EP2565399A1 - Dispositif de montage ou de démontage d'un composant sur ou dans une turbine à gaz stationnaire et procédé de montage et de démontage d'un composant d'une turbine à gaz stationnaire - Google Patents

Dispositif de montage ou de démontage d'un composant sur ou dans une turbine à gaz stationnaire et procédé de montage et de démontage d'un composant d'une turbine à gaz stationnaire Download PDF

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Publication number
EP2565399A1
EP2565399A1 EP11007152A EP11007152A EP2565399A1 EP 2565399 A1 EP2565399 A1 EP 2565399A1 EP 11007152 A EP11007152 A EP 11007152A EP 11007152 A EP11007152 A EP 11007152A EP 2565399 A1 EP2565399 A1 EP 2565399A1
Authority
EP
European Patent Office
Prior art keywords
gas turbine
component
rail
rails
rail system
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Withdrawn
Application number
EP11007152A
Other languages
German (de)
English (en)
Inventor
Andreas Griese
Dirk MÜLLER
Simon Purschke
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 EP11007152A priority Critical patent/EP2565399A1/fr
Priority to KR1020147005032A priority patent/KR101942126B1/ko
Priority to MX2014002283A priority patent/MX348001B/es
Priority to JP2014527645A priority patent/JP5908083B2/ja
Priority to CN201280042798.5A priority patent/CN103764955B/zh
Priority to RU2014112690/02A priority patent/RU2575109C2/ru
Priority to US14/241,473 priority patent/US9404390B2/en
Priority to CA2847324A priority patent/CA2847324A1/fr
Priority to PCT/EP2012/066772 priority patent/WO2013030230A2/fr
Publication of EP2565399A1 publication Critical patent/EP2565399A1/fr
Withdrawn legal-status Critical Current

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Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/28—Supporting or mounting arrangements, e.g. for turbine casing
    • F01D25/285—Temporary support structures, e.g. for testing, assembling, installing, repairing; Assembly methods using such 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
    • F23R3/42—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
    • F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R2900/00—Special features of, or arrangements for continuous combustion chambers; Combustion processes therefor
    • F23R2900/00017—Assembling combustion chamber liners or subparts
    • Y—GENERAL 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
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00—Metal working
    • Y10T29/49—Method of mechanical manufacture
    • Y10T29/49316—Impeller making
    • Y—GENERAL 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
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00—Metal working
    • Y10T29/49—Method of mechanical manufacture
    • Y10T29/49316—Impeller making
    • Y10T29/49318—Repairing or disassembling
    • Y—GENERAL 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
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00—Metal working
    • Y10T29/49—Method of mechanical manufacture
    • Y10T29/49316—Impeller making
    • Y10T29/4932—Turbomachine making
    • Y—GENERAL 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
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00—Metal working
    • Y10T29/49—Method of mechanical manufacture
    • Y10T29/49826—Assembling or joining
    • Y10T29/49895—Associating parts by use of aligning means [e.g., use of a drift pin or a "fixture"]
    • Y—GENERAL 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
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00—Metal working
    • Y10T29/53—Means to assemble or disassemble
    • Y10T29/53978—Means to assemble or disassemble including means to relatively position plural work parts

