ES2345303T3 - Junta de rendija para alabes de una turbomaquina. - Google Patents

Junta de rendija para alabes de una turbomaquina. Download PDF

Info

Publication number
ES2345303T3
ES2345303T3 ES08153316T ES08153316T ES2345303T3 ES 2345303 T3 ES2345303 T3 ES 2345303T3 ES 08153316 T ES08153316 T ES 08153316T ES 08153316 T ES08153316 T ES 08153316T ES 2345303 T3 ES2345303 T3 ES 2345303T3
Authority
ES
Spain
Prior art keywords
slit
blade
longitudinal
blades
groove
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.)
Active
Application number
ES08153316T
Other languages
English (en)
Spanish (es)
Inventor
Thomas Heinz-Schwarzmaier
Sven Olmes
Ronald Wifling
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.)
GE Vernova GmbH
Original Assignee
Alstom Technology 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 Alstom Technology AG filed Critical Alstom Technology AG
Application granted granted Critical
Publication of ES2345303T3 publication Critical patent/ES2345303T3/es
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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
    • F01D11/00—Preventing or minimising internal leakage of working-fluid, e.g. between stages
    • F01D11/005—Sealing means between non relatively rotating elements
    • F01D11/006—Sealing the gap between rotor blades or blades and rotor
    • F01D11/008—Sealing the gap between rotor blades or blades and rotor by spacer elements between the blades, e.g. independent interblade platforms

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)
  • Sealing Using Fluids, Sealing Without Contact, And Removal Of Oil (AREA)
ES08153316T 2007-04-05 2008-03-26 Junta de rendija para alabes de una turbomaquina. Active ES2345303T3 (es)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
CH5732007 2007-04-05
CH57320/07 2007-04-05

Publications (1)

Publication Number Publication Date
ES2345303T3 true ES2345303T3 (es) 2010-09-20

Family

ID=38457915

Family Applications (1)

Application Number Title Priority Date Filing Date
ES08153316T Active ES2345303T3 (es) 2007-04-05 2008-03-26 Junta de rendija para alabes de una turbomaquina.

Country Status (6)

Country Link
US (1) US8043050B2 (cg-RX-API-DMAC10.html)
EP (1) EP1995413B1 (cg-RX-API-DMAC10.html)
JP (1) JP5094510B2 (cg-RX-API-DMAC10.html)
AT (1) ATE466169T1 (cg-RX-API-DMAC10.html)
DE (1) DE502008000588D1 (cg-RX-API-DMAC10.html)
ES (1) ES2345303T3 (cg-RX-API-DMAC10.html)

Families Citing this family (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP2213841B1 (en) * 2009-01-28 2011-12-14 Alstom Technology Ltd Strip seal and method for designing a strip seal
US20120045337A1 (en) * 2010-08-20 2012-02-23 Michael James Fedor Turbine bucket assembly and methods for assembling same
US8905716B2 (en) 2012-05-31 2014-12-09 United Technologies Corporation Ladder seal system for gas turbine engines
BE1022361B1 (fr) * 2014-11-06 2016-03-17 Techspace Aero Sa Stator mixte de compresseur de turbomachine axiale.
EP3438410B1 (en) 2017-08-01 2021-09-29 General Electric Company Sealing system for a rotary machine
EP3498980B1 (en) * 2017-12-15 2021-02-17 Ansaldo Energia Switzerland AG Shiplap seal arrangement
CN114233402B (zh) * 2020-09-09 2024-07-16 中国航发商用航空发动机有限责任公司 具有叶片缘板密封结构的静子叶片

Family Cites Families (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3981609A (en) * 1975-06-02 1976-09-21 United Technologies Corporation Coolable blade tip shroud
US3995971A (en) * 1975-06-02 1976-12-07 United Technologies Corporation Rotatable vane seal
US3970318A (en) * 1975-09-26 1976-07-20 General Electric Company Sealing means for a segmented ring
EP0103260A3 (en) * 1982-09-06 1984-09-26 Hitachi, Ltd. Clearance control for turbine blade tips
FR2552159B1 (fr) * 1983-09-21 1987-07-10 Snecma Dispositif de liaison et d'etancheite de secteurs d'aubes de stator de turbine
JPS60133103U (ja) * 1984-02-17 1985-09-05 株式会社日立製作所 シ−ル構造
EP0536575B1 (de) * 1991-10-08 1995-04-05 Asea Brown Boveri Ag Deckband für axialdurchströmte Turbine
EP0902167B1 (de) * 1997-09-15 2003-10-29 ALSTOM (Switzerland) Ltd Kühlvorrichtung für Gasturbinenkomponenten
JP3999395B2 (ja) * 1999-03-03 2007-10-31 三菱重工業株式会社 ガスタービン分割環
EP1163427B1 (de) * 1999-03-19 2003-12-10 Siemens Aktiengesellschaft Gasturbinenrotor mit innenraumgekühlter gasturbinenschaufel
JP2002201913A (ja) * 2001-01-09 2002-07-19 Mitsubishi Heavy Ind Ltd ガスタービンの分割壁およびシュラウド
JP4508482B2 (ja) 2001-07-11 2010-07-21 三菱重工業株式会社 ガスタービン静翼
US6910854B2 (en) * 2002-10-08 2005-06-28 United Technologies Corporation Leak resistant vane cluster
JP2005233141A (ja) * 2004-02-23 2005-09-02 Mitsubishi Heavy Ind Ltd 動翼およびその動翼を用いたガスタービン

Also Published As

Publication number Publication date
EP1995413B1 (de) 2010-04-28
JP5094510B2 (ja) 2012-12-12
US8043050B2 (en) 2011-10-25
US20080247867A1 (en) 2008-10-09
JP2008255989A (ja) 2008-10-23
EP1995413A1 (de) 2008-11-26
DE502008000588D1 (de) 2010-06-10
ATE466169T1 (de) 2010-05-15

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