 which is described in greater detail in FIG. 2, is shown in a longitudinal section.
  • the inlet opening 35 of the cooling air passage 34 is in alignment with a cooling air duct 45 arranged in the support structure.
  • the fastening section 23 is arranged on the support structure 43 such that the cooling air passage 34 corresponds to a cooling air duct 45 arranged in the support structure 43.
  • two flow paths 47 and 48 are shown by way of example, along which part of the cooling air flowing out of the cooling air duct 45 passes through the cooling air passage 34.
  • FIG. 4 shows an inventive holding element 54 according to a second exemplary embodiment.
  • the holding element 54 differs from the holding element shown in Figure 2 by another embodiment of the cooling air passage 55.
  • the mounting portion 23 here comprises a längli- che base plate 57, at one end face of the holding portion 24 connects and at the other end face 58 to the base plate 57 in the direction of heat shield brick (not shown) offset a blockade plate 60 is arranged.
  • a step-shaped elevation 30 is formed in the upper side of the fastening section 23, and the fastening section 23 is steppedly offset.
  • the cooling air passage 55 is delimited by the underside of the blockage plate 60 and the front side 58 of the base plate 57 running below the blocking plate.
  • the cooling air passage 55 thus comprises an outlet opening 62 which is arranged in the side surfaces of the fastening section 23 and revolves around the end of the fastening section 23.
  • the cooling air will have an outflow direction 59, 61, 63 as it passes through the cooling air passage 55. shaped, which runs parallel to the cold side of a held by the holding section heat shield stone.
  • FIG. 5 shows a section of a heat shield 64 according to the invention with a support structure 43 and a holding element 54 fastened to the support structure, which is designed in accordance with FIG.
  • the mounting portion 23 comprising the base plate 57 and the blocking plate 60 is fixed to the support structure 43 such that a cooling air passage 45 communicates with the cooling air passage 55. Cooling air, which flows along the exemplified flow paths 65 and 66 from the cooling air duct 45 into the inlet opening 68 of the cooling air passage 55 and out of the outlet opening 62, by means of the cooling air passage 55 a
  • the outflow direction in the illustrated embodiment is parallel to the cold side of a heat shield block held by the holding section 24 (not shown).
  • the illustrated embodiment is particularly well suited for cooling the groove edges of a mounting groove (not shown) in which the retaining element 54 is secured to the support structure.
  • a direction parallel to the cold side of the heat shield brick is synonymous with a direction parallel to the heat shield brick facing surface of the support structure. Surface irregularities of the support structure are not taken into account.

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Ceramic Engineering (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Cooling Or The Like Of Electrical Apparatus (AREA)

Abstract

L'invention concerne un élément de retenue (22, 54) destiné à maintenir une tuile de protection thermique sur une structure support (43) au moyen d'au moins une portion de fixation (23) pouvant être fixée à la structure support et d'au moins une portion de retenue (24) dotée d'une tête de retenue (25) qui est conformée pour s'engager dans un dispositif d'engagement présent au niveau de la tuile de protection thermique. Dans le cas d'une portion de fixation fixée à la structure support (43) d'une portion de retenue s'engageant au niveau de la tuile de protection thermique, la portion de fixation (23) comporte un côté supérieur (28) dirigé vers le côté froid de la tuile de protection thermique. L'élément de retenue permet d'éviter de façon particulièrement efficace un calaminage de la structure support dû à l'aspiration de gaz chaud. Pour cela, la portion de fixation (23) comporte au moins un passage d'air de refroidissement (34 , 55) qui possède un orifice d'entrée (35 , 68) et au moins un orifice de sortie (37, 38, 62) ménagé dans une face latérale (32) et/ou sur le côté supérieur (28) de la portion de fixation. Le passage d'air de refroidissement permet d'imposer à l'air de refroidissement qui entre par l'orifice d'entrée (35, 68) et qui sort par le ou les orifices de sortie une direction d'écoulement (50, 51, 59, 63, 61) respective qui présente une composante de vitesse parallèle au côté froid et qui évite un refroidissement par impact de la tuile de protection thermique maintenue par la portion de retenue. Ici, la portion de fixation peut être disposée sur la structure support de telle sorte que le passage d'air de refroidissement (34, 55) correspond à au moins un conduit d'air de refroidissement (45) disposé dans la structure support.
EP13762847.5A 2012-09-21 2013-09-17 Élément de retenue destiné à maintenir une tuile de protection thermique et procédé de refroidissement de la structure support d'un bouclier thermique Not-in-force EP2898269B1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
EP13762847.5A EP2898269B1 (fr) 2012-09-21 2013-09-17 Élément de retenue destiné à maintenir une tuile de protection thermique et procédé de refroidissement de la structure support d'un bouclier thermique