Definitions

  • the invention relates to a device for mounting or dismounting a component on or in a stationary gas turbine and a method for this purpose.
  • Stationary gas turbines have long been known from the extensive state of the art.
  • One type of known stationary gas turbine is equipped with evenly distributed over the circumference combustion chambers, which are each referred to as a tube combustion chamber or as Can combustion chamber.
  • Each of these tube combustion chambers always includes a burner sitting in the gas turbine housing burner with a burner tube to which a transition pipe - in English also referred to as "transition" - connects.
  • the transition tubes conduct the resulting in the individual cylindrical burner tubes hot gas in an annular channel.
  • the transition tubes on the burner side have a circular cross-section, which merges on the output side into a sector-shaped cross-section.
  • the sector-shaped cross sections of all transition tubes are usually in the circumferential direction to each other, so that the hot gas generated in the individual tube combustion chambers can be converted loss in the annular channel of the gas turbine.
  • the turbine blades arranged in the turbine are arranged in stages.
  • a firing exchange system in which a rail is attached to a peripheral flange of two axially adjacent parts of the gas turbine housing, along which a lavishly designed carriage for transporting the burner to be mounted is movable.
  • the carriage is equipped with a joint and with a translationally displaceable burner carrier in order to be able to transport individual burners of the gas turbine to their destination.
  • a disadvantage of the known device is that it is very spacious and requires a relatively large space for movement around the gas turbine housing around. This free movement space is so large that its outermost radius is far greater than the outermost radius of the gas turbine housing. However, this space is not always available.
  • Another disadvantage of the known device is that due to the relatively long and free-ended linkage on the slide and the considerable weights of the components to be replaced, such as burners and transition tubes they are insufficiently accurately against the component opening through which they are to be introduced into the gas turbine can be positioned ,
  • the object of the invention is therefore to provide a device for mounting or dismounting a component on or in a stationary gas turbine, which on the one hand is comparatively small in size and on the other hand allows a precise positioning of the relevant component on or in the stationary gas turbine.
  • Another object of the invention is to provide a method for assembling and disassembling a component of a stationary gas turbine, which is comparatively quickly feasible without a particularly large demand for mounting space.
  • the object directed to the device is achieved with such according to the device features according to claim 1.
  • the object directed to the method is achieved with one according to claim 9.
  • Advantageous embodiments of the device and the method are specified in the respective subclaims. Unless otherwise stated, the features of different subclaims can be combined with one another in any desired manner.
  • the device for mounting or dismounting a component on or in a stationary gas turbine comprises a rail system with a frame carriage movable along it, on which an insertion unit with a carrier unit for the component which is displaceable along a displacement axis is arranged, wherein the sliding system is two-lane - that includes two rails - and the displacement axis extends transversely to the plane spanned by the rails between the two rails.
  • the frame carriage, the insertion unit and the carrier unit - with or without it temporarily attached component hereinafter also referred to as a movable unit.
  • the invention is thus based on the finding that the attachment of the rail system known from the prior art to the housing flange of the gas turbine is unfavorable.
  • An insertion opening near attachment of the rail system is structurally much cheaper.
  • the invention proposes to use a two-track rail system.
  • the rails and the components sliding or rolling thereon can be made smaller in size than in a design with only one rail.
  • the two rails on both sides of the insertion opening for the relevant component - ie in relation to the machine axis of the gas turbine further inside and further outside - can be attached to the housing of the gas turbine.
  • the component to be assembled or disassembled can then be mounted between the two rails by the support unit is displaceable along a displacement axis, which displacement axis is transverse to a plane which is spanned between the two rails. Consequently, the rails are so far apart that when the device is attached to the gas turbine, the insertion opening is completely free.
  • the relevant component can thus be easily moved along the displacement axis between the two rails into the gas turbine or out of the gas turbine.
  • Another advantage is that with respect to the central axis of the gas turbine no such large diameter for the movement space of the mounting device is required as in the prior art, since even the outer rail of the rail system is located within the outermost diameter of the housing of the gas turbine.
  • the rail system is designed either as an endless circular path or as a circular arc.
