WO2007048584A1 - Vorrichtung zur seitlichen montage und demontage eines kompressorbarrels - Google Patents
Vorrichtung zur seitlichen montage und demontage eines kompressorbarrels Download PDFInfo
- Publication number
- WO2007048584A1 WO2007048584A1 PCT/EP2006/010256 EP2006010256W WO2007048584A1 WO 2007048584 A1 WO2007048584 A1 WO 2007048584A1 EP 2006010256 W EP2006010256 W EP 2006010256W WO 2007048584 A1 WO2007048584 A1 WO 2007048584A1
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- housing
- turbocompressor
- compressor
- compressor barrel
- support arm
- Prior art date
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23P—METAL-WORKING NOT OTHERWISE PROVIDED FOR; COMBINED OPERATIONS; UNIVERSAL MACHINE TOOLS
- B23P19/00—Machines for simply fitting together or separating metal parts or objects, or metal and non-metal parts, whether or not involving some deformation; Tools or devices therefor so far as not provided for in other classes
- B23P19/02—Machines for simply fitting together or separating metal parts or objects, or metal and non-metal parts, whether or not involving some deformation; Tools or devices therefor so far as not provided for in other classes for connecting objects by press fit or for detaching same
- B23P19/022—Extracting or inserting relatively long parts
-
- 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
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D17/00—Radial-flow pumps, e.g. centrifugal pumps; Helico-centrifugal pumps
- F04D17/08—Centrifugal pumps
- F04D17/10—Centrifugal pumps for compressing or evacuating
- F04D17/12—Multi-stage pumps
- F04D17/122—Multi-stage pumps the individual rotor discs being, one for each stage, on a common shaft and axially spaced, e.g. conventional centrifugal multi- stage compressors
- F04D17/125—Multi-stage pumps the individual rotor discs being, one for each stage, on a common shaft and axially spaced, e.g. conventional centrifugal multi- stage compressors the casing being vertically split
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/60—Mounting; Assembling; Disassembling
- F04D29/62—Mounting; Assembling; Disassembling of radial or helico-centrifugal pumps
- F04D29/624—Mounting; Assembling; Disassembling of radial or helico-centrifugal pumps especially adapted for elastic fluid pumps
-
- 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
- Y10T29/53—Means to assemble or disassemble
-
- 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
- Y10T29/53961—Means to assemble or disassemble with work-holder for assembly
Definitions
- the invention relates to a device for laterally mounting and dismounting a compressor barrel of a turbocompressor in or out of a housing which is vertically divided, with the features of the preamble of claim 1.
- Turbochargers with a vertically split housing are used especially for higher gas pressures.
- the known from practice assembly devices for turbo compressors with horizontal ports use a leadership that - out of the drive side m the housing of the turbocompressor - the complete Kompressorbarrel m horizontal position in equilibrium, while on the non-drive side an axially sliding Abstutzung to the base frame or Basic frame done.
- the so-supported, complete, consisting of the inner part package with seals and lying in the bearings rotor compressor barrel is then installed axially or pulled out.
- Another mounting device uses instead of the described Abstutzung an existing crane to maintain the balance.
- a rope is placed around the compressor barrel and held by the crane. This requires a repeated implementation of the rope layer with the risk of a-Havarie.
- the invention has for its object to provide a device for mounting and dismounting a compressor barrels, in which the rotor is not supported on one side on the drive side by the already disassembled radial bearing and the rotor must be kept in equilibrium during assembly and disassembly.
- the compressor barrel can be kept in equilibrium from one side, even if the rotor is not or is no longer held on the other side in a radial bearing. This is particularly advantageous if, because of the horizontal position of the intake and discharge ports on the compressor housing no lateral guide rails for the mounting device can be mounted and on the drive side of the turbo compressor accessibility is limited by the constructive execution of forged to the compressor housing floor.
- FIG. 1 shows a longitudinal section through a turbocompressor with a
- Assembly / disassembly device and Fig. 2 is the side view of Fig. 1st
- the drawing shows a multi-stage turbocompressor only a vertically divided housing 1 in a state m the compressor barrel 2 is located immediately before installation or immediately after removal outside of the housing 1.
