BR112015010425A2 - aparelhos de invólucro de turbina para um motor de turbina a gás - Google Patents

aparelhos de invólucro de turbina para um motor de turbina a gás

Info

Publication number
BR112015010425A2
BR112015010425A2 BR112015010425A BR112015010425A BR112015010425A2 BR 112015010425 A2 BR112015010425 A2 BR 112015010425A2 BR 112015010425 A BR112015010425 A BR 112015010425A BR 112015010425 A BR112015010425 A BR 112015010425A BR 112015010425 A2 BR112015010425 A2 BR 112015010425A2
Authority
BR
Brazil
Prior art keywords
casing apparatus
gas turbine
turbine
turbine engine
engine
Prior art date
Application number
BR112015010425A
Other languages
English (en)
Inventor
Charles Albers Joseph
Lee Shelton Monty
Russo Richard Jr
Proctor Robert
Original Assignee
Gen Electric
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 Gen Electric filed Critical Gen Electric
Publication of BR112015010425A2 publication Critical patent/BR112015010425A2/pt

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
    • F01D25/28—Supporting or mounting arrangements, e.g. for turbine casing
    • 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
    • F01D11/08—Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between rotor blade tips and stator
    • F01D11/12—Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between rotor blade tips and stator using a rubstrip, e.g. erodible. deformable or resiliently-biased part
    • F01D11/122—Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between rotor blade tips and stator using a rubstrip, e.g. erodible. deformable or resiliently-biased part with erodable or abradable material
    • 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
    • F01D11/08—Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between rotor blade tips and stator
    • F01D11/12—Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between rotor blade tips and stator using a rubstrip, e.g. erodible. deformable or resiliently-biased part
    • F01D11/127—Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between rotor blade tips and stator using a rubstrip, e.g. erodible. deformable or resiliently-biased part with a deformable or crushable structure, e.g. honeycomb
    • 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
    • F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/12—Blades
    • 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
    • F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/12—Blades
    • F01D5/22—Blade-to-blade connections, e.g. for damping vibrations
    • F01D5/225—Blade-to-blade connections, e.g. for damping vibrations by shrouding

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
BR112015010425A 2012-11-21 2013-10-15 aparelhos de invólucro de turbina para um motor de turbina a gás BR112015010425A2 (pt)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US13/683,813 US9238977B2 (en) 2012-11-21 2012-11-21 Turbine shroud mounting and sealing arrangement
PCT/US2013/064916 WO2014081517A1 (en) 2012-11-21 2013-10-15 Turbine shroud mounting and sealing arrangement

Publications (1)

Publication Number Publication Date
BR112015010425A2 true BR112015010425A2 (pt) 2018-04-10

Family

ID=49943492

Family Applications (1)

Application Number Title Priority Date Filing Date
BR112015010425A BR112015010425A2 (pt) 2012-11-21 2013-10-15 aparelhos de invólucro de turbina para um motor de turbina a gás

Country Status (7)

Country Link
US (1) US9238977B2 (pt)
EP (1) EP2923041A1 (pt)
JP (1) JP2015535565A (pt)
CN (1) CN104797784B (pt)
BR (1) BR112015010425A2 (pt)
CA (1) CA2891616A1 (pt)
WO (1) WO2014081517A1 (pt)

Families Citing this family (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP2696037B1 (de) * 2012-08-09 2017-03-01 MTU Aero Engines AG Abdichtung des Strömungskanals einer Strömungsmaschine
EP2961940B1 (en) 2013-02-28 2019-04-03 United Technologies Corporation Contoured blade outer air seal for a gas turbine engine
US20140271142A1 (en) 2013-03-14 2014-09-18 General Electric Company Turbine Shroud with Spline Seal
JP6233578B2 (ja) * 2013-12-05 2017-11-22 株式会社Ihi タービン
EP3228826B1 (de) * 2016-04-05 2021-03-17 MTU Aero Engines GmbH Dichtungssegmentanordnung mit steckverbindung, zugehörige gasturbine und herstellungsverfahren
US20180340437A1 (en) * 2017-02-24 2018-11-29 General Electric Company Spline for a turbine engine
US10648362B2 (en) * 2017-02-24 2020-05-12 General Electric Company Spline for a turbine engine
US10655495B2 (en) * 2017-02-24 2020-05-19 General Electric Company Spline for a turbine engine
US20180355754A1 (en) * 2017-02-24 2018-12-13 General Electric Company Spline for a turbine engine
US20180347399A1 (en) * 2017-06-01 2018-12-06 Pratt & Whitney Canada Corp. Turbine shroud with integrated heat shield
US10519790B2 (en) * 2017-06-15 2019-12-31 General Electric Company Turbine shroud assembly
FR3071273B1 (fr) * 2017-09-21 2019-08-30 Safran Aircraft Engines Ensemble d'etancheite de turbine pour turbomachine
US10982559B2 (en) * 2018-08-24 2021-04-20 General Electric Company Spline seal with cooling features for turbine engines
US20200141276A1 (en) * 2018-11-07 2020-05-07 General Electric Company Turbine shroud with lapped seal segments
FR3096723B1 (fr) * 2019-05-29 2022-03-25 Safran Helicopter Engines Anneau d’etancheite pour une roue de turbine de turbomachine
FR3100838B1 (fr) * 2019-09-13 2021-10-01 Safran Aircraft Engines Anneau d’etancheite de turbomachine
US11608752B2 (en) 2021-02-22 2023-03-21 General Electric Company Sealing apparatus for an axial flow turbomachine
CN115263808B (zh) * 2022-09-28 2023-02-21 中国航发四川燃气涡轮研究院 集成式双转子航空发动机的中介机匣

