EP0899426A3 - Guide vane for a gas turbine - Google Patents

Guide vane for a gas turbine Download PDF

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Publication number
EP0899426A3
EP0899426A3 EP98114445A EP98114445A EP0899426A3 EP 0899426 A3 EP0899426 A3 EP 0899426A3 EP 98114445 A EP98114445 A EP 98114445A EP 98114445 A EP98114445 A EP 98114445A EP 0899426 A3 EP0899426 A3 EP 0899426A3
Authority
EP
European Patent Office
Prior art keywords
guide vane
projection
gas turbine
platform
vane
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
EP98114445A
Other languages
German (de)
French (fr)
Other versions
EP0899426B1 (en
EP0899426A2 (en
Inventor
Rudolf Stanka
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
MTU Aero Engines AG
Original Assignee
MTU Motoren und Turbinen Union Muenchen GmbH
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by MTU Motoren und Turbinen Union Muenchen GmbH filed Critical MTU Motoren und Turbinen Union Muenchen GmbH
Publication of EP0899426A2 publication Critical patent/EP0899426A2/en
Publication of EP0899426A3 publication Critical patent/EP0899426A3/en
Application granted granted Critical
Publication of EP0899426B1 publication Critical patent/EP0899426B1/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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
    • F01D9/00—Stators
    • F01D9/02—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
    • F01D9/04—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector
    • F01D9/042—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector fixing blades to stators

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)
  • Control Of Turbines (AREA)

Abstract

Die Erfindung betrifft eine Leitschaufel für eine Gasturbine, insbesondere eine Niederdruckturbine, mit einem Schaufelblatt, das sich zwischen einer inneren Plattform und einer äußeren Plattform erstreckt, wobei die äußere Plattform Befestigungsmittel zur Anbringung an einem Gehäuse aufweist, und wobei wenigstens eine von der äußeren oder inneren Plattform an einer ersten Stirnfläche einen Vorsprung mit vorstehender Seitenfläche aufweist und an einer zweiten, gegenüberliegenden Stirnfläche eine Aufnahme zum formschlüssigen Aufnehmen eines Vorsprungs einer benachbarten Leitschaufel aufweist, deren Dimensionierung so auf den Vorsprung abgestimmt ist, daß die Plattformen benachbarter Leitschaufeln im montierten Zustand fluchten, ein Leitschaufelsegment aus wenigsten drei Leitschaufeln sowie einen Leitkranzverbund.

Figure 00000001
The invention relates to a vane for a gas turbine, particularly a low pressure turbine, having a blade that extends between an inner platform and an outer platform, the outer platform having fasteners for attachment to a housing, and at least one of the outer or inner Platform has a projection with a protruding side surface on a first end face and has a receptacle on a second, opposite end face for positively receiving a projection of an adjacent guide vane, the dimensions of which are matched to the projection such that the platforms of adjacent guide vanes are aligned when assembled Guide vane segment consisting of at least three guide vanes and a guide ring assembly.
Figure 00000001
EP98114445A 1997-08-23 1998-08-01 Guide vane for a gas turbine Expired - Lifetime EP0899426B1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE29715180U DE29715180U1 (en) 1997-08-23 1997-08-23 Guide blade for a gas turbine
DE29715180U 1997-08-23

Publications (3)

Publication Number Publication Date
EP0899426A2 EP0899426A2 (en) 1999-03-03
EP0899426A3 true EP0899426A3 (en) 1999-12-08
EP0899426B1 EP0899426B1 (en) 2003-04-02

Family

ID=8045040

Family Applications (1)

Application Number Title Priority Date Filing Date
EP98114445A Expired - Lifetime EP0899426B1 (en) 1997-08-23 1998-08-01 Guide vane for a gas turbine

Country Status (4)

Country Link
US (1) US6217282B1 (en)
EP (1) EP0899426B1 (en)
JP (1) JPH11107704A (en)
DE (2) DE29715180U1 (en)