- the housing 1 of the turbocompressor has a vertical parting line
- the housing 1 rests with GeHousefußen 5 on a base frame 6.
- a suction nozzle 7 and a discharge nozzle 8 are connected to the housing 1.
- the two sockets 7, 8 can also be located in the lower two thirds of the housing periphery in a position between the 2 o'clock and the 10 o'clock. Be arranged clock position.
- the compressor barrel 2 is shown as if it had already been mounted for installation in the housing 1. It consists of a rotor 9 with a shaft and rotatably mounted on the shaft impellers 10. The rotor 9 is inserted into a stationary inner part package 11. This inner part package 11 consists of discs 12, which surround the wheels 10 of the rotor 9 and internal Um Replacementskanäle between the wheels 10 and to the nozzle 1, 8 limit. The individual discs 12 are divided horizontally and bolted together. To the first disc 12 of the compressor barrel 2, a lid 13 is screwed. The compressor barrel 2 further comprises a bearing block 14 with bearings for supporting one end of the rotor 9.
- a support arm 15 is releasably connected to the cover 13 of the Kor ⁇ pressorbarrels 2 laterally.
- the support arm 15 extends above the compressor barrier 2 m in its longitudinal direction and is dimensioned so long that it projects beyond the inner part packet 11.
- a roller 16 is attached at the free end of the support arm 15.
- the roller 16 can roll up to a position 16 'on a track 17, which is laid on the housing 1 of the turbo compressor above the suction nozzle 7 and the discharge nozzle 8.
- a stop 18 is provided on the housing 1, which prevents the roller 16 from rolling back over the edge of the housing 1.
- the compressor barrel 2 is supported on the housing 1 axially displaceable.
- support device 19 With the bearing block 14 of the compressor barrel 2, a support device 19 is releasably connected.
- support means 19 consists of two obliquely placed Siutzen 20, which are interconnected by a transverse web 21.
- a slide 22 Below each support 20 of the support device 19 is a slide 22, via which the support device is supported 19 m longitudinal direction of the compressor barrier 2 and to move.
- a lifting cable 23 is attached.
- the flexible traction means 24 of the hoist cable 23 is releasably connected on the one hand to the support arm 15 and on the other hand to the housing 1.
- Rope 26 of this cable 25 is guided around a pulley 27 to a not shown, lying outside the turbo compressor cable drive.
- the pulley 27 is m rotatably mounted m anchored on the base frame 6 pendulum support 28.
- the guidance of the cable 26 of the described cable 25 is chosen so that the portion of the cable 26 between the Support device 19 and the deflection point of the cable 26 to the pulley 27 in the longitudinal axis of the compressor drum 2 lie.
- Kor ⁇ pressorbarrel 2 is mounted on a prism bracket to ensure safe storage of Kompressorbarrels 2 during the cultivation or dismantling of the support arm 15 and the support means 19.
- the compressor barrel 2 Prior to installation in the housing 1, the compressor barrel 2 is aligned so that its longitudinal axis in the extension of the longitudinal axis of the housing 1 comes to rest, that the support arm 15 facing away from the end of the rotor 9 projects into the housing 1 and that the roller 16 of the Support arm 15 is seated on the track 17 on the housing 1 behind the stop 18.
- the support arm 15 and the support means 19 are axially displaced with the Kompressorbarrel 2 until the Kompressorbarrel 2 m the housing 1 has assumed the intended position.
- a temporary guide 29 within the bottom 4 of the housing 1 ensures a secure support of the rotor 9.
- the temporary guide 29 is later replaced by a bearing.
- the Kompressorbarrel 2 is pulled out over the cable 25.