  • the rail system is designed as an endless circular path, so that with the help of this endless circular path of the frame carriage and arranged thereon insertion unit and carrier unit can approach each arranged on the gas turbine insertion opening.
  • this endless circular path of the frame carriage and arranged thereon insertion unit and carrier unit can approach each arranged on the gas turbine insertion opening.
  • the rail system comprises for each rail a plurality of rail holders for fastening the rail system to the gas turbine.
  • the rail holder can be designed modular in order to attach it to the insertion of the burner can.
  • the rail system can also be attached next to the insertion, for example, by bolts.
  • the frame carriage per rail of the rail system comprises at least two on the respective rail synchronously moved roller carriage, which preferably each comprise at least two rollers.
  • a secure attachment of the roller carriage on the two-track rail system is possible without further aids must prevent derailing of the movable along the circumference of the gas turbine frame truck.
  • this allows the weight forces of the movable unit and the component to be mounted on four corners of the frame carriage - more precisely on the eight roles - much more widely distributed than in the prior art in the rail system and derive the gas turbine housing. This avoids point loading, which would require larger components for the device.
  • the rollers are unrolled on those sides of the rails, which respectively face the other rails.
  • the rollers each press with their rolling surface against the inside of the respective rail, so that in principle the two rails are slightly pressed apart by the rollers.
  • the rollers are preferably designed as deflection rollers, so that in principle the rolling surface is bounded on both sides by a flange. This is at the same time given a form fit between the respective rail and the respective roles, so that a derailment of the frame carriage is reliably prevented by the rail system for each circumferential position of the frame carriage on the rail system.
  • the insertion unit comprises at least two rails supporting rails, along which the support unit is displaceable. This ensures a guided movement of the component when it is introduced into the gas turbine or when it is removed from the gas turbine. This prevents unwanted, accidental contact of component and housing, which protects the two elements from damage.
  • FIG. 1 a part of the housing 10 of a stationary gas turbine is shown in a perspective view.
  • the housing part comprises a lower half 12 and an upper half 14, which abut one another in a flange-like manner in a dividing plane 16 and whose flanges are screwed together.
  • Each half has a coaxial wall section 17 and a wall section 21 set up steeply for this purpose.
  • 14 openings 18 are provided, all of which lie on an imaginary circle, which is concentric with the machine axis 19.
  • the openings 18 are burner or insertion openings.
  • a burner 20 is inserted in one of the openings 18, whereby the opening 18 is closed.
  • the components may be known from the prior art burner tubes or transitional tubes.
  • the burner tube or the transition tube and at the same time a space-saving Design, the use of a device 22 (FIG. FIG. 2 ) provided for mounting and dismounting of these gas turbine components.
  • a device 22 FIG. FIG. 2
  • the following embodiment describes only the installation of a burner of the gas turbine, this is not limiting.
  • the device 22 is also suitable for removing a burner.
  • the burner and transition tubes using the device 22 can be mounted or removed.
  • FIG. 2 are not shown for reasons of clarity for the invention not further relevant parts of the housing and the gas turbine.
  • the openings 18 are located on the wall portion 21 of the gas turbine housing 10, which is comparatively only slightly angled with respect to the radial direction of the machine axis 19.
  • the device 22 comprises a rail system 23 with two rails, an outer rail 25 and an inner rail 26.
  • the terms “inside” and “outside” refer to the machine axis 19 of the gas turbine.
  • Each rail 25, 26 is fastened to the wall section 21 via a plurality of rail holders 28.
  • the inner rail 26 may additionally or alternatively also be fastened to the coaxial wall section 17.
  • the device 22 further comprises a unit 35 which can be moved along the rails 25, 26.
  • This unit 35 has a frame carriage 30, an insertion unit 36 fixed to the frame carriage 30 and having a carrier unit 40 displaceable longitudinally thereon.
  • On the support unit 40 is the component to be mounted - according to FIG. 2 a burner 50 - bolted to the tube combustion chambers of the gas turbine. In one of the openings 18, a further burner 50 is already attached.
  • FIG. 3 shows in contrast to FIG. 2 an alternative device 22 which extends substantially from the device 22 FIG. 2 differs in that the rail system 23 only over a circular arc of the circumference of the gas turbine housing 10 stretches and not - as in FIG. 2 - Is designed as an endless circular path.
  • a roller carriage 32 is provided with two rollers at each corner 27 of the frame carriage 30.
  • the rollers 34 are in the form of pulleys, so formed with a double-sided flange, so that the rollers 34 can not slip off the rails 25, 26 laterally.
  • the frame carriage 30 and thus also the insertion unit 36 together with the carrier unit 40 are displaceable along the rails 25, 26 in the circumferential direction of the gas turbine housing 10, which is represented by the double arrow 52.