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US6435813B1 (en) * 2000-05-10 2002-08-20 General Electric Company Impigement cooled airfoil
RU2272151C2 (en) * 2000-12-28 2006-03-20 Альстом Текнолоджи Лтд Axial-flow turbine stator blade
DE10111896B8 (en) * 2001-03-13 2012-06-06 Eads Space Transportation Gmbh Metallic ring for the connection of two rotationally symmetrical structural parts
RU2362886C2 (en) * 2002-08-14 2009-07-27 Вольво Аэро Корпорейшн Manufacturing method of stator component (versions)
US7597542B2 (en) * 2005-08-30 2009-10-06 General Electric Company Methods and apparatus for controlling contact within stator assemblies
US7594404B2 (en) * 2006-07-27 2009-09-29 United Technologies Corporation Embedded mount for mid-turbine frame
US8257038B2 (en) * 2008-02-01 2012-09-04 Siemens Energy, Inc. Metal injection joining
US8043044B2 (en) * 2008-09-11 2011-10-25 General Electric Company Load pin for compressor square base stator and method of use
US20100068050A1 (en) * 2008-09-12 2010-03-18 General Electric Company Gas turbine vane attachment
EP2295724B1 (en) * 2009-08-28 2012-02-29 Siemens Aktiengesellschaft Stator vane for an axial-flow turbomachine and corresponding stator vane assembly
US8360716B2 (en) * 2010-03-23 2013-01-29 United Technologies Corporation Nozzle segment with reduced weight flange
US8356975B2 (en) * 2010-03-23 2013-01-22 United Technologies Corporation Gas turbine engine with non-axisymmetric surface contoured vane platform
US9976433B2 (en) 2010-04-02 2018-05-22 United Technologies Corporation Gas turbine engine with non-axisymmetric surface contoured rotor blade platform
FR2961554B1 (en) * 2010-06-18 2012-07-20 Snecma ANGULAR RECTIFIER SECTOR FOR TURBOMACHINE COMPRESSOR, TURBOMACHINE RECTIFIER AND TURBOMACHINE COMPRISING SUCH A SECTOR
DE102010041808B4 (en) * 2010-09-30 2014-10-23 Siemens Aktiengesellschaft Blade segment, turbomachinery and process for their preparation
JP5358559B2 (en) * 2010-12-28 2013-12-04 株式会社日立製作所 Axial flow compressor
US9028744B2 (en) 2011-08-31 2015-05-12 Pratt & Whitney Canada Corp. Manufacturing of turbine shroud segment with internal cooling passages
US9079245B2 (en) 2011-08-31 2015-07-14 Pratt & Whitney Canada Corp. Turbine shroud segment with inter-segment overlap
US8784044B2 (en) 2011-08-31 2014-07-22 Pratt & Whitney Canada Corp. Turbine shroud segment
US8784041B2 (en) 2011-08-31 2014-07-22 Pratt & Whitney Canada Corp. Turbine shroud segment with integrated seal
US8784037B2 (en) 2011-08-31 2014-07-22 Pratt & Whitney Canada Corp. Turbine shroud segment with integrated impingement plate
EP2617945B1 (en) * 2012-01-23 2018-03-14 MTU Aero Engines GmbH Rotor for a turbo machine and manufacturing process
EP2666969B1 (en) 2012-05-21 2017-04-19 General Electric Technology GmbH Turbine diaphragm construction
EP2669477B1 (en) * 2012-05-31 2017-04-05 General Electric Technology GmbH Shroud for airfoils
US10309235B2 (en) 2012-08-27 2019-06-04 United Technologies Corporation Shiplap cantilevered stator
ITCO20130004A1 (en) * 2013-02-20 2014-08-21 Nuovo Pignone Srl METHOD TO REALIZE A IMPELLER FROM SECTOR SEGMENTS
US9556746B2 (en) 2013-10-08 2017-01-31 Pratt & Whitney Canada Corp. Integrated strut and turbine vane nozzle arrangement
US9816387B2 (en) 2014-09-09 2017-11-14 United Technologies Corporation Attachment faces for clamped turbine stator of a gas turbine engine
US10018075B2 (en) * 2015-04-22 2018-07-10 General Electric Company Methods for positioning neighboring nozzles of a gas turbine engine
JP6763157B2 (en) * 2016-03-11 2020-09-30 株式会社Ihi Turbine nozzle
WO2017158637A1 (en) 2016-03-15 2017-09-21 株式会社 東芝 Turbine and turbine stator blade
GB2551164B (en) * 2016-06-08 2019-12-25 Rolls Royce Plc Metallic stator vane
US11274569B2 (en) 2017-12-13 2022-03-15 Pratt & Whitney Canada Corp. Turbine shroud cooling
US10502093B2 (en) * 2017-12-13 2019-12-10 Pratt & Whitney Canada Corp. Turbine shroud cooling
US10570773B2 (en) 2017-12-13 2020-02-25 Pratt & Whitney Canada Corp. Turbine shroud cooling
US10533454B2 (en) 2017-12-13 2020-01-14 Pratt & Whitney Canada Corp. Turbine shroud cooling
US10738634B2 (en) * 2018-07-19 2020-08-11 Raytheon Technologies Corporation Contact coupled singlets
JP2021143658A (en) * 2020-03-13 2021-09-24 東芝エネルギーシステムズ株式会社 Turbine stationary blade
US11365645B2 (en) 2020-10-07 2022-06-21 Pratt & Whitney Canada Corp. Turbine shroud cooling
US12055056B2 (en) 2021-06-18 2024-08-06 Rtx Corporation Hybrid superalloy article and method of manufacture thereof
EP4105450A1 (en) 2021-06-18 2022-12-21 Raytheon Technologies Corporation Passive clearance control (apcc) system produced by field assisted sintering technology (fast)
EP4105444A1 (en) * 2021-06-18 2022-12-21 Raytheon Technologies Corporation Joining individual turbine vanes with field assisted sintering technology (fast)
FR3137120A1 (en) * 2022-06-22 2023-12-29 Safran Aircraft Engines Bladed turbomachine assembly comprising means of limiting vibrations between platforms