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Supercharger (AREA)
Abstract
Description
Claims
Priority Applications (6)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
UAA200807339A UA89578C2 (uk) | 2005-10-28 | 2006-10-25 | Пристрій для бічного монтажу і демонтажу барабана компресора |
EP06806513.5A EP1952030B2 (de) | 2005-10-28 | 2006-10-25 | Vorrichtung zur seitlichen montage und demontage eines kompressorbarrels |
US12/084,168 US8677589B2 (en) | 2005-10-28 | 2006-10-25 | Device for the lateral fitting and removal of a compressor barrel |
DE502006005626T DE502006005626D1 (de) | 2005-10-28 | 2006-10-25 | Vorrichtung zur seitlichen montage und demontage eines kompressorbarrels |
JP2008536986A JP5021659B2 (ja) | 2005-10-28 | 2006-10-25 | 圧縮機バレルの横方向の着脱のための装置 |
CN2006800401617A CN101297120B (zh) | 2005-10-28 | 2006-10-25 | 用于在侧面安装和拆卸压缩机筒的装置 |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE102005052077.4 | 2005-10-28 | ||
DE102005052077.4A DE102005052077B4 (de) | 2005-10-28 | 2005-10-28 | Vorrichtung zur seitlichen Montage und Demontage eines Kompressorbarrels |
Publications (1)
Publication Number | Publication Date |
---|---|
WO2007048584A1 true WO2007048584A1 (de) | 2007-05-03 |
Family
ID=37547549
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PCT/EP2006/010256 WO2007048584A1 (de) | 2005-10-28 | 2006-10-25 | Vorrichtung zur seitlichen montage und demontage eines kompressorbarrels |
Country Status (8)
Country | Link |
---|---|
US (1) | US8677589B2 (de) |
EP (1) | EP1952030B2 (de) |
JP (1) | JP5021659B2 (de) |
CN (1) | CN101297120B (de) |
DE (2) | DE102005052077B4 (de) |
RU (1) | RU2406882C2 (de) |
UA (1) | UA89578C2 (de) |
WO (1) | WO2007048584A1 (de) |
Cited By (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN102434497A (zh) * | 2011-11-18 | 2012-05-02 | 浙江科尔泵业股份有限公司 | 用于离心泵泵芯轴向定位的自紧方法及其自紧装置 |
WO2015060734A1 (en) * | 2013-10-25 | 2015-04-30 | General Electric Company | Nozzle segment removal tool and method |
WO2015158905A1 (de) * | 2014-04-17 | 2015-10-22 | Siemens Aktiengesellschaft | Anordnung von bauteilen einer fluidenergiemaschine und montageverfahren |
EP2543868A3 (de) * | 2011-07-05 | 2016-09-14 | United Technologies Corporation | Fantriebwerk |
US10001143B2 (en) | 2013-02-26 | 2018-06-19 | Mitsubishi Heavy Industries Compressor Corporation | Method for assembling compressor, and bundle guide device |
CN109236678A (zh) * | 2018-10-30 | 2019-01-18 | 浙江水利水电学院 | 长短叶片诱导轮前置预旋板的泵结构 |
US10233945B2 (en) | 2013-02-27 | 2019-03-19 | Mitsubishi Heavy Industries Compressor Corporation | Compressor assembly method, and bundle guiding device |
Families Citing this family (24)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE102005052077B4 (de) * | 2005-10-28 | 2016-11-24 | Man Diesel & Turbo Se | Vorrichtung zur seitlichen Montage und Demontage eines Kompressorbarrels |
EP2045472A1 (de) * | 2007-10-05 | 2009-04-08 | Siemens Aktiengesellschaft | Verfahren zur Montage grosser Turbomaschinen und Vorrichtung zur Durchführung desselben |
DE102007059820A1 (de) * | 2007-12-11 | 2009-06-18 | Innovative Windpower Ag | Wartungsvorrichtung einer Windenergieanlage |
FR2952921B1 (fr) * | 2009-11-20 | 2012-05-25 | Snecma | Chariot de transport d'un module de moteur d'aeronef |