Family Cites Families (26)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2081817B (en) 1980-08-08 1984-02-15 Rolls Royce Turbine blade shrouding
US4512712A (en) 1983-08-01 1985-04-23 United Technologies Corporation Turbine stator assembly
GB2206651B (en) 1987-07-01 1991-05-08 Rolls Royce Plc Turbine blade shroud structure
GB2249356B (en) 1990-11-01 1995-01-18 Rolls Royce Plc Shroud liners
US5188507A (en) * 1991-11-27 1993-02-23 General Electric Company Low-pressure turbine shroud
US5232340A (en) 1992-09-28 1993-08-03 General Electric Company Gas turbine engine stator assembly
US5927942A (en) 1993-10-27 1999-07-27 United Technologies Corporation Mounting and sealing arrangement for a turbine shroud segment
US5738490A (en) 1996-05-20 1998-04-14 Pratt & Whitney Canada, Inc. Gas turbine engine shroud seals
EP0844369B1 (en) 1996-11-23 2002-01-30 ROLLS-ROYCE plc A bladed rotor and surround assembly
US6120242A (en) 1998-11-13 2000-09-19 General Electric Company Blade containing turbine shroud
US6341938B1 (en) 2000-03-10 2002-01-29 General Electric Company Methods and apparatus for minimizing thermal gradients within turbine shrouds
US6340285B1 (en) 2000-06-08 2002-01-22 General Electric Company End rail cooling for combined high and low pressure turbine shroud
US6902371B2 (en) * 2002-07-26 2005-06-07 General Electric Company Internal low pressure turbine case cooling
US6814538B2 (en) 2003-01-22 2004-11-09 General Electric Company Turbine stage one shroud configuration and method for service enhancement
JP4285134B2 (ja) 2003-07-04 2009-06-24 株式会社Ｉｈｉ シュラウドセグメント
JP4269829B2 (ja) * 2003-07-04 2009-05-27 株式会社Ｉｈｉ シュラウドセグメント
US7186078B2 (en) 2003-07-04 2007-03-06 Ishikawajima-Harima Heavy Industries Co., Ltd. Turbine shroud segment
US7147429B2 (en) 2004-09-16 2006-12-12 General Electric Company Turbine assembly and turbine shroud therefor
US7377742B2 (en) 2005-10-14 2008-05-27 General Electric Company Turbine shroud assembly and method for assembling a gas turbine engine
FR2899275A1 (fr) * 2006-03-30 2007-10-05 Snecma Sa Dispositif de fixation de secteurs d'anneau sur un carter de turbine d'une turbomachine
US7527477B2 (en) 2006-07-31 2009-05-05 General Electric Company Rotor blade and method of fabricating same
US8240985B2 (en) 2008-04-29 2012-08-14 Pratt & Whitney Canada Corp. Shroud segment arrangement for gas turbine engines
JP5384983B2 (ja) 2009-03-27 2014-01-08 本田技研工業株式会社 タービンシュラウド
US8740552B2 (en) 2010-05-28 2014-06-03 General Electric Company Low-ductility turbine shroud and mounting apparatus
JP5653656B2 (ja) * 2010-06-02 2015-01-14 三菱重工業株式会社 ハニカム部材の温度推定方法及びハニカム部材
US8753073B2 (en) 2010-06-23 2014-06-17 General Electric Company Turbine shroud sealing apparatus

Also Published As

Publication number Publication date
WO2014081517A1 (en) 2014-05-30
US20140140833A1 (en) 2014-05-22
JP2015535565A (ja) 2015-12-14
CA2891616A1 (en) 2014-05-30
CN104797784A (zh) 2015-07-22
EP2923041A1 (en) 2015-09-30
CN104797784B (zh) 2016-09-14
US9238977B2 (en) 2016-01-19

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Legal Events

Date Code Title Description
B08F Application dismissed because of non-payment of annual fees [chapter 8.6 patent gazette]

Free format text: REFERENTE A 5A ANUIDADE.

B08K Patent lapsed as no evidence of payment of the annual fee has been furnished to inpi [chapter 8.11 patent gazette]

Free format text: REFERENTE AO ARQUIVAMENTO PUBLICADO NA RPI 2492 DE 09/10/2018.