RU2006142824A - Усовершенствованный направляющий сопловой аппарат газотурбинного двигателя - Google Patents

Усовершенствованный направляющий сопловой аппарат газотурбинного двигателя Download PDF

Info

Publication number
RU2006142824A
RU2006142824A RU2006142824/06A RU2006142824A RU2006142824A RU 2006142824 A RU2006142824 A RU 2006142824A RU 2006142824/06 A RU2006142824/06 A RU 2006142824/06A RU 2006142824 A RU2006142824 A RU 2006142824A RU 2006142824 A RU2006142824 A RU 2006142824A
Authority
RU
Russia
Prior art keywords
sector
nozzle apparatus
guide nozzle
flange
guiding nozzle
Prior art date
Application number
RU2006142824/06A
Other languages
English (en)
Russian (ru)
Inventor
Александр Николя ДЕРВО (FR)
Александр Николя ДЕРВО
Патрик Жозеф Мари ЖИРАР (FR)
Патрик Жозеф Мари ЖИРАР
Гаэль ЛОРО (FR)
Гаэль ЛОРО
Гийом Жан-Клод Робер РЕНОН (FR)
Гийом Жан-Клод Робер РЕНОН
Original Assignee
Снекма (Fr)
Снекма
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 Снекма (Fr), Снекма filed Critical Снекма (Fr)
Publication of RU2006142824A publication Critical patent/RU2006142824A/ru

Links

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
    • F01D11/001—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
    • 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
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
RU2006142824/06A 2005-12-05 2006-12-04 Усовершенствованный направляющий сопловой аппарат газотурбинного двигателя RU2006142824A (ru)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR0512295 2005-12-05
FR0512295A FR2894282A1 (fr) 2005-12-05 2005-12-05 Distributeur de turbine de turbomachine ameliore

Publications (1)

Publication Number Publication Date
RU2006142824A true RU2006142824A (ru) 2008-06-20

Family

ID=36950510

Family Applications (1)

Application Number Title Priority Date Filing Date
RU2006142824/06A RU2006142824A (ru) 2005-12-05 2006-12-04 Усовершенствованный направляющий сопловой аппарат газотурбинного двигателя

Country Status (8)

Country Link
US (1) US7780398B2 (OSRAM)
EP (1) EP1793093B1 (OSRAM)
JP (1) JP4794420B2 (OSRAM)
CN (1) CN1978870B (OSRAM)
CA (1) CA2569564C (OSRAM)
DE (1) DE602006012915D1 (OSRAM)
FR (1) FR2894282A1 (OSRAM)
RU (1) RU2006142824A (OSRAM)

Families Citing this family (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP5214128B2 (ja) * 2005-11-22 2013-06-19 シャープ株式会社 発光素子及び発光素子を備えたバックライトユニット
FR2928962B1 (fr) * 2008-03-19 2013-10-18 Snecma Distributeur de turbine a pales creuses.
EP2236761A1 (de) * 2009-04-02 2010-10-06 Siemens Aktiengesellschaft Leitschaufelträger
US8684683B2 (en) * 2010-11-30 2014-04-01 General Electric Company Gas turbine nozzle attachment scheme and removal/installation method
US8684689B2 (en) * 2011-01-14 2014-04-01 Hamilton Sundstrand Corporation Turbomachine shroud
FR2975771B1 (fr) * 2011-05-27 2014-03-14 Snecma Dispositif de mesure d'une piece dans une turbomachine
FR2979272B1 (fr) * 2011-08-24 2013-09-27 Snecma Outillage de prise de piece de turbomachine
US8888442B2 (en) 2012-01-30 2014-11-18 Pratt & Whitney Canada Corp. Stress relieving slots for turbine vane ring
US9291064B2 (en) 2012-01-31 2016-03-22 United Technologies Corporation Anti-icing core inlet stator assembly for a gas turbine engine
EP2706196A1 (en) 2012-09-07 2014-03-12 Siemens Aktiengesellschaft Turbine vane arrangement
WO2016068859A1 (en) * 2014-10-28 2016-05-06 Siemens Energy, Inc. Modular turbine vane
DE102016215784A1 (de) 2016-08-23 2018-03-01 MTU Aero Engines AG Positionierungselement mit Aussparungen für eine Leitschaufelanordnung
FR3084106B1 (fr) * 2018-07-23 2022-06-24 Safran Aircraft Engines Distributeur basse pression avec pales coulissantes
JP7284737B2 (ja) 2020-08-06 2023-05-31 三菱重工業株式会社 ガスタービン静翼
DE112021004251T5 (de) * 2020-08-13 2023-05-25 Mitsubishi Heavy Industries, Ltd. Statorschaufelsegment und damit versehene dampfturbine
US11519283B2 (en) * 2021-03-25 2022-12-06 Raytheon Technologies Corporation Attachment region for CMC components

