DE69817094D1 - Beschaufelung mit einer schraubenförmigen Rampe mit serieller Prallkühlung durch ein doppelwandiges Rippensystem - Google Patents

Beschaufelung mit einer schraubenförmigen Rampe mit serieller Prallkühlung durch ein doppelwandiges Rippensystem

Info

Publication number
DE69817094D1
DE69817094D1 DE69817094T DE69817094T DE69817094D1 DE 69817094 D1 DE69817094 D1 DE 69817094D1 DE 69817094 T DE69817094 T DE 69817094T DE 69817094 T DE69817094 T DE 69817094T DE 69817094 D1 DE69817094 D1 DE 69817094D1
Authority
DE
Germany
Prior art keywords
blading
double
helical ramp
impact cooling
rib system
Prior art date
Legal status (The legal status 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 status listed.)
Expired - Lifetime
Application number
DE69817094T
Other languages
English (en)
Other versions
DE69817094T2 (de
Inventor
Yves Maurice Bailly
Gerard Andre Coudray
Mischael Francois Loui Derrien
Jean-Michel Roger Fougeres
Philippe Christian Pellier
Jean-Claude Christian Taillant
Thierry Henri Marcel Tassin
Christophe Bernard Texier
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Safran Aircraft Engines SAS
Original Assignee
SNECMA Moteurs SA
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 SNECMA Moteurs SA filed Critical SNECMA Moteurs SA
Application granted granted Critical
Publication of DE69817094D1 publication Critical patent/DE69817094D1/de
Publication of DE69817094T2 publication Critical patent/DE69817094T2/de
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/12Blades
    • F01D5/14Form or construction
    • F01D5/18Hollow blades, i.e. blades with cooling or heating channels or cavities; Heating, heat-insulating or cooling means on blades
    • F01D5/187Convection cooling
    • F01D5/188Convection cooling with an insert in the blade cavity to guide the cooling fluid, e.g. forming a separation wall
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/12Blades
    • F01D5/14Form or construction
    • F01D5/18Hollow blades, i.e. blades with cooling or heating channels or cavities; Heating, heat-insulating or cooling means on blades
    • F01D5/187Convection cooling
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/12Blades
    • F01D5/14Form or construction
    • F01D5/18Hollow blades, i.e. blades with cooling or heating channels or cavities; Heating, heat-insulating or cooling means on blades
    • F01D5/187Convection cooling
    • F01D5/188Convection cooling with an insert in the blade cavity to guide the cooling fluid, e.g. forming a separation wall
    • F01D5/189Convection cooling with an insert in the blade cavity to guide the cooling fluid, e.g. forming a separation wall the insert having a tubular cross-section, e.g. airfoil shape
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2250/00Geometry
    • F05D2250/10Two-dimensional
    • F05D2250/15Two-dimensional spiral
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2250/00Geometry
    • F05D2250/20Three-dimensional
    • F05D2250/25Three-dimensional helical

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
DE69817094T 1997-06-26 1998-06-25 Beschaufelung mit einer schraubenförmigen Rampe mit serieller Prallkühlung durch ein doppelwandiges Rippensystem Expired - Lifetime DE69817094T2 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR9707988 1997-06-26
FR9707988A FR2765265B1 (fr) 1997-06-26 1997-06-26 Aubage refroidi par rampe helicoidale, par impact en cascade et par systeme a pontets dans une double peau

Publications (2)

Publication Number Publication Date
DE69817094D1 true DE69817094D1 (de) 2003-09-18
DE69817094T2 DE69817094T2 (de) 2004-06-17

Family

ID=9508460

Family Applications (1)

Application Number Title Priority Date Filing Date
DE69817094T Expired - Lifetime DE69817094T2 (de) 1997-06-26 1998-06-25 Beschaufelung mit einer schraubenförmigen Rampe mit serieller Prallkühlung durch ein doppelwandiges Rippensystem

Country Status (6)

Country Link
US (1) US5993156A (de)
EP (1) EP0887515B1 (de)
JP (1) JP3735201B2 (de)
DE (1) DE69817094T2 (de)
FR (1) FR2765265B1 (de)
RU (1) RU2146766C1 (de)