  • the carrier unit 40 is displaceable along a rail system 23, which is illustrated by means of the double arrow 54.
  • the travel path of the frame carriage 30 and the displacement axis of the carrier unit 40 are transverse to one another.
  • devices 22 is a comparatively simple and accurate fitting or disassembly of a component, such as a burner 50 on or in the stationary gas turbine possible.
  • a component such as a burner 50 on or in the stationary gas turbine.
  • the rail system 23 with the rails 25, 26 is first to be arranged on the housing 10 of the gas turbine.
  • the frame carriage 30 is inserted with the insertion unit 36 arranged thereon and with a support unit 40 displaceable thereon along a displacement axis into the rail system 23.
  • a cable is fastened to a hook 56 of the displaceable unit 35, to which the unit 35 then hangs.
  • the unit 35 can be moved to any position without fitters have to maintain the weight of the unit 35 and the burner.
  • the torch 50 may be temporarily attached to the carrier unit 40 for the last portion of the transport path.
  • the unit 35 then secured against further movement, which on the one hand relieves the cable and on the other hand allows a particularly accurate alignment of the burner 50 relative to the opening 18.
  • the carrier unit 40 is displaced along its displacement axis, so that meanwhile the burner 50 dips through the opening 18 into the interior of the gas turbine without a component-damaging contact.
  • a flange 51 arranged on the burner 51 can be screwed to a flange 18 located around the opening 18.
  • the burner 50 is released from the carrier unit 40, after which the assembly of the respective burner 50 is completed.
  • the movable unit 35 moves back to a loading position, in which the next component to be mounted on the support unit 40 can be attached.
  • the components to be assembled can be mounted in an easily accessible place in a "loading position" on the movable unit 35 and can be transported by a kind of turret system in a less accessible mounting position.
  • the arranged in the lower half of the housing openings 18 are classified as relatively difficult to access, as they can be equipped with the aid of a loading crane with burners 50 without the provision of such a device 22 insufficient.
  • Another advantage of the device 22 is the fact that assembly steps can be carried out partly in parallel. For example, it is conceivable that a burner 50 positioned with the aid of the frame carriage 30 is attached to its opening 18 only in the alternative, and then the attachment to the carrier unit 40 is released.
  • the frame carriage 30 together with the carrier unit 40 is ready to be fitted with the next burner 50 to be mounted, during which the first auxiliary burner 50 is then fastened to the housing 10 during the loading of the frame carriage 30 with the next burner 50 at the same time.
  • the rail holder 28 comprises an attachment 29 and a plate 31 and a receptacle 33.
  • the use of the attachment 29 is particularly advantageous if the rail holder 28 is to be mounted on a gas turbine, are still mounted on the burner burner 18 opening. In this case, the use of an attachment 29 is not required, which leads to the fact that irrespective of whether a burner 50 is fastened to an opening 18 or not, the rail 25 or 26 always has the same distance from the wall section 21.
  • each opening 18 can be equipped with burners 50 and not blocked by any rail brackets 28.
  • FIGS. 5, 6 show in cross-section two different configurations of roller carriage 32, each with two rollers 34 arranged thereon. They are mounted on an axis storage with two roller bearings 60 on the axes 62, wherein the axial securing in one direction by a shaft shoulder and in the other direction a nut is guaranteed. Both axes 62 are firmly clamped in the axle holder 64 by a nut 65. In order to ensure that always both rollers 34 rest against the rail, the axle holder 64 is rotatably mounted. For this purpose, a bearing with a radial sliding bearing 66 and two matched thrust bearings is provided, which is axially fixed by a groove nut 67 which is pressed against a lug.
  • the storage of the axle holder 64 on the longitudinal struts inside and outside are solved differently.
  • On the inside of the strut is an eccentric 69 ( FIG. 5 ), which allows an adjustment of the roller carriage 32 in the direction of the rail.
  • the alignment of the movable unit 35 with respect to the openings 18 can be adjustable with the eccentric.
  • For the upper axle of the Excenters 69 is inserted with a clearance in the bearing seat inside. Through an inserted hexagon socket on the front face of the upper axle 68 of the eccentric 69 and the external thread of this can be pressed with a defined force against the inner rail and fixed by bracing the components.
  • the invention thus relates to a device 22 for mounting or dismounting a component, preferably a burner 50 or a transition tube of a gas turbine on or in a stationary gas turbine, comprising a rail system 23 with a frame carriage 30 movable along it, on which an insertion unit 36 is arranged with a displaceable along a displacement axis carrier unit 40 for the component.
  • a rail system 23 is formed two lanes and the displacement axis transverse to the plane between the rails 25, 26 plane between the two rails 25, 26 extends therethrough.