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3781125A (en) * 1972-04-07 1973-12-25 Westinghouse Electric Corp Gas turbine nozzle vane structure
US4511306A (en) * 1982-02-02 1985-04-16 Westinghouse Electric Corp. Combustion turbine single airfoil stator vane structure
US5071313A (en) * 1990-01-16 1991-12-10 General Electric Company Rotor blade shroud segment
CA2070511C (en) * 1991-07-22 2001-08-21 Steven Milo Toborg Turbine nozzle support
US6210108B1 (en) * 1999-08-16 2001-04-03 General Electric Company Method for making an article portion subject to tensile stress and stress relieved article
FR2817285B1 (fr) * 2000-11-30 2003-06-13 Snecma Moteurs Virole interne de stator

Also Published As

Publication number Publication date
CA2569564C (fr) 2013-12-24
EP1793093B1 (fr) 2010-03-17
CN1978870B (zh) 2012-05-30
FR2894282A1 (fr) 2007-06-08
CN1978870A (zh) 2007-06-13
US7780398B2 (en) 2010-08-24
EP1793093A2 (fr) 2007-06-06
US20070128020A1 (en) 2007-06-07
CA2569564A1 (fr) 2007-06-05
JP2007154890A (ja) 2007-06-21
JP4794420B2 (ja) 2011-10-19
DE602006012915D1 (de) 2010-04-29
EP1793093A3 (fr) 2008-12-03

Similar Documents

Publication Publication Date Title
RU2006142824A (ru) Усовершенствованный направляющий сопловой аппарат газотурбинного двигателя
US8997351B2 (en) Non-metallic cover for a fixture
ATE437293T1 (de) Integral beschaufelter rotor
CA2566527C (en) Natural frequency tuning of gas turbine engine blades
BR0103410A (pt) Método e aparelho para reduzir a tensão na borda circunferencial do conjunto do rotor
US20070059157A1 (en) Fluid flow engine
RU2009115718A (ru) Направляющий аппарат турбомашины и направляющая лопатка для такого аппарата
US7731482B2 (en) Bucket vibration damper system
US9121283B2 (en) Assembly fixture with wedge clamps for stator vane assembly
DE602006008130D1 (de) Verschlussanordnung für turbinenschaufeln mit radialem einlass
EP1528224A3 (en) Method and apparatus for cooling gas turbine engine rotor blade
US20090304495A1 (en) Device for supplying ventilation air to the low pressure blades of a gas turbine engine
ATE548540T1 (de) Rotorstufe einer einteilig beschaufelten verdichtertrommel einer axialen strömungsmaschine und entsprechendes herstellungsverfahren.
RU2008120784A (ru) Устройство торможения турбины в газотурбинном двигателе в случае разрушения вала турбины и двухтактный газотурбинный двигатель
US20130084168A1 (en) Clearance flow control assembly having rail member
EP3812547A3 (en) Gas turbine engine rotor with blades having airfoil plugs for selected mistuning
KR970001851A (ko) 가동 블레이드 장착 장치 및 방법
WO2005059312A3 (de) Zentrierung der leitschaufelkränze in einer turbomaschine sowie montagevorrichtung
BR0200352A (pt) Conjunto de invólucro e método de usinagem do mesmo
RU2014118768A (ru) Лопатка статора турбомашины, содержащая выпуклый участок
FR2323007A1 (fr) Dispositif de refroidissement d'aube de turbine
US3521974A (en) Turbine blade construction
RU2011149631A (ru) Кольцо для статора турбинного двигателя летательного аппарата с прорезями снятия механической нагрузки лопаток
AU2001290458A1 (en) A method for manufacturing a vane to a gas turbine component and a method for manufacturing a gas turbine component
FI130754B1 (fi) Roottorin lapa ja tuuliturbiini

Legal Events

Date Code Title Description
FA92 Acknowledgement of application withdrawn (lack of supplementary materials submitted)

Effective date: 20090112