JP5554130B2 (ja) * | 2010-04-14 | 2014-07-23 | 三菱重工コンプレッサ株式会社 | コンプレッサおよびその組立方法 |
JP5550584B2 (ja) | 2011-02-25 | 2014-07-16 | 三菱重工コンプレッサ株式会社 | 圧縮機、この挿脱装置およびこの挿脱方法 |
JP5868646B2 (ja) * | 2011-09-28 | 2016-02-24 | 三菱重工コンプレッサ株式会社 | 回転機械 |
US9822798B2 (en) | 2012-02-24 | 2017-11-21 | Mitsubishi Heavy Industries Compressor Corporation | Bundle guiding device of compressor and bundle guiding method of compressor |
ITCO20120069A1 (it) * | 2012-12-27 | 2014-06-28 | Nuovo Pignone Srl | Assieme statorico di compressore di grandi dimensioni |
KR102191182B1 (ko) * | 2013-03-28 | 2020-12-16 | 에이비비 스위츠랜드 엘티디. | 로터 블록을 설치 및 분리하기 위한 캔틸레버 슬라이드 |
DE102014210297A1 (de) * | 2014-05-30 | 2015-12-03 | Lufthansa Technik Ag | Demontageverfahren für eine Gasturbine |
EP2993314B1 (de) * | 2014-09-05 | 2017-11-08 | Ansaldo Energia Switzerland AG | Vorrichtung und Verfahren zur Montage oder Demontage, zum Austausch und zur Wartung eines CAN-Verbrenners |
CN104500322B (zh) * | 2014-12-18 | 2016-12-07 | 郑清辉 | 一种浪涌发电机组系统 |
CN105458647B (zh) * | 2015-11-20 | 2017-06-30 | 沈阳黎明航空发动机(集团)有限责任公司 | 转子与静子轴向间隙无调整的动力涡轮的装配方法 |
CN105545767A (zh) * | 2016-02-08 | 2016-05-04 | 储继国 | 立式径流真空泵 |
US10662816B2 (en) | 2016-04-12 | 2020-05-26 | General Electric Company | System and method to move turbomachinery |
CN108927640B (zh) * | 2017-05-26 | 2021-02-05 | 中国电建集团上海能源装备有限公司 | 一种用于1000mw全容量火电机组给水泵芯包拆装的装置 |
EP3450704B1 (de) * | 2017-09-01 | 2020-08-05 | General Electric Company | Turbinenlagerwartungsvorrichtung und -verfahren |
FR3072137B1 (fr) | 2017-10-06 | 2020-07-24 | Safran Aircraft Engines | Dispositif pour l'assemblage d'une turbomachine, et procede utilisant le dispositif |
CN107877112A (zh) * | 2017-10-31 | 2018-04-06 | 沈阳透平机械股份有限公司 | 压缩机内机壳拆装装置 |
CN109175950B (zh) * | 2018-11-09 | 2020-07-24 | 无锡恒久安泰智能制造有限公司 | 一种立柱油缸自动装配机 |
CN109333045A (zh) * | 2018-12-04 | 2019-02-15 | 森松(江苏)重工有限公司 | 一种大型筒体内置设备安装工装 |
CN110862034B (zh) * | 2019-07-31 | 2020-12-25 | 大连长丰实业总公司 | 一种作动筒分解装配型架 |
CN110374932A (zh) * | 2019-08-08 | 2019-10-25 | 西安陕鼓动力股份有限公司 | 压缩机芯包组件、推进装置及压缩机 |
Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1923126A (en) * | 1932-06-16 | 1933-08-22 | Allis Chalmers Mfg Co | Rotary macuine-peime mover power unit and method of assembling and dismantling the same |
US3150820A (en) * | 1962-07-20 | 1964-09-29 | Worthington Corp | Turbine compressor unit |
DE2656826A1 (de) * | 1976-08-23 | 1978-03-09 | Worthington Pump | Mehrstufige zylinderzentrifugalpumpe |
JPH10220399A (ja) * | 1997-02-03 | 1998-08-18 | Mitsubishi Heavy Ind Ltd | 機器の内部部材抜き出し、組み込み装置及び方法 |
DE19919650A1 (de) * | 1998-06-03 | 1999-12-09 | Dresser Rand Co | Einstellbares Kompressorbündel-Einführungs- und Ausbausystem |
Family Cites Families (35)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US386255A (en) * | 1888-07-17 | Current-motor | ||
US2300259A (en) * | 1940-04-06 | 1942-10-27 | Wright Aeronautical Corp | Sealed engine container |
US3022740A (en) * | 1959-07-28 | 1962-02-27 | Wilfley & Sons Inc A | Centrifugal pump case alignment mounting |
US3140821A (en) * | 1962-02-05 | 1964-07-14 | Kloeckner Humboldt Deutz Ag | Gas turbine plant |
US3556672A (en) * | 1969-05-26 | 1971-01-19 | Gen Electric | Gas turbine support arrangement |