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Gas Burners (AREA)
  • Quick-Acting Or Multi-Walled Pipe Joints (AREA)
  • Incineration Of Waste (AREA)
  • Automatic Assembly (AREA)
EP11007152A 2011-09-02 2011-09-02 Dispositif de montage ou de démontage d'un composant sur ou dans une turbine à gaz stationnaire et procédé de montage et de démontage d'un composant d'une turbine à gaz stationnaire Withdrawn EP2565399A1 (fr)

Priority Applications (9)

Application Number Priority Date Filing Date Title
EP11007152A EP2565399A1 (fr) 2011-09-02 2011-09-02 Dispositif de montage ou de démontage d'un composant sur ou dans une turbine à gaz stationnaire et procédé de montage et de démontage d'un composant d'une turbine à gaz stationnaire
KR1020147005032A KR101942126B1 (ko) 2011-09-02 2012-08-29 고정 가스 터빈에 또는 그 안에 부품을 설치 및 제거하기 위한 장치 및 고정 가스 터빈의 부품을 설치 및 제거하기 위한 방법
MX2014002283A MX348001B (es) 2011-09-02 2012-08-29 Dispositivo para el montaje o desmontaje de un componente encima de o en el interior de una turbina de gas estacionaria y procedimiento para el montaje o desmontaje de un componente de una turbina de gas estacionaria.
JP2014527645A JP5908083B2 (ja) 2011-09-02 2012-08-29 定置型ガスタービンの外部または内部で部品を組立ておよび取外す装置、ならびに定置型ガスタービンの部品を組立ておよび取外す方法
CN201280042798.5A CN103764955B (zh) 2011-09-02 2012-08-29 在固定式燃气轮机上或内部安装或拆卸构件的设备相关方法
RU2014112690/02A RU2575109C2 (ru) 2011-09-02 2012-08-29 Устройство для монтажа и демонтажа конструктивного элемента стационарной газовой турбины, стационарная газовая турбина и способ монтажа и демонтажа конструктивного элемента стационарной газовой турбины
US14/241,473 US9404390B2 (en) 2011-09-02 2012-08-29 Device for installing and removing a component on or in a stationary gas turbine and method for installing and removing a component of a stationary gas turbine
CA2847324A CA2847324A1 (fr) 2011-09-02 2012-08-29 Dispositif pour le montage ou le demontage d'un element sur ou dans une turbine a gaz stationnaire et procede de montage et demontage d'un element d'une turbine a gaz stationnaire
PCT/EP2012/066772 WO2013030230A2 (fr) 2011-09-02 2012-08-29 Dispositif pour le montage ou le démontage d'un élément sur ou dans une turbine à gaz stationnaire et procédé de montage et démontage d'un élément d'une turbine à gaz stationnaire

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
EP11007152A EP2565399A1 (fr) 2011-09-02 2011-09-02 Dispositif de montage ou de démontage d'un composant sur ou dans une turbine à gaz stationnaire et procédé de montage et de démontage d'un composant d'une turbine à gaz stationnaire