Families Citing this family (77)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2345942B (en) * 1998-12-24 2002-08-07 Rolls Royce Plc Gas turbine engine internal air system
US6206638B1 (en) * 1999-02-12 2001-03-27 General Electric Company Low cost airfoil cooling circuit with sidewall impingement cooling chambers
US6402470B1 (en) * 1999-10-05 2002-06-11 United Technologies Corporation Method and apparatus for cooling a wall within a gas turbine engine
US6435814B1 (en) * 2000-05-16 2002-08-20 General Electric Company Film cooling air pocket in a closed loop cooled airfoil
US6508627B2 (en) 2001-05-30 2003-01-21 Lau Industries, Inc. Airfoil blade and method for its manufacture
US6609891B2 (en) * 2001-08-30 2003-08-26 General Electric Company Turbine airfoil for gas turbine engine
US6981846B2 (en) 2003-03-12 2006-01-03 Florida Turbine Technologies, Inc. Vortex cooling of turbine blades
US6932573B2 (en) 2003-04-30 2005-08-23 Siemens Westinghouse Power Corporation Turbine blade having a vortex forming cooling system for a trailing edge
US7343232B2 (en) * 2003-06-20 2008-03-11 Geneva Aerospace Vehicle control system including related methods and components
FR2858352B1 (fr) * 2003-08-01 2006-01-20 Snecma Moteurs Circuit de refroidissement pour aube de turbine
US6955525B2 (en) 2003-08-08 2005-10-18 Siemens Westinghouse Power Corporation Cooling system for an outer wall of a turbine blade
US7818127B1 (en) * 2004-06-18 2010-10-19 Geneva Aerospace, Inc. Collision avoidance for vehicle control systems
ATE410586T1 (de) * 2004-07-26 2008-10-15 Siemens Ag Gekühltes bauteil einer strömungsmaschine und verfahren zum giessen dieses gekühlten bauteils
GB0418914D0 (en) * 2004-08-25 2004-09-29 Rolls Royce Plc Turbine component
EP1655451B1 (de) * 2004-11-09 2010-06-30 Rolls-Royce Plc Kühlanordnung
US7163373B2 (en) * 2005-02-02 2007-01-16 Siemens Power Generation, Inc. Vortex dissipation device for a cooling system within a turbine blade of a turbine engine
RU2425982C2 (ru) * 2005-04-14 2011-08-10 Альстом Текнолоджи Лтд Лопатка газовой турбины
US7563072B1 (en) * 2006-09-25 2009-07-21 Florida Turbine Technologies, Inc. Turbine airfoil with near-wall spiral flow cooling circuit
US7641445B1 (en) 2006-12-01 2010-01-05 Florida Turbine Technologies, Inc. Large tapered rotor blade with near wall cooling
US7753650B1 (en) 2006-12-20 2010-07-13 Florida Turbine Technologies, Inc. Thin turbine rotor blade with sinusoidal flow cooling channels
US7665965B1 (en) * 2007-01-17 2010-02-23 Florida Turbine Technologies, Inc. Turbine rotor disk with dirt particle separator
US7901182B2 (en) * 2007-05-18 2011-03-08 Siemens Energy, Inc. Near wall cooling for a highly tapered turbine blade
US20090060714A1 (en) * 2007-08-30 2009-03-05 General Electric Company Multi-part cast turbine engine component having an internal cooling channel and method of forming a multi-part cast turbine engine component
FR2924156B1 (fr) * 2007-11-26 2014-02-14 Snecma Aube de turbomachine
US9322285B2 (en) * 2008-02-20 2016-04-26 United Technologies Corporation Large fillet airfoil with fanned cooling hole array
US8297927B1 (en) * 2008-03-04 2012-10-30 Florida Turbine Technologies, Inc. Near wall multiple impingement serpentine flow cooled airfoil
GB2462087A (en) * 2008-07-22 2010-01-27 Rolls Royce Plc An aerofoil comprising a partition web with a chordwise or spanwise variation
US8303252B2 (en) * 2008-10-16 2012-11-06 United Technologies Corporation Airfoil with cooling passage providing variable heat transfer rate
US8096766B1 (en) 2009-01-09 2012-01-17 Florida Turbine Technologies, Inc. Air cooled turbine airfoil with sequential cooling
US8342797B2 (en) * 2009-08-31 2013-01-01 Rolls-Royce North American Technologies Inc. Cooled gas turbine engine airflow member
US9528382B2 (en) * 2009-11-10 2016-12-27 General Electric Company Airfoil heat shield
US8511994B2 (en) * 2009-11-23 2013-08-20 United Technologies Corporation Serpentine cored airfoil with body microcircuits
US20120076660A1 (en) * 2010-09-28 2012-03-29 Spangler Brandon W Conduction pedestals for a gas turbine engine airfoil
US9011077B2 (en) 2011-04-20 2015-04-21 Siemens Energy, Inc. Cooled airfoil in a turbine engine
GB2498551B (en) * 2012-01-20 2015-07-08 Rolls Royce Plc Aerofoil cooling
DE102012017491A1 (de) * 2012-09-04 2014-03-06 Rolls-Royce Deutschland Ltd & Co Kg Turbinenschaufel einer Gasturbine mit Drallerzeugungselement
KR101317443B1 (ko) * 2012-10-10 2013-10-10 한국항공대학교산학협력단 가스터빈의 냉각블레이드
