RU2005124856A - Изделие и компрессор, содержащий крыльчатку турбокомпрессора, имеющую множество изделий (варианты) - Google Patents

Изделие и компрессор, содержащий крыльчатку турбокомпрессора, имеющую множество изделий (варианты) Download PDF

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Publication number
RU2005124856A
RU2005124856A RU2005124856/06A RU2005124856A RU2005124856A RU 2005124856 A RU2005124856 A RU 2005124856A RU 2005124856/06 A RU2005124856/06 A RU 2005124856/06A RU 2005124856 A RU2005124856 A RU 2005124856A RU 2005124856 A RU2005124856 A RU 2005124856A
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RU
Russia
Prior art keywords
product
aerodynamic surface
compressor
inches
profile
Prior art date
Application number
RU2005124856/06A
Other languages
English (en)
Russian (ru)
Inventor
Стивен Эрик ТОМБЕРГ (US)
Стивен Эрик ТОМБЕРГ
Роджер БЕХАРРИСИНГХ (US)
Роджер БЕХАРРИСИНГХ
Тимоти Э. ДЕДЖОРИС (US)
Тимоти Э. ДЕДЖОРИС
Уилль м Дж. МИЛЛЕР (US)
Уилльям Дж. МИЛЛЕР
Поль ДЕВЕРНУА (US)
Поль ДЕВЕРНУА
Венката Сива П. ЧАЛУВАДИ (US)
Венката Сива П. ЧАЛУВАДИ
Адриан Микр МИСТРЯНУ (US)
Адриан Микря МИСТРЯНУ
Майкл Джеймс ДУТКА (US)
Майкл Джеймс ДУТКА
Натан С. РЭЙС (US)
Натан С. РЭЙС
Джеффри БОЙД (US)
Джеффри БОЙД
Кристофер Дэвид МАКГОУВАН (US)
Кристофер Дэвид МАКГОУВАН
Питер Гейнс КЛИВЛАНД (US)
Питер Гейнс КЛИВЛАНД
Джейсон Томас ХАРРЕЛЛ (US)
Джейсон Томас ХАРРЕЛЛ
Карл Г. ШОТТ (US)
Карл Г. ШОТТ
Джон Дэвид СТЭМПФЛИ (US)
Джон Дэвид СТЭМПФЛИ
Рональд Стюарт ДЕНМАК (US)
Рональд Стюарт ДЕНМАК
Стевен Марк ШИРЛЕ (US)
Стевен Марк ШИРЛЕ
Дженнифер Б. МИШЕНФЕЛЬДЕР (US)
Дженнифер Б. МИШЕНФЕЛЬДЕР
Джон Ф. РАЙМАН (US)
Джон Ф. РАЙМАН
Original Assignee
Дженерал Электрик Компани (US)
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 (US), Дженерал Электрик Компани filed Critical Дженерал Электрик Компани (US)
Publication of RU2005124856A publication Critical patent/RU2005124856A/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
    • F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/12—Blades
    • 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
    • F01D5/14—Form or construction
    • F01D5/141—Shape, i.e. outer, aerodynamic form
    • 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
    • F01D5/14—Form or construction
    • 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
    • F05D2240/20—Rotors
    • F05D2240/30—Characteristics of rotor blades, i.e. of any element transforming dynamic fluid energy to or from rotational energy and being attached to a rotor
    • F05D2240/301—Cross-sectional characteristics
    • 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
    • Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10S416/00—Fluid reaction surfaces, i.e. impellers
    • Y10S416/02—Formulas of curves
    • 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
    • Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10S416/00—Fluid reaction surfaces, i.e. impellers
    • Y10S416/05—Variable camber or chord length

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Materials For Photolithography (AREA)
  • Developing Agents For Electrophotography (AREA)
RU2005124856/06A 2004-08-05 2005-08-04 Изделие и компрессор, содержащий крыльчатку турбокомпрессора, имеющую множество изделий (варианты) RU2005124856A (ru)

Applications Claiming Priority (4)

Application Number Priority Date Filing Date Title
US91174204A 2004-08-05 2004-08-05
US10/911,742 2004-08-05
US10/986,162 2004-11-12
US10/986,162 US7186090B2 (en) 2004-08-05 2004-11-12 Air foil shape for a compressor blade

Publications (1)

Publication Number Publication Date
RU2005124856A true RU2005124856A (ru) 2007-02-10

Family

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Family Applications (1)

Application Number Title Priority Date Filing Date
RU2005124856/06A RU2005124856A (ru) 2004-08-05 2005-08-04 Изделие и компрессор, содержащий крыльчатку турбокомпрессора, имеющую множество изделий (варианты)

Country Status (5)

Country Link
US (1) US7186090B2 (enExample)
EP (1) EP1624158A2 (enExample)
JP (1) JP2006046347A (enExample)
KR (1) KR20060049282A (enExample)
RU (1) RU2005124856A (enExample)

Cited By (4)

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RU2614423C2 (ru) * 2012-06-19 2017-03-28 Дженерал Электрик Компани Лопатка компрессора, имеющая аэродинамическую часть заданного профиля, лопатка компрессора, имеющая аэродинамическую часть со стороной пониженного давления заданного профиля, и компрессор
RU2614554C2 (ru) * 2012-06-19 2017-03-28 Дженерал Электрик Компани Лопатка компрессора, имеющая аэродинамическую часть заданного профиля, лопатка компрессора, имеющая аэродинамическую часть со стороной пониженного давления заданного профиля, и компрессор
RU2644662C2 (ru) * 2012-07-24 2018-02-13 Дженерал Электрик Компани Рабочая лопатка турбомашины (варианты)
RU2672204C2 (ru) * 2013-05-14 2018-11-12 Ман Дизель Унд Турбо Се Рабочая лопатка компрессора и компрессор с такой рабочей лопаткой

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US6866477B2 (en) * 2003-07-31 2005-03-15 General Electric Company Airfoil shape for a turbine nozzle
US6857855B1 (en) * 2003-08-04 2005-02-22 General Electric Company Airfoil shape for a turbine bucket
US6881038B1 (en) * 2003-10-09 2005-04-19 General Electric Company Airfoil shape for a turbine bucket

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RU2614423C2 (ru) * 2012-06-19 2017-03-28 Дженерал Электрик Компани Лопатка компрессора, имеющая аэродинамическую часть заданного профиля, лопатка компрессора, имеющая аэродинамическую часть со стороной пониженного давления заданного профиля, и компрессор
RU2614554C2 (ru) * 2012-06-19 2017-03-28 Дженерал Электрик Компани Лопатка компрессора, имеющая аэродинамическую часть заданного профиля, лопатка компрессора, имеющая аэродинамическую часть со стороной пониженного давления заданного профиля, и компрессор
RU2644662C2 (ru) * 2012-07-24 2018-02-13 Дженерал Электрик Компани Рабочая лопатка турбомашины (варианты)
RU2672204C2 (ru) * 2013-05-14 2018-11-12 Ман Дизель Унд Турбо Се Рабочая лопатка компрессора и компрессор с такой рабочей лопаткой

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US20060073014A1 (en) 2006-04-06
US7186090B2 (en) 2007-03-06
KR20060049282A (ko) 2006-05-18
JP2006046347A (ja) 2006-02-16

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