RU2614474C2 - Турбомашинный компонент, способ присоединения накладки к турбомашинному компоненту и турбомашинная установка - Google Patents

Турбомашинный компонент, способ присоединения накладки к турбомашинному компоненту и турбомашинная установка Download PDF

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Publication number
RU2614474C2
RU2614474C2 RU2012158306A RU2012158306A RU2614474C2 RU 2614474 C2 RU2614474 C2 RU 2614474C2 RU 2012158306 A RU2012158306 A RU 2012158306A RU 2012158306 A RU2012158306 A RU 2012158306A RU 2614474 C2 RU2614474 C2 RU 2614474C2
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RU
Russia
Prior art keywords
mounting element
mounting
specified
passage
turbomachine
Prior art date
Application number
RU2012158306A
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English (en)
Russian (ru)
Other versions
RU2012158306A (ru
Inventor
Аарон Грегори УИНН
Майкл Гордон ШЕРМАН
Ниранджан Гокулдас ПАЙ
Original Assignee
Дженерал Электрик Компани
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Application filed by Дженерал Электрик Компани filed Critical Дженерал Электрик Компани
Publication of RU2012158306A publication Critical patent/RU2012158306A/ru
Application granted granted Critical
Publication of RU2614474C2 publication Critical patent/RU2614474C2/ru

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    • 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
    • F01D9/04—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector
    • F01D9/042—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector fixing blades to stators
    • 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
    • F01D9/04—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector
    • F01D9/041—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector using blades
    • 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
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00—Metal working
    • Y10T29/49—Method of mechanical manufacture
    • Y10T29/49229—Prime mover or fluid pump making
    • Y10T29/49236—Fluid pump or compressor making

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
RU2012158306A 2012-01-09 2012-12-27 Турбомашинный компонент, способ присоединения накладки к турбомашинному компоненту и турбомашинная установка RU2614474C2 (ru)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US13/345,959 US9133724B2 (en) 2012-01-09 2012-01-09 Turbomachine component including a cover plate
US13/345,959 2012-01-09

Publications (2)

Publication Number Publication Date
RU2012158306A RU2012158306A (ru) 2014-07-10
RU2614474C2 true RU2614474C2 (ru) 2017-03-28

Family

ID=47678561

Family Applications (1)

Application Number Title Priority Date Filing Date
RU2012158306A RU2614474C2 (ru) 2012-01-09 2012-12-27 Турбомашинный компонент, способ присоединения накладки к турбомашинному компоненту и турбомашинная установка

Country Status (5)

Country Link
US (1) US9133724B2 (https=)
EP (1) EP2613005B1 (https=)
JP (1) JP6604600B2 (https=)
CN (1) CN103195516B (https=)
RU (1) RU2614474C2 (https=)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB201213109D0 (en) * 2012-07-24 2012-09-05 Rolls Royce Plc Seal segment
JP6209375B2 (ja) 2013-07-08 2017-10-04 株式会社日本マイクロニクス 電気的接続装置

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* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6382906B1 (en) * 2000-06-16 2002-05-07 General Electric Company Floating spoolie cup impingement baffle
RU2362886C2 (ru) * 2002-08-14 2009-07-27 Вольво Аэро Корпорейшн Способ изготовления компонента статора (варианты)
RU2347079C2 (ru) * 2003-03-06 2009-02-20 Снекма Мотёр Турбомашина с охлаждаемыми кольцевыми сегментами
US7534086B2 (en) * 2006-05-05 2009-05-19 Siemens Energy, Inc. Multi-layer ring seal

Also Published As

Publication number Publication date
CN103195516B (zh) 2017-03-01
JP6604600B2 (ja) 2019-11-13
EP2613005A1 (en) 2013-07-10
US20130177408A1 (en) 2013-07-11
JP2013142390A (ja) 2013-07-22
US9133724B2 (en) 2015-09-15
EP2613005B1 (en) 2015-11-04
RU2012158306A (ru) 2014-07-10
CN103195516A (zh) 2013-07-10

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