UA84846C2 - Лопатка турбины высокого давления турбомашины с окнами выпуска охлаждающего воздуха, формовочный элемент для изготовления лопатки, турбина высокого давления турбомашины и сопловой аппарат турбомашины - Google Patents

Лопатка турбины высокого давления турбомашины с окнами выпуска охлаждающего воздуха, формовочный элемент для изготовления лопатки, турбина высокого давления турбомашины и сопловой аппарат турбомашины

Info

Publication number
UA84846C2
UA84846C2 UAA200500303A UAA200500303A UA84846C2 UA 84846 C2 UA84846 C2 UA 84846C2 UA A200500303 A UAA200500303 A UA A200500303A UA A200500303 A UAA200500303 A UA A200500303A UA 84846 C2 UA84846 C2 UA 84846C2
Authority
UA
Ukraine
Prior art keywords
blade
turbo
machine
pressure turbine
wall
Prior art date
Application number
UAA200500303A
Other languages
English (en)
Ukrainian (uk)
Inventor
Жак Бурі
Моріс Жуде
Жакі Табарден
Original Assignee
Снекма Мотерс
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 Мотерс filed Critical Снекма Мотерс
Publication of UA84846C2 publication Critical patent/UA84846C2/ru

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B22—CASTING; POWDER METALLURGY
    • B22C—FOUNDRY MOULDING
    • B22C9/00—Moulds or cores; Moulding processes
    • B22C9/10—Cores; Manufacture or installation of cores
    • B22C9/103—Multipart cores
    • 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
    • F01D5/142—Shape, i.e. outer, aerodynamic form of the blades of successive rotor or stator blade-rows
    • F01D5/143—Contour of the outer or inner working fluid flow path wall, i.e. shroud or hub contour
    • 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
    • F01D5/18—Hollow blades, i.e. blades with cooling or heating channels or cavities; Heating, heat-insulating or cooling means on blades
    • F01D5/186—Film cooling
    • 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
    • F01D5/18—Hollow blades, i.e. blades with cooling or heating channels or cavities; Heating, heat-insulating or cooling means on blades
    • F01D5/187—Convection cooling
    • 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
    • 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
    • F05D2230/00—Manufacture
    • F05D2230/20—Manufacture essentially without removing material
    • F05D2230/21—Manufacture essentially without removing material by casting
    • 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
    • F05D2230/00—Manufacture
    • F05D2230/20—Manufacture essentially without removing material
    • F05D2230/21—Manufacture essentially without removing material by casting
    • F05D2230/211—Manufacture essentially without removing material by casting by precision casting, e.g. microfusing or investment casting
    • 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
    • F05D2240/10—Stators
    • F05D2240/12—Fluid guiding means, e.g. vanes
    • F05D2240/122—Fluid guiding means, e.g. vanes related to the trailing edge of a stator vane
    • 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
    • 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
    • F05D2240/304—Characteristics of rotor blades, i.e. of any element transforming dynamic fluid energy to or from rotational energy and being attached to a rotor related to the trailing edge of a rotor blade
    • 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
    • F05D2240/80—Platforms for stationary or moving blades

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)

Abstract

Лопатка турбины турбомашины содержит по меньшей мере одну нижнюю полку (24), соединенную с основой (16) лопатки нижней соединительной зоной (26), и контур охлаждения, который состоит из по меньшей мере одной полости и нескольких окон (30, 30а) выпуска воздуха, расположенных вдоль задней кромки (22) лопатки. Нижнее из этих окон, окно (30а) выпуска воздуха, расположено вблизи основы (16) лопатки. Это окно имеет боковую стенку (36), оборудованную отверстием (38), которое соединяется с полостью, углубленную стенку (32), нижнюю стенку (34), расположенную со стороны основы лопатки, нижний стык (40), образованный между углубленной стенкой (32) и нижней стенкой (34), и нижнее ребро (42), образованное между нижней стойкой и нижней соединительной зоной (26). Нижний стык (40) и нижнее ребро (42) нижнего окна (30а) выпуска воздуха имеют поперечные сечения, в сущности, закругленной формы, что исключает наличие между отверстием (38) окна и нижней соединительной зоной (26) каких-нибудь выступающих углов.
UAA200500303A 2004-01-14 2005-01-13 Лопатка турбины высокого давления турбомашины с окнами выпуска охлаждающего воздуха, формовочный элемент для изготовления лопатки, турбина высокого давления турбомашины и сопловой аппарат турбомашины UA84846C2 (ru)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0400289A FR2864990B1 (fr) 2004-01-14 2004-01-14 Perfectionnements apportes aux fentes d'evacuation de l'air de refroidissement d'aubes de turbine haute-pression

Publications (1)

Publication Number Publication Date
UA84846C2 true UA84846C2 (ru) 2008-12-10

Family

ID=34610765

Family Applications (1)

Application Number Title Priority Date Filing Date
UAA200500303A UA84846C2 (ru) 2004-01-14 2005-01-13 Лопатка турбины высокого давления турбомашины с окнами выпуска охлаждающего воздуха, формовочный элемент для изготовления лопатки, турбина высокого давления турбомашины и сопловой аппарат турбомашины