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE485833C (en) * 1929-11-08 J A Maffei A G Process for the production of blades for turbo machines, in particular for steam or gas turbines
US2801076A (en) * 1952-11-18 1957-07-30 Parsons & Marine Eng Turbine Turbine nozzles
GB918692A (en) * 1958-07-11 1963-02-13 Ass Elect Ind Improvements relating to turbine nozzle blocks
EP0654586A1 (en) * 1993-11-19 1995-05-24 United Technologies Corporation Stator vane assembly

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3442442A (en) * 1966-12-02 1969-05-06 Gen Electric Mounting of blades in an axial flow compressor
CH488928A (en) * 1968-03-22 1970-04-15 Sulzer Ag Guide vane fastening in turbo machines
US4832568A (en) * 1982-02-26 1989-05-23 General Electric Company Turbomachine airfoil mounting assembly
US5848874A (en) * 1997-05-13 1998-12-15 United Technologies Corporation Gas turbine stator vane assembly

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE485833C (en) * 1929-11-08 J A Maffei A G Process for the production of blades for turbo machines, in particular for steam or gas turbines
US2801076A (en) * 1952-11-18 1957-07-30 Parsons & Marine Eng Turbine Turbine nozzles
GB918692A (en) * 1958-07-11 1963-02-13 Ass Elect Ind Improvements relating to turbine nozzle blocks
EP0654586A1 (en) * 1993-11-19 1995-05-24 United Technologies Corporation Stator vane assembly

Also Published As

Publication number Publication date
US6217282B1 (en) 2001-04-17
DE59807705D1 (en) 2003-05-08
DE29715180U1 (en) 1997-10-16
EP0899426B1 (en) 2003-04-02
EP0899426A2 (en) 1999-03-03
JPH11107704A (en) 1999-04-20

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