US20160010466A1 (en) * 2013-03-15 2016-01-14 United Technologies Corporation Gas turbine engine component with twisted internal channel
WO2015030926A1 (en) 2013-08-30 2015-03-05 United Technologies Corporation Baffle for gas turbine engine vane
WO2015034717A1 (en) 2013-09-06 2015-03-12 United Technologies Corporation Gas turbine engine airfoil with wishbone baffle cooling scheme
WO2015076909A2 (en) * 2013-09-09 2015-05-28 United Technologies Corporation Cooling configuration for engine component
EP2863010A1 (de) * 2013-10-21 2015-04-22 Siemens Aktiengesellschaft Turbinenschaufel
US8864438B1 (en) * 2013-12-05 2014-10-21 Siemens Energy, Inc. Flow control insert in cooling passage for turbine vane
WO2015094531A1 (en) 2013-12-20 2015-06-25 United Technologies Corporation Gas turbine engine component cooling cavity with vortex promoting features
KR101509385B1 (ko) * 2014-01-16 2015-04-07 두산중공업 주식회사 스월링 냉각 채널을 구비한 터빈 블레이드 및 그 냉각 방법
US20150204197A1 (en) * 2014-01-23 2015-07-23 Siemens Aktiengesellschaft Airfoil leading edge chamber cooling with angled impingement
RU2568763C2 (ru) * 2014-01-30 2015-11-20 Альстом Текнолоджи Лтд Компонент газовой турбины
EP3105436A4 (de) * 2014-02-13 2017-03-08 United Technologies Corporation Gasturbinenmotorkomponente mit trennungsrippe für kühlkanäle
US10012090B2 (en) * 2014-07-25 2018-07-03 United Technologies Corporation Airfoil cooling apparatus
FR3032173B1 (fr) 2015-01-29 2018-07-27 Safran Aircraft Engines Pale d'helice de turbopropulseur a soufflage
US10190420B2 (en) * 2015-02-10 2019-01-29 United Technologies Corporation Flared crossovers for airfoils
US9849510B2 (en) 2015-04-16 2017-12-26 General Electric Company Article and method of forming an article
US9915151B2 (en) * 2015-05-26 2018-03-13 Rolls-Royce Corporation CMC airfoil with cooling channels
US9976441B2 (en) 2015-05-29 2018-05-22 General Electric Company Article, component, and method of forming an article
US10739087B2 (en) 2015-09-08 2020-08-11 General Electric Company Article, component, and method of forming an article
US10253986B2 (en) 2015-09-08 2019-04-09 General Electric Company Article and method of forming an article
US10087776B2 (en) 2015-09-08 2018-10-02 General Electric Company Article and method of forming an article
RU2706211C2 (ru) 2016-01-25 2019-11-14 Ансалдо Энерджиа Свитзерлэнд Аг Охлаждаемая стенка компонента турбины и способ охлаждения этой стенки
EP3228819B1 (de) * 2016-04-08 2021-06-09 Ansaldo Energia Switzerland AG Schaufel umfassend cmc-schichten
US10156146B2 (en) * 2016-04-25 2018-12-18 General Electric Company Airfoil with variable slot decoupling
FR3052183B1 (fr) * 2016-06-02 2020-03-06 Safran Aircraft Engines Aube de turbine comprenant une portion d'admission d'air de refroidissement incluant un element helicoidal pour faire tourbillonner l'air de refroidissement
RU171631U1 (ru) * 2016-09-14 2017-06-07 Федеральное государственное унитарное предприятие "Центральный институт авиационного моторостроения им. П.И. Баранова" Охлаждаемая лопатка турбины
DE102016221009A1 (de) 2016-10-26 2018-04-26 Continental Reifen Deutschland Gmbh Druckregelvorrichtung
US20180149028A1 (en) 2016-11-30 2018-05-31 General Electric Company Impingement insert for a gas turbine engine
CN106703899B (zh) * 2017-01-23 2019-08-23 中国航发沈阳发动机研究所 高压涡轮转子叶片前缘冲击冷却结构及具有其的发动机
US10494948B2 (en) * 2017-05-09 2019-12-03 General Electric Company Impingement insert
US10570751B2 (en) * 2017-11-22 2020-02-25 General Electric Company Turbine engine airfoil assembly
US10787912B2 (en) * 2018-04-25 2020-09-29 Raytheon Technologies Corporation Spiral cavities for gas turbine engine components
US10787913B2 (en) * 2018-11-01 2020-09-29 United Technologies Corporation Airfoil cooling circuit
US11149550B2 (en) * 2019-02-07 2021-10-19 Raytheon Technologies Corporation Blade neck transition
US10871074B2 (en) 2019-02-28 2020-12-22 Raytheon Technologies Corporation Blade/vane cooling passages
FR3107919B1 (fr) 2020-03-03 2022-12-02 Safran Aircraft Engines Aube creuse de turbomachine et plateforme inter-aubes équipées de saillies perturbatrices de flux de refroidissement
FR3108145B1 (fr) * 2020-03-13 2022-02-18 Safran Helicopter Engines Aube creuse de turbomachine
CN112610284A (zh) * 2020-12-17 2021-04-06 东北电力大学 一种具有螺旋纽带的燃气轮机涡轮叶片
CN113374536B (zh) * 2021-06-09 2022-08-09 中国航发湖南动力机械研究所 燃气涡轮导向叶片
US20230417146A1 (en) * 2022-06-23 2023-12-28 Solar Turbines Incorporated Pneumatically variable turbine nozzle
CN116950723B (zh) * 2023-09-19 2024-01-09 中国航发四川燃气涡轮研究院 一种低应力双层壁涡轮导向叶片冷却结构及其设计方法

