EP3143261A1 - Apparatus for orienting a guide vane support relative to a turbine casing - Google Patents
Apparatus for orienting a guide vane support relative to a turbine casingInfo
- Publication number
- EP3143261A1 EP3143261A1 EP15720738.2A EP15720738A EP3143261A1 EP 3143261 A1 EP3143261 A1 EP 3143261A1 EP 15720738 A EP15720738 A EP 15720738A EP 3143261 A1 EP3143261 A1 EP 3143261A1
- Authority
- EP
- European Patent Office
- Prior art keywords
- adjusting element
- guide
- adjusting
- housing
- guide channel
- 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
Links
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
- F01D25/24—Casings; Casing parts, e.g. diaphragms, casing fastenings
- F01D25/246—Fastening of diaphragms or stator-rings
-
- 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
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2230/00—Manufacture
- F05D2230/60—Assembly methods
Definitions
- the present invention relates to an apparatus for off ⁇ directing a guide vane to a housing of a door ⁇ bine.
- the invention relates particularly to such a pre ⁇ direction, comprising a guiding device with an ERS th region and a second region wherein the first region in a receptacle of the guide vane and the two ⁇ th region are arranged in a recess of the housing.
- the second region of the guide device has a guide channel with a first internal thread, wherein in the guide channel, a first adjusting element is arranged with a first Au ⁇ Hzgewinde.
- the first external thread can be screwed to the first internal thread.
- the first adjusting element is so positionable in the guide channel, that in the different bearing ⁇ zen of the guiding device against a supporting surface of the initial recess, a force flow from the receptacle to the guide device by the first adjusting element extends.
- vane carriers are attached to the outer turbine housing.
- the vane carriers have fixed vanes which direct the internal flow in a predefined manner.
- a predefined flow exactly implement ei ⁇ nes fluid in a turbine
- the stator blade carrier with the blades must be exactly housing the turbine and are oriented to the rotor of the turbine.
- the guide vanes with the guide vanes must be arranged in an exactly predefined position with respect to the rotor blades of the rotor in order to provide the predefined flow of the fluid and to produce the predefined function-dependent games between the guide vanes and the rotor or rotor blades and vane carrier.
- a positioning system for aligning a guide vane carrier of a turbine to a housing of the turbine to each other which has a positioning ⁇ tion element with a first region and a second region, and an actuating element.
- the Position istsele ⁇ ment is positively fastened with the first portion in a mating opening in the guide vane.
- the positioning element can be fastened to the second region in a receptacle ⁇ opening of the housing by means of the adjusting element.
- the position of the positioning element in the receiving opening is adjustable relative to the housing.
- This device for aligning a guide vane carrier to a housing of a turbine has the disadvantage that for aligning ⁇ an upper part of the housing of the turbine fitting pieces must be used, which are attached to a lower part of the housing by means of a screw connection. Such alignment is particularly complex and requires a variety of different fittings. Therefore, it is the object of the present invention to provide a device for aligning a guide vane carrier to a housing of a turbine, which at least partially does not have the above disadvantages.
- the object is achieved by a device for aligning a guide vane carrier to a housing of a turbine, comprising a Füh ⁇ tion device with a first region and a second region, wherein the first region in a receptacle of the guide vane carrier and the second region is arranged in a recess of the housing.
- the second region of the guide ⁇ device has a guide channel with a first internal thread, wherein in the guide channel, a first Justier ⁇ element is arranged with a first external thread.
- the first external thread is with the first internal thread
- the first adjusting element can be arranged in the guide channel such that when the guide device is supported against a support surface of the recess, a force flow from the receptacle to the guide device extends through the first adjusting element.
- a second adjusting element with a second external thread is arranged ⁇ , wherein the second external thread with the first inner screw is screwed.
- the second adjusting element is so positionable in the guide channel, that a power flow of egg ⁇ nem top of the housing to the guide device by the second adjusting element extends.
- the first adjusting element is secured via a securing device with the second adjusting element in the guide channel against rotation relative to the guide channel.
- the first adjusting element and the second adjusting element are preferably cylindrical and have a length which ensures that during the adjustment process always a sufficient number of threads with the ers ⁇ th internal thread of the guide channel are engaged to forces acting on the device without damage of the thread. Furthermore, the length of the first
- Justification element adjusting the guide vane carrier to the housing and the length of the second adjusting element allow adjustment of the upper part to the vane carrier.
