RU2392449C2 - Турбина, содержащая сменные носители истираемого уплотнения для создания уплотнения между вращающимся и стационарным компонентами турбины - Google Patents

Турбина, содержащая сменные носители истираемого уплотнения для создания уплотнения между вращающимся и стационарным компонентами турбины Download PDF

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Publication number
RU2392449C2
RU2392449C2 RU2005140142/06A RU2005140142A RU2392449C2 RU 2392449 C2 RU2392449 C2 RU 2392449C2 RU 2005140142/06 A RU2005140142/06 A RU 2005140142/06A RU 2005140142 A RU2005140142 A RU 2005140142A RU 2392449 C2 RU2392449 C2 RU 2392449C2
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RU
Russia
Prior art keywords
diaphragm
sealing
seal
sealing surface
turbine
Prior art date
Application number
RU2005140142/06A
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English (en)
Russian (ru)
Other versions
RU2005140142A (ru
Inventor
Роберт Джеймз БРАКЕН (US)
Роберт Джеймз БРАКЕН
Стерлинг Рей ХАТАУЭЙ (US)
Стерлинг Рей ХАТАУЭЙ
Дэвид Орус ФИТТС (US)
Дэвид Орус ФИТТС
Рон В. КОРЗУН (US)
Рон В. КОРЗУН
Лоренс Скотт ДАКЛОС (US)
Лоренс Скотт ДАКЛОС
Уилльям Эдвард ЭЙДИС (US)
Уилльям Эдвард ЭЙДИС
Марк Уилльям КОВАЛЬЧИК (US)
Марк Уилльям КОВАЛЬЧИК
Бернард Артур КУТЮР (US)
Бернард Артур КУТЮР
Original Assignee
ДЖЕНЕРАЛ ЭЛЕКТРИК КОМПАНИ (э Нью Йорк Корпорейшн)
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.)
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Publication of RU2005140142A publication Critical patent/RU2005140142A/ru
Application granted granted Critical
Publication of RU2392449C2 publication Critical patent/RU2392449C2/ru

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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
    • F01D11/08—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
    • F01D11/001—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
    • F01D5/12—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)
RU2005140142/06A 2004-12-22 2005-12-21 Турбина, содержащая сменные носители истираемого уплотнения для создания уплотнения между вращающимся и стационарным компонентами турбины RU2392449C2 (ru)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US11/017,661 2004-12-22
US11/017,661 US7287956B2 (en) 2004-12-22 2004-12-22 Removable abradable seal carriers for sealing between rotary and stationary turbine components

Publications (2)

Publication Number Publication Date
RU2005140142A RU2005140142A (ru) 2007-06-27
RU2392449C2 true RU2392449C2 (ru) 2010-06-20

Family

ID=36585717

Family Applications (1)

Application Number Title Priority Date Filing Date
RU2005140142/06A RU2392449C2 (ru) 2004-12-22 2005-12-21 Турбина, содержащая сменные носители истираемого уплотнения для создания уплотнения между вращающимся и стационарным компонентами турбины

Country Status (6)

Country Link
US (1) US7287956B2 (enExample)
JP (1) JP4740730B2 (enExample)
CN (1) CN1800589B (enExample)
FR (1) FR2879649B1 (enExample)
IT (1) ITMI20052424A1 (enExample)
RU (1) RU2392449C2 (enExample)

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JP5567077B2 (ja) * 2012-08-23 2014-08-06 三菱重工業株式会社 回転機械
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US10119410B2 (en) 2013-10-03 2018-11-06 United Technologies Corporation Vane seal system having spring positively locating seal member in axial direction
EP3489465B1 (en) 2013-10-03 2023-05-17 Raytheon Technologies Corporation Seal for a vane seal system and method for managing damping in a vane seal system
US9394801B2 (en) 2013-10-07 2016-07-19 General Electric Company Adjustable turbine seal and method of assembling same
US9429041B2 (en) 2014-05-14 2016-08-30 General Electric Company Turbomachine component displacement apparatus and method of use
FR3047075B1 (fr) * 2016-01-27 2018-02-23 Safran Aircraft Engines Piece de revolution pour banc d'essai de turbine ou pour turbomachine, banc d'essais de turbines comprenant ladite piece, et procede les utilisant
WO2016179608A2 (en) * 2016-04-29 2016-11-10 Stein Seal Company Intershaft seal with asymmetric sealing ring
US10598035B2 (en) * 2016-05-27 2020-03-24 General Electric Company Intershaft sealing systems for gas turbine engines and methods for assembling the same
FR3058755B1 (fr) * 2016-11-15 2020-09-25 Safran Aircraft Engines Turbine pour turbomachine
FR3058756B1 (fr) 2016-11-15 2020-10-16 Safran Aircraft Engines Turbine pour turbomachine
FR3068070B1 (fr) * 2017-06-26 2019-07-19 Safran Aircraft Engines Turbine pour turbomachine
JP7051656B2 (ja) * 2018-09-28 2022-04-11 三菱重工コンプレッサ株式会社 タービンステータ、蒸気タービン、及び仕切板
CN110761848A (zh) * 2019-12-16 2020-02-07 中国船舶重工集团公司第七0三研究所 一种燃气轮机压气机静叶环
CN112610335B (zh) * 2020-12-21 2021-12-31 杭州汽轮动力集团有限公司 一种燃气轮机涡轮盘腔密封结构
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Also Published As

Publication number Publication date
JP4740730B2 (ja) 2011-08-03
ITMI20052424A1 (it) 2006-06-23
RU2005140142A (ru) 2007-06-27
FR2879649A1 (fr) 2006-06-23
FR2879649B1 (fr) 2012-09-21
CN1800589B (zh) 2010-06-02
US7287956B2 (en) 2007-10-30
US20060133928A1 (en) 2006-06-22
CN1800589A (zh) 2006-07-12
JP2006177355A (ja) 2006-07-06

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