US3927763A (en) * | 1970-12-15 | 1975-12-23 | Bbc Sulzer Turbomaschinen | Installation unit for a multistage radial compressor |
GB1409902A (en) * | 1972-05-24 | 1975-10-15 | Rolls Royce | Stationary gas turbine power plant mounting apparatus |
SE387408B (sv) * | 1974-12-23 | 1976-09-06 | Stal Laval Turbin Ab | Forfarande vid montage i en maskinhall av ett gasturbinaggregat |
DE2719850C3 (de) | 1977-05-04 | 1981-06-25 | MTU Motoren- und Turbinen-Union München GmbH, 8000 München | Vorrichtung zur Wartung von Gasturbinentriebwerken, insbesondere Gasturbinenstrahltriebwerken |
US4451979A (en) * | 1980-10-27 | 1984-06-05 | Elliott Turbomachinery Company, Inc. | Assembly and disassembly apparatus for use with a rotary machine |
IT1150185B (it) * | 1982-02-05 | 1986-12-10 | Nuovo Pignone Spa | Carro ponte perfezionato per cabinati di turbine a gas di potenza |
US4590653A (en) * | 1983-05-04 | 1986-05-27 | General Electric Company | Turbine rotor heating, disassembly, handling and reassembly method and apparatus |
US4567649A (en) * | 1983-05-04 | 1986-02-04 | General Electric Company | System for heating, disassembly, handling and reassembly of a turbine rotor |
DE3528724A1 (de) * | 1985-08-09 | 1987-02-12 | Kuehnle Kopp Kausch Ag | Verfahren und vorrichtung zur montage schwerer einseitig gelagerter laufraeder von turboverdichtern oder ventilatoren |
GB2199461B (en) | 1986-12-24 | 1991-03-13 | Philips Electronic Associated | Image display apparatus |
DE59007880D1 (de) * | 1990-12-10 | 1995-01-12 | Asea Brown Boveri | Lagerung einer thermischen Turbomaschine. |
NZ241415A (en) * | 1992-01-27 | 1995-04-27 | Air New Zealand Ltd | Gas turbine engine transporting frames |
US5575607A (en) * | 1994-11-02 | 1996-11-19 | United Technologies Corporation | Jet engine transport vehicle lift system and a build cell |
US5816367A (en) * | 1995-11-30 | 1998-10-06 | Stanley Aviation Corporation | Jet aircraft engine transport apparatus |
DE29520021U1 (de) * | 1995-12-18 | 1996-02-01 | Duerr Gmbh & Co | Als Radialventilator ausgebildeter Großventilator |
DE19617090A1 (de) * | 1996-04-29 | 1997-10-30 | Konrad Wolfgang Maier | Kran- und Transportvorrichtung mit Laufkatze |
DE29719605U1 (de) * | 1997-11-05 | 1997-12-18 | Gebhardt Ventilatoren | Ventilatoranordnung |
JP4088369B2 (ja) * | 1998-06-09 | 2008-05-21 | 三菱重工業株式会社 | 低圧蒸気タービンの輸送方法及び輸送用治具 |
US6279309B1 (en) * | 1998-09-24 | 2001-08-28 | Ramgen Power Systems, Inc. | Modular multi-part rail mounted engine assembly |
US6170141B1 (en) * | 1998-09-25 | 2001-01-09 | Stanley Aviation Corporation | Shipping system for jet aircraft engine and method of installing and removing jet aircraft engine |
US6224332B1 (en) * | 1999-05-14 | 2001-05-01 | General Electric Co. | Apparatus and methods for installing, removing and adjusting an inner turbine shell section relative to an outer turbine shell section |
DE19927765C2 (de) | 1999-06-17 | 2003-05-08 | Metso Lindemann Gmbh | Verfahren und Vorrichtung zur Demontage/Remontage von Hämmern, Hammerachsen und/oder Schutzkappen der Rotoren von Hammerbrechern |
DE10344718B3 (de) * | 2003-09-26 | 2005-01-05 | Elektror M. Müller GmbH | Seitenkanalverdichter |
US7779540B2 (en) * | 2005-08-12 | 2010-08-24 | United Technologies Corporation | Apparatus and method for quadrail ergonomic assembly |