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
EP12185430.1A EP2711633A1 (fr) 2012-09-21 2012-09-21 Elément de retenue pour maintenir un bouclier de protection thermique et procédé de refroidissement de la structure porteuse d'un bouclier thermique
EP13762847.5A EP2898269B1 (fr) 2012-09-21 2013-09-17 Élément de retenue destiné à maintenir une tuile de protection thermique et procédé de refroidissement de la structure support d'un bouclier thermique
PCT/EP2013/069271 WO2014044673A2 (fr) 2012-09-21 2013-09-17 Élément de retenue destiné à maintenir une tuile de protection thermique et procédé de refroidissement de la structure support d'un bouclier thermique

Publications (2)

Publication Number Publication Date
EP2898269A2 true EP2898269A2 (fr) 2015-07-29
EP2898269B1 EP2898269B1 (fr) 2016-11-30

Family

ID=46963539

Family Applications (2)

Application Number Title Priority Date Filing Date
EP12185430.1A Withdrawn EP2711633A1 (fr) 2012-09-21 2012-09-21 Elément de retenue pour maintenir un bouclier de protection thermique et procédé de refroidissement de la structure porteuse d'un bouclier thermique
EP13762847.5A Not-in-force EP2898269B1 (fr) 2012-09-21 2013-09-17 Élément de retenue destiné à maintenir une tuile de protection thermique et procédé de refroidissement de la structure support d'un bouclier thermique

Family Applications Before (1)

Application Number Title Priority Date Filing Date
EP12185430.1A Withdrawn EP2711633A1 (fr) 2012-09-21 2012-09-21 Elément de retenue pour maintenir un bouclier de protection thermique et procédé de refroidissement de la structure porteuse d'un bouclier thermique

Country Status (6)

Country Link
US (1) US9657948B2 (fr)
EP (2) EP2711633A1 (fr)
KR (1) KR20150058230A (fr)
CN (1) CN104769362B (fr)
RU (1) RU2634992C2 (fr)
WO (1) WO2014044673A2 (fr)

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EP3033509B1 (fr) * 2013-08-15 2019-05-15 United Technologies Corporation Turbine à gas comprenant un panneau de protection et support à cet effet
DE102014206018A1 (de) * 2014-03-31 2015-10-01 Siemens Aktiengesellschaft Gasturbinenanlage
DE102015206033A1 (de) * 2015-04-02 2016-10-06 Siemens Aktiengesellschaft Steinhalter
CN109724110B (zh) * 2018-12-07 2020-06-30 西安航天动力研究所 一种具有装配补偿功能的助推器安装支撑结构
DE102019200593A1 (de) 2019-01-17 2020-07-23 Siemens Aktiengesellschaft Brennkammer

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Also Published As

Publication number Publication date
CN104769362B (zh) 2016-10-26
WO2014044673A2 (fr) 2014-03-27
EP2898269B1 (fr) 2016-11-30
US20150247640A1 (en) 2015-09-03
RU2015114793A (ru) 2016-11-10
KR20150058230A (ko) 2015-05-28
EP2711633A1 (fr) 2014-03-26
RU2634992C2 (ru) 2017-11-08
US9657948B2 (en) 2017-05-23
WO2014044673A3 (fr) 2014-05-22
CN104769362A (zh) 2015-07-08

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