- the length of the adjusting elements is limited in particular by the fact that an adjusting element may not hinder an adjustment of the respective other adjusting element. Accordingly, it is advantageous if the adjusting elements for adjustment of the second adjusting element spaced from each other are integrally ⁇ belongs to the guide channel.
- the guide blade carrier By rotating the first adjusting element relative to the guide channel, the guide blade carrier can be raised or lowered relative to the housing and thus an adjustment of the guide blade carrier to the housing is possible.
- the second adjusting element By rotating the second adjusting element is a contact surface for the upper ⁇ part of the housing can be raised or lowered and thus a Jus ⁇ animals of the upper part to the vane carrier possible.
- the first area is arranged on the guide blade carrier and the second area on the housing.
- the first region can be arranged in a receptacle of the housing and the second region can be arranged in a recess of the guide blade carrier.
- a relative movement takes place between the guide device and the guide blade carrier during the adjustment process.
- an adjusting means is disposed between the first adjusting element and the supporting surface of the off ⁇ recess.
- the adjusting means is preferably disc-shaped.
- a first JUS animal element facing contact surface of said adjustment ent ⁇ speaks preferably substantially a negative of the corresponding surface of the first adjustment means.
- the adjusting means has a part-circular
- a contact surface of the first adjusting element and adjusting means is formed substantially spherical. It is preferable that the adjusting means has a convex contact surface and the first adjusting element has a concave surface Kon ⁇ clock. About a pairing of a convex and egg ⁇ ner corresponding concave surface is a relative
- the device has a first screw for fixing the guide device to the vane carrier.
- the first screw prevents the guide device dissolves when cooling the turbine from the recording.
- the first region can be arranged in a form-fitting manner in the receptacle.
- the first adjusting element has a form ⁇ closing section for engaging a mounting tool, which is guided by the guide channel.
- the second adjusting element is preferably not yet arranged in the guide channel.
- the second adjusting element can have a passage for a corresponding tool, so that the second adjusting element can also be arranged in the guide channel during the adjustment by means of the first adjusting element.
- the securing means comprises a second screw for clamping together the first JUS animal elements with the second adjusting element in the guide channel ⁇ .
- the first Justierele ⁇ ment a second internal thread for receiving a thread of the second screw and the second adjusting element has a bore for passing the second screw and a contact surface for supporting a screw head of the second screw ⁇ .
- the object is achieved by a housing ei ⁇ ner turbine with a vane carrier, wherein between the vane carrier and the housing at least one Inventive device is arranged.
- a method for aligning a guide blade carrier to a housing of a turbine comprising the steps:
- Figure 1 shows an embodiment of a device according to the invention.
- a device 1 according to the invention is shown in a longitudinal section.
- the device 1 comprises a guide ⁇ means 4 with a first portion 5 and a second region.
- the first portion 5 is positively located in a recess 7 of a web receiving a guide vane carrier 2 and xed by a first screw 18 at this ⁇ fi.
- the second region 6 is arranged in a recess 8 of a housing 3 and has a guide channel 9 with a through ⁇ usual first internal thread 10.
- the first internal thread 10 may also be interrupted, in particular in a middle section.
- a first adjusting element 11 is arranged with a first external thread 12, so that the first external thread 12 is in engagement with the first internal thread 10.
- the first adjusting element 11 has a substantially cylindrical base body, which on a support side
- the support side is arranged on egg ⁇ ner part spherical contact side of an adjusting 17.
- the contact side and the contact side are formed in such a way that they essentially correspond inversely and thus in the paired state touch each other essentially over their entire surface.
- the adjustment means 17 is Zvi ⁇ rule a support surface 13 of the recess 8 and the first adjustment member 11 is arranged.
- a second adjusting element 14 is provided with a second External thread 15 arranged so that the second external thread
- the second adjusting element 14 has a substantially cylindrical base body and a bore 21 for the passage of a second screw 19 and a contact surface 22 for a screw head 23.
- a top ⁇ part 16 of the housing 3 relative to the guide blade carrier 2 can be raised or lowered and thus adjustable.
- the device 1 has a second screw 19, which is guided through the bore 21 of the second adjusting element 14 and arranged with a threaded portion in a second internal thread 20 of the first adjusting element 11.
