DE69734558T2 - Gasturbine und Rotorabdichtung um dem Rotor ein Kühlmedium zuzuführen - Google Patents

Gasturbine und Rotorabdichtung um dem Rotor ein Kühlmedium zuzuführen Download PDF

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Publication number
DE69734558T2
DE69734558T2 DE69734558T DE69734558T DE69734558T2 DE 69734558 T2 DE69734558 T2 DE 69734558T2 DE 69734558 T DE69734558 T DE 69734558T DE 69734558 T DE69734558 T DE 69734558T DE 69734558 T2 DE69734558 T2 DE 69734558T2
Authority
DE
Germany
Prior art keywords
rotor
cooling medium
guide ring
steam
around
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
DE69734558T
Other languages
German (de)
English (en)
Other versions
DE69734558D1 (de
Inventor
Clement Schenectady Gazzillo
Steven John Ballston Spa Croft
San-dar Schenectady Gau
Denise Marie Ballston Lake Parent
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
Publication of DE69734558D1 publication Critical patent/DE69734558D1/de
Application granted granted Critical
Publication of DE69734558T2 publication Critical patent/DE69734558T2/de
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/12—Cooling of plants
    • F02C7/16—Cooling of plants characterised by cooling medium
    • F02C7/18—Cooling of plants characterised by cooling medium the medium being gaseous, e.g. air
    • 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
    • F01D11/02—Preventing or minimising internal leakage of working-fluid, e.g. between stages by non-contact sealings, e.g. of labyrinth type
    • F01D11/04—Preventing or minimising internal leakage of working-fluid, e.g. between stages by non-contact sealings, e.g. of labyrinth type using sealing fluid, e.g. steam
    • 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
    • F01D5/085—Heating, heat-insulating or cooling means cooling fluid circulating inside the 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
    • F01D9/00—Stators
    • F01D9/02—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
    • F01D9/026—Scrolls for radial machines or engines
    • 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
    • F05D2260/00—Function
    • F05D2260/20—Heat transfer, e.g. cooling
    • F05D2260/205—Cooling fluid recirculation, i.e. after cooling one or more components is the cooling fluid recovered and used elsewhere for other purposes
    • 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
    • F05D2260/00—Function
    • F05D2260/20—Heat transfer, e.g. cooling
    • F05D2260/232—Heat transfer, e.g. cooling characterized by the cooling medium
    • F05D2260/2322—Heat transfer, e.g. cooling characterized by the cooling medium steam

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
DE69734558T 1996-11-12 1997-07-11 Gasturbine und Rotorabdichtung um dem Rotor ein Kühlmedium zuzuführen Expired - Lifetime DE69734558T2 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US745542 1996-11-12
US08/745,542 US5738488A (en) 1996-11-12 1996-11-12 Gland for transferring cooling medium to the rotor of a gas turbine

Publications (2)

Publication Number Publication Date
DE69734558D1 DE69734558D1 (de) 2005-12-15
DE69734558T2 true DE69734558T2 (de) 2006-07-27

Family

ID=24997126

Family Applications (1)

Application Number Title Priority Date Filing Date
DE69734558T Expired - Lifetime DE69734558T2 (de) 1996-11-12 1997-07-11 Gasturbine und Rotorabdichtung um dem Rotor ein Kühlmedium zuzuführen

Country Status (5)

Country Link
US (1) US5738488A (enExample)
EP (1) EP0841471B1 (enExample)
JP (1) JP4090091B2 (enExample)
KR (1) KR19980041781A (enExample)
DE (1) DE69734558T2 (enExample)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102009025805B4 (de) * 2008-05-16 2021-02-04 General Electric Co. Kühlkreislauf zur Verwendung bei der Turbinenschaufelkühlung

Families Citing this family (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP3567065B2 (ja) * 1997-07-31 2004-09-15 株式会社東芝 ガスタービン
JP4308388B2 (ja) * 1998-12-18 2009-08-05 ゼネラル・エレクトリック・カンパニイ タービンロータを蒸気冷却するためのボアチューブアセンブリ
JP4527824B2 (ja) * 1998-12-22 2010-08-18 ゼネラル・エレクトリック・カンパニイ タービンロータの軸受用冷却系
KR20000071290A (ko) * 1999-01-29 2000-11-25 제이 엘. 차스킨, 버나드 스나이더, 아더엠. 킹 조합된 사이클 시스템 및 가스 터빈
US6827350B2 (en) * 2002-10-30 2004-12-07 General Electric Company Hybrid honeycomb and brush seal for steam gland
DE102005035540A1 (de) * 2005-07-29 2007-02-01 Mtu Aero Engines Gmbh Vorrichtung zur aktiven Spaltkontrolle für eine Strömungsmaschine
FR2907183B1 (fr) * 2006-10-11 2009-01-30 Snecma Sa Systeme d'etancheite entre deux arbres tournants coaxiaux
US8192151B2 (en) * 2009-04-29 2012-06-05 General Electric Company Turbine engine having cooling gland
US8388313B2 (en) * 2009-11-05 2013-03-05 General Electric Company Extraction cavity wing seal
US10378379B2 (en) 2015-08-27 2019-08-13 General Electric Company Gas turbine engine cooling air manifolds with spoolies
CN109404057B (zh) * 2018-10-24 2021-09-07 中国船舶重工集团公司第七0五研究所 一种应用于热电涡轮机的迷宫密封水路冷却装置及方法

Family Cites Families (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2788951A (en) * 1951-02-15 1957-04-16 Power Jets Res & Dev Ltd Cooling of turbine rotors
US2778601A (en) * 1951-05-28 1957-01-22 Ernst R G Eckert Fluid cooled turbine blade construction
CH443821A (de) * 1966-01-14 1967-09-15 Escher Wyss Ag Vorrichtung zur Abdichtung der Welle einer Turbomaschine für Wärmekraftanlagen, deren gasförmiges Arbeitsmittel in einem Atomkern-Reaktor erhitzt wird
CH487337A (de) * 1968-01-10 1970-03-15 Sulzer Ag Anordnung für den Durchtritt von Gas durch den Mantel eines hohlen Rotors
US3729930A (en) * 1970-06-23 1973-05-01 Rolls Royce Gas turbine engine
AU538118B2 (en) * 1979-10-29 1984-08-02 Rockwell International Inc. Seal assembly
JPS5951109A (ja) * 1982-09-17 1984-03-24 Hitachi Ltd 蒸気原動所の復水器真空保持装置
JP3142850B2 (ja) * 1989-03-13 2001-03-07 株式会社東芝 タービンの冷却翼および複合発電プラント
DE4433289A1 (de) * 1994-09-19 1996-03-21 Abb Management Ag Axialdurchströmte Gasturbine
US5599026A (en) * 1995-09-06 1997-02-04 Innovative Technology, L.L.C. Turbine seal with sealing strip and rubbing strip

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102009025805B4 (de) * 2008-05-16 2021-02-04 General Electric Co. Kühlkreislauf zur Verwendung bei der Turbinenschaufelkühlung

Also Published As

Publication number Publication date
EP0841471A3 (en) 1999-10-13
DE69734558D1 (de) 2005-12-15
KR19980041781A (ko) 1998-08-17
JPH10141004A (ja) 1998-05-26
EP0841471A2 (en) 1998-05-13
EP0841471B1 (en) 2005-11-09
JP4090091B2 (ja) 2008-05-28
US5738488A (en) 1998-04-14

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