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DE60134614D1 - Turbinendichtring und entsprechende Turbine - Google Patents

Turbinendichtring und entsprechende Turbine

Info

Publication number
DE60134614D1
DE60134614D1 DE60134614T DE60134614T DE60134614D1 DE 60134614 D1 DE60134614 D1 DE 60134614D1 DE 60134614 T DE60134614 T DE 60134614T DE 60134614 T DE60134614 T DE 60134614T DE 60134614 D1 DE60134614 D1 DE 60134614D1
Authority
DE
Germany
Prior art keywords
turbine
seal
turbine seal
corresponding turbine
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.)
Expired - Lifetime
Application number
DE60134614T
Other languages
English (en)
Inventor
Steven Milo Toborg
Dennis Eugene Moore
Richard William Albrecht
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.)
General Electric Co
Original Assignee
General Electric Co
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 General Electric Co filed Critical General Electric Co
Application granted granted Critical
Publication of DE60134614D1 publication Critical patent/DE60134614D1/de
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
    • F01D11/00—Preventing or minimising internal leakage of working-fluid, e.g. between stages
    • F01D11/001—Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between stator blade and rotor
    • 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
    • F01D5/02—Blade-carrying members, e.g. rotors
    • F01D5/08—Heating, heat-insulating or cooling means
    • F01D5/081—Cooling fluid being directed on the side of the rotor disc or at the roots of the blades
    • 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
    • F05D2240/00—Components
    • F05D2240/55—Seals
    • 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
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
DE60134614T 2000-12-04 2001-11-30 Turbinendichtring und entsprechende Turbine Expired - Lifetime DE60134614D1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US09/729,370 US6464453B2 (en) 2000-12-04 2000-12-04 Turbine interstage sealing ring

Publications (1)

Publication Number Publication Date
DE60134614D1 true DE60134614D1 (de) 2008-08-14

Family

ID=24930729

Family Applications (1)

Application Number Title Priority Date Filing Date
DE60134614T Expired - Lifetime DE60134614D1 (de) 2000-12-04 2001-11-30 Turbinendichtring und entsprechende Turbine

Country Status (6)

Country Link
US (1) US6464453B2 (de)
EP (1) EP1211386B1 (de)
JP (1) JP4108323B2 (de)
BR (1) BR0105891B1 (de)
CA (1) CA2363669C (de)
DE (1) DE60134614D1 (de)