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Abstract
Description
Claims
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
PL15720738T PL3143261T3 (en) | 2014-07-25 | 2015-05-11 | Apparatus for orienting a guide vane support relative to a turbine casing |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE102014214703.4A DE102014214703A1 (en) | 2014-07-25 | 2014-07-25 | Apparatus for aligning a vane carrier to a housing of a turbine |
PCT/EP2015/060303 WO2016012115A1 (en) | 2014-07-25 | 2015-05-11 | Apparatus for orienting a guide vane support relative to a turbine casing |
Publications (2)
Publication Number | Publication Date |
---|---|
EP3143261A1 true EP3143261A1 (en) | 2017-03-22 |
EP3143261B1 EP3143261B1 (en) | 2018-03-14 |
Family
ID=53052872
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP15720738.2A Active EP3143261B1 (en) | 2014-07-25 | 2015-05-11 | Apparatus for orienting a guide vane support relative to a turbine casing |
Country Status (8)
Country | Link |
---|---|
US (1) | US10865659B2 (en) |
EP (1) | EP3143261B1 (en) |
JP (1) | JP6453440B2 (en) |
CN (1) | CN106536871B (en) |
BR (1) | BR112017001507B8 (en) |
DE (1) | DE102014214703A1 (en) |
PL (1) | PL3143261T3 (en) |
WO (1) | WO2016012115A1 (en) |
Families Citing this family (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE102018120808A1 (en) * | 2018-08-27 | 2020-02-27 | Renk Aktiengesellschaft | Bearing arrangement and adjusting screw for adjusting the bearing play |
US11988101B2 (en) | 2022-03-10 | 2024-05-21 | Ge Infrastructure Technology Llc | Device for fixing position of adjustable rows of guide vanes of turbomachine |
US11920482B2 (en) * | 2022-03-10 | 2024-03-05 | General Electric Company | Device for fixing position of adjustable rows of guide vanes of turbomachine |
Family Cites Families (35)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1706651A (en) * | 1928-03-26 | 1929-03-26 | James D Casey | Extension bolt |
DE726510C (en) * | 1940-01-25 | 1942-10-15 | Aeg | Carrying and centering device for guide wheels of steam or gas turbines divided into the parting line of the housing |
US2247423A (en) * | 1940-01-25 | 1941-07-01 | Gen Electric | Elastic fluid turbine diaphragm supporting and centering arrangement |
US2886090A (en) * | 1956-06-29 | 1959-05-12 | Rosan Joseph | Top locking insert |
US3498727A (en) * | 1968-01-24 | 1970-03-03 | Westinghouse Electric Corp | Blade ring support |
US3461769A (en) * | 1968-03-06 | 1969-08-19 | Fritz V Brosseit | Adjustable length shoulder screw |
US4204803A (en) * | 1978-07-21 | 1980-05-27 | General Electric Company | Diaphragm support |
DE59106601D1 (en) * | 1991-11-22 | 1995-11-02 | Werner Simon | Tightening unit. |
JPH10299411A (en) * | 1997-04-28 | 1998-11-10 | Toshiba Corp | Supporting device for steam turbine nozzle |
US6357953B1 (en) * | 1999-12-16 | 2002-03-19 | General Motors Corporation | Tolerance compensation apparatus |
US6325596B1 (en) * | 2000-07-21 | 2001-12-04 | General Electric Company | Turbine diaphragm support system |
US6547523B2 (en) * | 2001-09-12 | 2003-04-15 | General Electric Company | Diaphragm screw support for and method of supporting a turbine diaphragm |
US7645106B2 (en) * | 2002-09-03 | 2010-01-12 | Mark Gordon | Cone-head thrust screw |
DE202004019153U1 (en) * | 2004-12-10 | 2005-02-10 | Böllhoff Verbindungstechnik GmbH | Screw connection with tolerance compensation |
US7329098B2 (en) * | 2005-05-06 | 2008-02-12 | Geenral Electric Company | Adjustable support bar with adjustable shim design for steam turbine diaphragms |
DE202005010873U1 (en) * | 2005-07-11 | 2005-09-22 | Böllhoff Verbindungstechnik GmbH | Tolerance equalizing unit for automatic equalizing of tolerances in the distance between two structural components and is cost effective to produce |