Country Status (9)

Country Link
US (1) US7278827B2 (ru)
EP (1) EP1555390B1 (ru)
JP (1) JP4619135B2 (ru)
CA (1) CA2493094C (ru)
DE (1) DE602004003331T2 (ru)
ES (1) ES2276254T3 (ru)
FR (1) FR2864990B1 (ru)
RU (1) RU2294438C2 (ru)
UA (1) UA84846C2 (ru)

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US7371048B2 (en) * 2005-05-27 2008-05-13 United Technologies Corporation Turbine blade trailing edge construction
FR2899269A1 (fr) * 2006-03-30 2007-10-05 Snecma Sa Aube de redresseur optimisee, secteur de redresseurs, etage de compression, compresseur et turbomachine comportant une telle aube
FR2899270A1 (fr) * 2006-03-30 2007-10-05 Snecma Sa Aube de redresseur a amenagement de forme localise, secteur de redresseurs, etage de compression, compresseur et turbomachine comportant une telle aube
FR2924156B1 (fr) * 2007-11-26 2014-02-14 Snecma Aube de turbomachine
DE102008035271B4 (de) 2008-07-29 2023-06-29 Genady Maslov Verfahren und Einrichtung zur Verarbeitung von Abgasen (Dieselmotor)
DE202008010121U1 (de) 2008-07-29 2009-05-14 Koltun, Mykhaylo Einrichtung zur Durchführung des Abgasreinigungsverfahrens (Dieselmotor)
DE202008010119U1 (de) 2008-07-29 2009-05-07 Koltun, Mykhaylo Einrichtung zur Reinigung von Abgasen der Turbostrahltriebwerke
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US8113784B2 (en) * 2009-03-20 2012-02-14 Hamilton Sundstrand Corporation Coolable airfoil attachment section
US8632297B2 (en) * 2010-09-29 2014-01-21 General Electric Company Turbine airfoil and method for cooling a turbine airfoil
EP2639004B1 (de) * 2012-03-15 2016-05-11 MTU Aero Engines GmbH Schaufelkranzsegment mit Ringraumbegrenzungsfläche mit einem welligen Höhenprofil sowie Verfahren zur Herstellung desselben
US9175569B2 (en) * 2012-03-30 2015-11-03 General Electric Company Turbine airfoil trailing edge cooling slots
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US20130302176A1 (en) * 2012-05-08 2013-11-14 Robert Frederick Bergholz, JR. Turbine airfoil trailing edge cooling slot
US20130302179A1 (en) * 2012-05-09 2013-11-14 Robert Frederick Bergholz, JR. Turbine airfoil trailing edge cooling hole plug and slot
EP2941543B1 (en) 2013-03-13 2017-03-22 Rolls-Royce Corporation Trenched cooling hole arrangement for a ceramic matrix composite vane
DE102013213416B4 (de) * 2013-07-09 2017-11-09 MTU Aero Engines AG Schaufel für eine Gasturbomaschine
US9995166B2 (en) * 2014-11-21 2018-06-12 General Electric Company Turbomachine including a vane and method of assembling such turbomachine
US20160208626A1 (en) * 2015-01-19 2016-07-21 United Technologies Corporation Integrally bladed rotor with pressure side thickness on blade trailing edge
US10196904B2 (en) 2016-01-24 2019-02-05 Rolls-Royce North American Technologies Inc. Turbine endwall and tip cooling for dual wall airfoils
US10240462B2 (en) 2016-01-29 2019-03-26 General Electric Company End wall contour for an axial flow turbine stage
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FR3108364B1 (fr) 2020-03-18 2022-03-11 Safran Aircraft Engines Aube de turbine comportant des nervures entre des sorties de refroidissement avec des orifices de refroidissement
FR3108363B1 (fr) 2020-03-18 2022-03-11 Safran Aircraft Engines Aube de turbine comportant trois types d’orifices de refroidissement du bord de fuite
DE102020207646A1 (de) 2020-06-22 2021-12-23 Siemens Aktiengesellschaft Turbinenschaufel und Verfahren zum Bearbeiten einer solchen
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CN113236370B (zh) * 2021-05-25 2023-04-25 杭州汽轮动力集团有限公司 一种燃气轮机涡轮高压动叶片的冷却结构
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Also Published As

Publication number Publication date
EP1555390A1 (fr) 2005-07-20
FR2864990B1 (fr) 2008-02-22
ES2276254T3 (es) 2007-06-16
DE602004003331T2 (de) 2007-06-21
US20050249593A1 (en) 2005-11-10
RU2294438C2 (ru) 2007-02-27
FR2864990A1 (fr) 2005-07-15
CA2493094A1 (fr) 2006-07-14
JP4619135B2 (ja) 2011-01-26
RU2005100467A (ru) 2006-06-20
CA2493094C (fr) 2011-10-11
EP1555390B1 (fr) 2006-11-22
JP2005201273A (ja) 2005-07-28
US7278827B2 (en) 2007-10-09
DE602004003331D1 (de) 2007-01-04

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