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US6939106B2 (en) * 2002-12-11 2005-09-06 General Electric Company Sealing of steam turbine nozzle hook leakages using a braided rope seal
US6832892B2 (en) * 2002-12-11 2004-12-21 General Electric Company Sealing of steam turbine bucket hook leakages using a braided rope seal
US6899520B2 (en) * 2003-09-02 2005-05-31 General Electric Company Methods and apparatus to reduce seal rubbing within gas turbine engines
US7001145B2 (en) * 2003-11-20 2006-02-21 General Electric Company Seal assembly for turbine, bucket/turbine including same, method for sealing interface between rotating and stationary components of a turbine
JP2006097585A (ja) * 2004-09-29 2006-04-13 Mitsubishi Heavy Ind Ltd エアセパレータの取付構造及びそれを備えたガスタービン
GB2420155B (en) * 2004-11-12 2008-08-27 Rolls Royce Plc Turbine blade cooling system
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US7836593B2 (en) 2005-03-17 2010-11-23 Siemens Energy, Inc. Cold spray method for producing gas turbine blade tip
US7520718B2 (en) * 2005-07-18 2009-04-21 Siemens Energy, Inc. Seal and locking plate for turbine rotor assembly between turbine blade and turbine vane
FR2889249B1 (fr) * 2005-07-29 2007-10-19 Snecma Montage d'un support de joint a labyrinthe sur un rotor de turbomachine
CA2619730A1 (en) * 2005-08-23 2007-03-01 Alstom Technology Ltd Locking and fixing device for a heat shield element for a rotor unit of a turbomachine
US7331763B2 (en) * 2005-12-20 2008-02-19 General Electric Company Turbine disk
GB0603030D0 (en) 2006-02-15 2006-03-29 Rolls Royce Plc Gas turbine engine rotor ventilation arrangement
US7722314B2 (en) * 2006-06-22 2010-05-25 General Electric Company Methods and systems for assembling a turbine
JP5036240B2 (ja) * 2006-07-21 2012-09-26 株式会社リコー 帯電ローラ軸受部材、プロセスカートリッジ及び画像形成装置
JP4616869B2 (ja) * 2007-08-24 2011-01-19 三菱重工業株式会社 ガスタービン
US8128349B2 (en) * 2007-10-17 2012-03-06 United Technologies Corp. Gas turbine engines and related systems involving blade outer air seals
US8469656B1 (en) 2008-01-15 2013-06-25 Siemens Energy, Inc. Airfoil seal system for gas turbine engine
US8534993B2 (en) 2008-02-13 2013-09-17 United Technologies Corp. Gas turbine engines and related systems involving blade outer air seals
US8221083B2 (en) * 2008-04-15 2012-07-17 United Technologies Corporation Asymmetrical rotor blade fir-tree attachment
JP2010077868A (ja) * 2008-09-25 2010-04-08 Mitsubishi Heavy Ind Ltd ガスタービンのリムシール構造
US8137067B2 (en) * 2008-11-05 2012-03-20 General Electric Company Turbine with interrupted purge flow
US8221062B2 (en) * 2009-01-14 2012-07-17 General Electric Company Device and system for reducing secondary air flow in a gas turbine
US8235656B2 (en) * 2009-02-13 2012-08-07 General Electric Company Catenary turbine seal systems
US8177495B2 (en) * 2009-03-24 2012-05-15 General Electric Company Method and apparatus for turbine interstage seal ring
US8348603B2 (en) * 2009-04-02 2013-01-08 General Electric Company Gas turbine inner flowpath coverpiece
GB2477736B (en) * 2010-02-10 2014-04-09 Rolls Royce Plc A seal arrangement
DE102010015211B4 (de) * 2010-04-16 2013-06-20 Mtu Aero Engines Gmbh Dämpfungselement zur Dämpfung von Laufschaufelschwingungen, Laufschaufel sowie Rotor
US8845284B2 (en) 2010-07-02 2014-09-30 General Electric Company Apparatus and system for sealing a turbine rotor
US9145771B2 (en) 2010-07-28 2015-09-29 United Technologies Corporation Rotor assembly disk spacer for a gas turbine engine
US8534673B2 (en) * 2010-08-20 2013-09-17 Mitsubishi Power Systems Americas, Inc. Inter stage seal housing having a replaceable wear strip
US8608436B2 (en) * 2010-08-31 2013-12-17 General Electric Company Tapered collet connection of rotor components
US20120067054A1 (en) 2010-09-21 2012-03-22 Palmer Labs, Llc High efficiency power production methods, assemblies, and systems
US9022727B2 (en) * 2010-11-15 2015-05-05 Mtu Aero Engines Gmbh Rotor for a turbo machine
US9200527B2 (en) 2011-01-04 2015-12-01 General Electric Company Systems, methods, and apparatus for a turbine interstage rim seal
US9074609B2 (en) * 2011-02-15 2015-07-07 Siemens Energy, Inc. Gas turbine engine
FR2973829B1 (fr) * 2011-04-05 2013-05-24 Snecma Flasque d'etancheite pour etage de turbine de turbomachine d'aeronef, comprenant
US20130025290A1 (en) * 2011-07-29 2013-01-31 United Technologies Corporation Ingestion-tolerant low leakage low pressure turbine