DE102005052077B4 (de) * | 2005-10-28 | 2016-11-24 | Man Diesel & Turbo Se | Vorrichtung zur seitlichen Montage und Demontage eines Kompressorbarrels |
EP1996796B1 (de) * | 2006-03-17 | 2016-01-06 | Alstom Technology Ltd | Vorrichtung und Verfahren zur Lagerung einer Strömungsrotationsmaschine |
US7559280B2 (en) * | 2006-04-28 | 2009-07-14 | United Technologies Corporation | Adjustable link system |
US7976266B2 (en) * | 2006-06-30 | 2011-07-12 | Solar Turbines Inc | Power system |
GB0613929D0 (en) * | 2006-07-13 | 2006-08-23 | Rolls Royce Plc | An engine core stand arrangement and method of removal and transportation of an engine core |
BRPI0717088B1 (pt) * | 2006-09-25 | 2019-10-29 | Dresser Rand Co | sistema de proteção de acoplamento |
-
2005
- 2005-10-28 DE DE102005052077.4A patent/DE102005052077B4/de not_active Withdrawn - After Issue
-
2006
- 2006-10-25 WO PCT/EP2006/010256 patent/WO2007048584A1/de active Application Filing
- 2006-10-25 CN CN2006800401617A patent/CN101297120B/zh not_active Expired - Fee Related
- 2006-10-25 RU RU2008115026/06A patent/RU2406882C2/ru not_active IP Right Cessation
- 2006-10-25 UA UAA200807339A patent/UA89578C2/uk unknown
- 2006-10-25 EP EP06806513.5A patent/EP1952030B2/de not_active Expired - Fee Related
- 2006-10-25 DE DE502006005626T patent/DE502006005626D1/de active Active
- 2006-10-25 JP JP2008536986A patent/JP5021659B2/ja not_active Expired - Fee Related
- 2006-10-25 US US12/084,168 patent/US8677589B2/en not_active Expired - Fee Related
Patent Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1923126A (en) * | 1932-06-16 | 1933-08-22 | Allis Chalmers Mfg Co | Rotary macuine-peime mover power unit and method of assembling and dismantling the same |
US3150820A (en) * | 1962-07-20 | 1964-09-29 | Worthington Corp | Turbine compressor unit |
DE2656826A1 (de) * | 1976-08-23 | 1978-03-09 | Worthington Pump | Mehrstufige zylinderzentrifugalpumpe |
JPH10220399A (ja) * | 1997-02-03 | 1998-08-18 | Mitsubishi Heavy Ind Ltd | 機器の内部部材抜き出し、組み込み装置及び方法 |
DE19919650A1 (de) * | 1998-06-03 | 1999-12-09 | Dresser Rand Co | Einstellbares Kompressorbündel-Einführungs- und Ausbausystem |
Cited By (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP2543868A3 (de) * | 2011-07-05 | 2016-09-14 | United Technologies Corporation | Fantriebwerk |
CN102434497A (zh) * | 2011-11-18 | 2012-05-02 | 浙江科尔泵业股份有限公司 | 用于离心泵泵芯轴向定位的自紧方法及其自紧装置 |
CN102434497B (zh) * | 2011-11-18 | 2013-09-04 | 浙江科尔泵业股份有限公司 | 用于离心泵泵芯轴向定位的自紧方法及其自紧装置 |
US10001143B2 (en) | 2013-02-26 | 2018-06-19 | Mitsubishi Heavy Industries Compressor Corporation | Method for assembling compressor, and bundle guide device |
US10233945B2 (en) | 2013-02-27 | 2019-03-19 | Mitsubishi Heavy Industries Compressor Corporation | Compressor assembly method, and bundle guiding device |
WO2015060734A1 (en) * | 2013-10-25 | 2015-04-30 | General Electric Company | Nozzle segment removal tool and method |
WO2015158905A1 (de) * | 2014-04-17 | 2015-10-22 | Siemens Aktiengesellschaft | Anordnung von bauteilen einer fluidenergiemaschine und montageverfahren |
CN106232948A (zh) * | 2014-04-17 | 2016-12-14 | 西门子公司 | 流体动力机械的构件的装置和装配方法 |
CN109236678A (zh) * | 2018-10-30 | 2019-01-18 | 浙江水利水电学院 | 长短叶片诱导轮前置预旋板的泵结构 |
Also Published As
Publication number | Publication date |