US7458770B2 (en) * | 2005-11-30 | 2008-12-02 | General Electric Company | Adjustable support for steam turbine diaphragms |
US7588386B2 (en) * | 2006-08-30 | 2009-09-15 | Silicon Valley Automation | Leveling and aligning device |
US7887291B2 (en) | 2007-05-15 | 2011-02-15 | General Electric Company | Support bar with adjustable shim design for turbine diaphragms |
US8430625B2 (en) | 2007-06-19 | 2013-04-30 | Siemens Demag Delaval Turbomachinery, Inc. | Centerline suspension for turbine internal component |
US8152117B2 (en) * | 2008-12-30 | 2012-04-10 | Paul R. Gain | Adjustable bushing |
DE102009012751A1 (en) | 2009-03-12 | 2010-09-23 | Siemens Aktiengesellschaft | Device for vertical and horizontal positioning of guide vanes in the turbine housing in the installed state |
EP2478292B1 (en) | 2009-09-17 | 2015-04-29 | Koninklijke Philips N.V. | Lighting system with gravity controlled light beam |
JP2011169246A (en) * | 2010-02-19 | 2011-09-01 | Mitsubishi Heavy Ind Ltd | Gas turbine casing structure |
CN102418733B (en) * | 2010-09-28 | 2013-08-07 | 富泰华工业(深圳)有限公司 | Height adjusting mechanism and assembly method for assembling electronic device by using same |
US8894362B2 (en) * | 2010-10-21 | 2014-11-25 | Siemens Energy, Inc. | Torque pin for adjusting position of blade ring relative to rotor in a gas turbine engine |
US9285067B2 (en) * | 2011-04-28 | 2016-03-15 | Aktiebolaget Skf | Modular double adjustable chock |
DE102012202468B3 (en) * | 2012-02-17 | 2013-07-04 | Siemens Aktiengesellschaft | turbomachinery |
US9828878B2 (en) * | 2012-05-30 | 2017-11-28 | Dresser-Rand Company | Method and apparatus for supporting and aligning diaphragms in turbomachines |
EP2772617B1 (en) * | 2013-02-27 | 2018-11-28 | Ansaldo Energia Switzerland AG | Rotary flow machine with support means |
US9500130B2 (en) * | 2013-03-05 | 2016-11-22 | General Electric Company | Centerline support bar for steam turbine component |
US20140353463A1 (en) * | 2013-06-04 | 2014-12-04 | Fluor Technologies Coporation | Rotating equipment modularization |
US20150063999A1 (en) * | 2013-08-27 | 2015-03-05 | Schaeffler Technologies Gmbh & Co. Kg | Press fit keyed outer race in stator |
DE112014005921T5 (en) * | 2013-12-19 | 2016-10-13 | Mitsubishi Hitachi Power Systems, Ltd. | Positioning device, rotating machine comprising this positioning device and positioning method |
JP6194553B2 (en) * | 2014-01-27 | 2017-09-13 | 三菱日立パワーシステムズ株式会社 | POSITION ADJUSTING DEVICE, ROTARY MACHINE HAVING THE SAME, AND POSITION ADJUSTING METHOD |
-
2014
- 2014-07-25 DE DE102014214703.4A patent/DE102014214703A1/en not_active Withdrawn
-
2015
- 2015-05-11 CN CN201580041397.1A patent/CN106536871B/en active Active
- 2015-05-11 EP EP15720738.2A patent/EP3143261B1/en active Active
- 2015-05-11 WO PCT/EP2015/060303 patent/WO2016012115A1/en active Application Filing
- 2015-05-11 PL PL15720738T patent/PL3143261T3/en unknown
- 2015-05-11 US US15/326,731 patent/US10865659B2/en active Active
- 2015-05-11 JP JP2017504080A patent/JP6453440B2/en active Active
- 2015-05-11 BR BR112017001507A patent/BR112017001507B8/en active IP Right Grant
Also Published As
Publication number | Publication date |
---|---|
BR112017001507B1 (en) | 2022-10-18 |
PL3143261T3 (en) | 2018-08-31 |
CN106536871A (en) | 2017-03-22 |
JP6453440B2 (en) | 2019-01-16 |
BR112017001507B8 (en) | 2023-04-25 |
WO2016012115A1 (en) | 2016-01-28 |
EP3143261B1 (en) | 2018-03-14 |
US10865659B2 (en) | 2020-12-15 |
US20170204745A1 (en) | 2017-07-20 |
CN106536871B (en) | 2018-04-27 |
DE102014214703A1 (en) | 2016-01-28 |
JP2017530286A (en) | 2017-10-12 |
BR112017001507A2 (en) | 2017-12-05 |
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