US8864453B2 (en) 2012-01-20 2014-10-21 General Electric Company Near flow path seal for a turbomachine
US9080456B2 (en) * 2012-01-20 2015-07-14 General Electric Company Near flow path seal with axially flexible arms
US9091173B2 (en) * 2012-05-31 2015-07-28 United Technologies Corporation Turbine coolant supply system
US10094389B2 (en) * 2012-12-29 2018-10-09 United Technologies Corporation Flow diverter to redirect secondary flow
US10344603B2 (en) 2013-07-30 2019-07-09 United Technologies Corporation Gas turbine engine turbine vane ring arrangement
FR3011032B1 (fr) * 2013-09-25 2017-12-29 Snecma Ensemble rotatif pour turbomachine
RU2536652C1 (ru) * 2013-10-04 2014-12-27 Открытое акционерное общество "Авиадвигатель" Ротор турбины низкого давления
US9404376B2 (en) * 2013-10-28 2016-08-02 General Electric Company Sealing component for reducing secondary airflow in a turbine system
US9719363B2 (en) * 2014-06-06 2017-08-01 United Technologies Corporation Segmented rim seal spacer for a gas turbine engine
FR3022944B1 (fr) * 2014-06-26 2020-02-14 Safran Aircraft Engines Ensemble rotatif pour turbomachine
FR3026430B1 (fr) * 2014-09-29 2020-07-10 Safran Aircraft Engines Roue de turbine dans une turbomachine
US20170226861A1 (en) * 2014-10-15 2017-08-10 Safran Aircraft Engines Rotary assembly for a turbine engine comprising a self-supported rotor collar
US10125722B2 (en) 2015-02-13 2018-11-13 United Technologies Corporation Turbine engine with a turbo-compressor
US10337401B2 (en) 2015-02-13 2019-07-02 United Technologies Corporation Turbine engine with a turbo-compressor
US10100731B2 (en) * 2015-02-13 2018-10-16 United Technologies Corporation Turbine engine with a turbo-compressor
US12037926B2 (en) 2016-02-05 2024-07-16 Siemens Energy Global GmbH & Co. KG Rotor comprising a rotor component arranged between two rotor discs
CN106523037A (zh) * 2016-12-12 2017-03-22 中国燃气涡轮研究院 一种带高位预旋流路的涡轮挡板结构
US10539035B2 (en) 2017-06-29 2020-01-21 General Electric Company Compliant rotatable inter-stage turbine seal
KR102000360B1 (ko) * 2017-11-02 2019-07-15 두산중공업 주식회사 압축기 및 이를 포함하는 가스 터빈
US10704400B2 (en) * 2018-10-17 2020-07-07 Pratt & Whitney Canada Corp. Rotor assembly with rotor disc lip
CN109356662B (zh) * 2018-11-27 2021-06-18 中国航发沈阳黎明航空发动机有限责任公司 一种航空发动机低压涡轮转子装配的工艺方法
FR3092609B1 (fr) * 2019-02-12 2021-02-12 Safran Aircraft Engines Ensemble de turbine pour turbomachine d’aeronef a circuit de refroidissement de disque ameliore
GB2581964A (en) 2019-03-04 2020-09-09 Rolls Royce Plc A turbomachine for a gas turbine engine
KR102127429B1 (ko) * 2019-06-05 2020-06-26 두산중공업 주식회사 터빈 로터 디스크와 인터스테이지 디스크 사이의 실링 구조
CN112129476B (zh) * 2019-06-24 2022-08-02 中国航发商用航空发动机有限责任公司 级间封严盘试验夹具
FR3101374B1 (fr) * 2019-09-30 2021-09-17 Safran Aircraft Engines Structure de refroidissement d’une turbine avec coopération radiale entre anneau d’étanchéité et disque de roue mobile
JP7394979B2 (ja) * 2019-10-18 2023-12-08 シーメンス エナジー グローバル ゲゼルシャフト ミット ベシュレンクテル ハフツング ウント コンパニー コマンディートゲゼルシャフト ２つのロータディスクの間に配置されたロータコンポーネントを有するロータ
FR3108661B1 (fr) * 2020-03-25 2022-09-02 Safran Aircraft Engines Couronne d’injecteurs de turbine
CN114607468B (zh) * 2020-12-09 2024-08-02 中国航发商用航空发动机有限责任公司 冷却气供给结构、冷却方法、涡轮以及燃气涡轮发动机
FR3126022A1 (fr) * 2021-08-05 2023-02-10 Safran Aircraft Engines Ensemble pour turbomachine d’aeronef comprenant une anneau de recouvrement pour l’isolement d’organes de fixation mecanique vis-a-vis d’un flux d’air
CN114973902B (zh) * 2022-04-14 2023-06-23 西北工业大学 一种教学用航空发动机低压涡轮模型及装配方法
GB202315091D0 (en) * 2023-10-02 2023-11-15 Rolls Royce Plc Gas turbine engine

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FR2744761B1 (fr) * 1996-02-08 1998-03-13 Snecma Disque labyrinthe avec raidisseur incorpore pour rotor de turbomachine
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Also Published As

Publication number Publication date
BR0105891A (pt) 2002-08-13
EP1211386A3 (de) 2004-01-21
US20020067987A1 (en) 2002-06-06
BR0105891B1 (pt) 2011-12-27
EP1211386A2 (de) 2002-06-05
US6464453B2 (en) 2002-10-15
EP1211386B1 (de) 2008-07-02
JP4108323B2 (ja) 2008-06-25
CA2363669C (en) 2008-06-17
JP2002201915A (ja) 2002-07-19
CA2363669A1 (en) 2002-06-04

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Legal Events

Date Code Title Description
8364 No opposition during term of opposition