---|---|
JP2009513863A (ja) | 2009-04-02 |
JP5021659B2 (ja) | 2012-09-12 |
EP1952030B2 (de) | 2015-01-21 |
EP1952030A1 (de) | 2008-08-06 |
DE102005052077B4 (de) | 2016-11-24 |
DE502006005626D1 (de) | 2010-01-21 |
UA89578C2 (uk) | 2010-02-10 |
US20090288291A1 (en) | 2009-11-26 |
RU2406882C2 (ru) | 2010-12-20 |
US8677589B2 (en) | 2014-03-25 |
RU2008115026A (ru) | 2009-12-10 |
CN101297120A (zh) | 2008-10-29 |
DE102005052077A1 (de) | 2007-05-10 |
CN101297120B (zh) | 2010-12-22 |
EP1952030B1 (de) | 2009-12-09 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
WO2007048584A1 (de) | Vorrichtung zur seitlichen montage und demontage eines kompressorbarrels | |
EP1394451B1 (de) | Wellenabdichtung für Turbolader | |
DE1930959A1 (de) | Rotations-Stroemungsmaschine fuer elastische Stroemungsmittel | |
DE7033081U (de) | Turbinengehaeuse. | |
DE102016204076A1 (de) | Abgasturbolader | |
DE2656826A1 (de) | Mehrstufige zylinderzentrifugalpumpe | |
EP3201440A1 (de) | Gasturbine mit hebevorrichtung | |
WO2014206638A1 (de) | Kreiselpumpe | |
EP2978942A1 (de) | Kragträgerschlitten für montage und demontage eines rotorblocks | |
DE102012206302A1 (de) | Variable Turbinen-/Verdichtergeometrie | |
DE2413674A1 (de) | Radialer turboverdichter | |
DE4339060A1 (de) | Getriebeverdichter für die Verdichtung von Sauerstoff | |
WO2014019976A1 (de) | Segmentplattenventil und dampfturbinenanordnung | |
DE1403540A1 (de) | Pumpe | |
DE102015003864B3 (de) | Verschlussdeckel mit integrierter Demontage-/Montagefunktion | |
DE1628271C3 (de) | Mehrstufiger Flüssigkeitsringverdichter bzw. mehrstufige Flüssigkeitsringpumpe | |
DE102012211417A1 (de) | Leitschaufel-Anordnung für einen Abgasturbolader | |
DE19824421A1 (de) | Gehäuseausbildung an einer Gasturbine | |
WO2019034276A1 (de) | Verstellbarer leitapparat für eine turbine, turbine für einen abgasturbolader und abgasturbolader | |
DE2523213C3 (de) | Kompakte mehrstufige Kreiselpumpe mit Zwischenentnahme und Wiedereinspeisung | |
DE202018001455U1 (de) | Bremssystem mit Blockierunterstützung für Seile aus Natur- oder Synthetikfasern und Bandmaterial | |
DE102012018066A1 (de) | Wasserturbine | |
WO2018099592A1 (de) | Abgasturbolader | |
DE102008057532B4 (de) | Ladeeinrichtung | |
DE7206517U (de) | Zwischenflansch Rückschlagventil |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
WWE | Wipo information: entry into national phase |
Ref document number: 200680040161.7 Country of ref document: CN |
|
121 | Ep: the epo has been informed by wipo that ep was designated in this application | ||
ENP | Entry into the national phase |
Ref document number: 2008536986 Country of ref document: JP Kind code of ref document: A |
|
WWE | Wipo information: entry into national phase |
Ref document number: 2021/KOLNP/2008 Country of ref document: IN |
|
WWE | Wipo information: entry into national phase |
Ref document number: 2006806513 Country of ref document: EP |
|
WWE | Wipo information: entry into national phase |
Ref document number: 2008115026 Country of ref document: RU |
|
WWE | Wipo information: entry into national phase |
Ref document number: 12084168 Country of ref document: US |
|
WWP | Wipo information: published in national office |
Ref document number: 2006806513 Country of ref document: EP |