Publications (1)

Publication Number Publication Date
EP2565399A1 true EP2565399A1 (fr) 2013-03-06

Family

ID=46800181

Family Applications (1)

Application Number Title Priority Date Filing Date
EP11007152A Withdrawn EP2565399A1 (fr) 2011-09-02 2011-09-02 Dispositif de montage ou de démontage d'un composant sur ou dans une turbine à gaz stationnaire et procédé de montage et de démontage d'un composant d'une turbine à gaz stationnaire

Country Status (8)

Country Link
US (1) US9404390B2 (fr)
EP (1) EP2565399A1 (fr)
JP (1) JP5908083B2 (fr)
KR (1) KR101942126B1 (fr)
CN (1) CN103764955B (fr)
CA (1) CA2847324A1 (fr)
MX (1) MX348001B (fr)
WO (1) WO2013030230A2 (fr)

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JP2015025450A (ja) * 2013-07-26 2015-02-05 斗山重工業株式会社 タービン用燃焼器組立装置、及びこれを用いた燃焼器組立方法
EP2949886A1 (fr) * 2014-05-26 2015-12-02 Alstom Technology Ltd Procédé et dispositif pour le montage et le démontage d'un composant de turbine
WO2017116243A1 (fr) * 2015-12-31 2017-07-06 General Electric Company Rails de guidage d'ensemble de chambre de combustion et turbomachines équipées desdits rails

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EP2990616A1 (fr) 2014-08-26 2016-03-02 Siemens Aktiengesellschaft Dispositif de montage et de démontage d'un composant sur une turbine à gaz
EP2993314B1 (fr) * 2014-09-05 2017-11-08 Ansaldo Energia Switzerland AG Dispositif et procédé pour le montage ou le démontage, le remplacement et l'entretien d'une chambre de combustion CAN
EP3067627B1 (fr) * 2015-03-12 2019-09-18 Ansaldo Energia Switzerland AG Dispositif de montage et de démontage pour le revêtement d'une turbine à gaz et procédé associé
US10088167B2 (en) 2015-06-15 2018-10-02 General Electric Company Combustion flow sleeve lifting tool
JP6499947B2 (ja) * 2015-09-07 2019-04-10 東芝プラントシステム株式会社 ガスタービン燃焼器分解組立輸送装置
US10208627B2 (en) * 2015-12-10 2019-02-19 General Electric Company Combustor assembly lift systems
US20170167298A1 (en) * 2015-12-10 2017-06-15 General Electric Company Combustor assembly lift systems and methods for using the same to install and remove combustor assemblies
PL3414491T3 (pl) * 2015-12-31 2023-05-22 General Electric Company Układy podnoszenia zespołu komory spalania i sposoby ich stosowania do montażu i usuwania zespołów komory spalania
KR102204455B1 (ko) * 2019-09-27 2021-01-18 두산중공업 주식회사 서포트를 포함하는 트랜지션피스 조립 지그 및 이를 이용하여 조립된 연소기
KR102138722B1 (ko) * 2019-10-21 2020-07-28 두산중공업 주식회사 트랜지션피스 케리어를 포함하는 트랜지션피스 조립 지그
US11873727B2 (en) 2021-04-15 2024-01-16 General Electric Company System and method for hoisting gas engine assemblies
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CN103764955B (zh) 2016-04-13
US20140215800A1 (en) 2014-08-07
US9404390B2 (en) 2016-08-02
KR101942126B1 (ko) 2019-01-24
WO2013030230A3 (fr) 2013-04-25
KR20140053237A (ko) 2014-05-07
JP2014525542A (ja) 2014-09-29
CN103764955A (zh) 2014-04-30
JP5908083B2 (ja) 2016-04-26
MX2014002283A (es) 2014-03-27
MX348001B (es) 2017-05-03
RU2014112690A (ru) 2015-10-10
WO2013030230A2 (fr) 2013-03-07

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