RU2312224C2 - Газовая турбина (варианты) - Google Patents

Газовая турбина (варианты) Download PDF

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Publication number
RU2312224C2
RU2312224C2 RU2003114120/06A RU2003114120A RU2312224C2 RU 2312224 C2 RU2312224 C2 RU 2312224C2 RU 2003114120/06 A RU2003114120/06 A RU 2003114120/06A RU 2003114120 A RU2003114120 A RU 2003114120A RU 2312224 C2 RU2312224 C2 RU 2312224C2
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RU
Russia
Prior art keywords
brace
parts
gas turbine
shroud
ceramic
Prior art date
Application number
RU2003114120/06A
Other languages
English (en)
Russian (ru)
Other versions
RU2003114120A (ru
Inventor
Эдвард Ли МАКГРЭТ (US)
Эдвард Ли МАКГРЭТ
Грегори С. КОРМЭН (US)
Грегори С. КОРМЭН
Энтони Дж. ДИН (US)
Энтони Дж. ДИН
Марк Стюарт ШРЕДЕР (US)
Марк Стюарт ШРЕДЕР
Крис Бэйзил ДЖИОМАКАС (US)
Крис Бэйзил ДЖИОМАКАС
Томас Реймонд ФЭРРЭЛЛ (US)
Томас Реймонд ФЭРРЭЛЛ
Кеннет Лоренцо ПАРКС (US)
Кеннет Лоренцо ПАРКС
Original Assignee
Дженерал Электрик Компани
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 Дженерал Электрик Компани filed Critical Дженерал Электрик Компани
Publication of RU2003114120A publication Critical patent/RU2003114120A/ru
Application granted granted Critical
Publication of RU2312224C2 publication Critical patent/RU2312224C2/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
    • 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
    • F01D5/28—Selecting particular materials; Particular measures relating thereto; Measures against erosion or corrosion
    • 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
    • F01D25/24—Casings; Casing parts, e.g. diaphragms, casing fastenings
    • F01D25/246—Fastening of diaphragms or stator-rings
    • 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
    • F05D2260/30—Retaining components in desired mutual position
    • 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)
  • Chemical & Material Sciences (AREA)
  • Materials Engineering (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Gasket Seals (AREA)
  • Inorganic Insulating Materials (AREA)
RU2003114120/06A 2002-05-15 2003-05-14 Газовая турбина (варианты) RU2312224C2 (ru)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US10/144,851 US6726448B2 (en) 2002-05-15 2002-05-15 Ceramic turbine shroud
US10/144,851 2002-05-15

Publications (2)

Publication Number Publication Date
RU2003114120A RU2003114120A (ru) 2004-11-10
RU2312224C2 true RU2312224C2 (ru) 2007-12-10

Family

ID=29269733

Family Applications (1)

Application Number Title Priority Date Filing Date
RU2003114120/06A RU2312224C2 (ru) 2002-05-15 2003-05-14 Газовая турбина (варианты)

Country Status (10)

Country Link
US (1) US6726448B2 (enExample)
EP (1) EP1362983B1 (enExample)
JP (1) JP4308574B2 (enExample)
KR (1) KR100776072B1 (enExample)
CN (1) CN100335752C (enExample)
AT (1) ATE437294T1 (enExample)
CZ (1) CZ302320B6 (enExample)
DE (1) DE60328432D1 (enExample)
ES (1) ES2327726T3 (enExample)
RU (1) RU2312224C2 (enExample)

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Also Published As

Publication number Publication date
US20030215328A1 (en) 2003-11-20
CZ302320B6 (cs) 2011-03-09
EP1362983A2 (en) 2003-11-19
DE60328432D1 (de) 2009-09-03
CN1458393A (zh) 2003-11-26
KR20030088878A (ko) 2003-11-20
JP2004003477A (ja) 2004-01-08
EP1362983B1 (en) 2009-07-22
CZ2003887A3 (cs) 2003-12-17
US6726448B2 (en) 2004-04-27
EP1362983A3 (en) 2007-12-05
ATE437294T1 (de) 2009-08-15
JP4308574B2 (ja) 2009-08-05
CN100335752C (zh) 2007-09-05
KR100776072B1 (ko) 2007-11-15
ES2327726T3 (es) 2009-11-03

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