Family Cites Families (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE853534C (de) * 1943-02-27 1952-10-27 Maschf Augsburg Nuernberg Ag Luftgekuehlte Gasturbinenschaufel
BE485284A (de) * 1947-10-28
BE496812A (de) * 1949-07-06 1900-01-01
DE2514208A1 (de) * 1975-04-01 1976-10-14 Kraftwerk Union Ag Gasturbine der scheibenbauart
CH584833A5 (de) * 1975-05-16 1977-02-15 Bbc Brown Boveri & Cie
US4173120A (en) * 1977-09-09 1979-11-06 International Harvester Company Turbine nozzle and rotor cooling systems
US4407632A (en) * 1981-06-26 1983-10-04 United Technologies Corporation Airfoil pedestaled trailing edge region cooling configuration
DE3306894A1 (de) * 1983-02-26 1984-08-30 MTU Motoren- und Turbinen-Union München GmbH, 8000 München Turbinenleit- oder laufschaufel mit kuehlkanal
JPS62228603A (ja) * 1986-03-31 1987-10-07 Toshiba Corp ガスタ−ビンの翼
US5002460A (en) * 1989-10-02 1991-03-26 General Electric Company Internally cooled airfoil blade
FR2678318B1 (fr) * 1991-06-25 1993-09-10 Snecma Aube refroidie de distributeur de turbine.
JP3006174B2 (ja) * 1991-07-04 2000-02-07 株式会社日立製作所 内部に冷却通路を有する部材
US5259730A (en) * 1991-11-04 1993-11-09 General Electric Company Impingement cooled airfoil with bonding foil insert
US5695322A (en) * 1991-12-17 1997-12-09 General Electric Company Turbine blade having restart turbulators
US5464322A (en) * 1994-08-23 1995-11-07 General Electric Company Cooling circuit for turbine stator vane trailing edge
US5472316A (en) * 1994-09-19 1995-12-05 General Electric Company Enhanced cooling apparatus for gas turbine engine airfoils

Also Published As

Publication number Publication date
DE69817094T2 (de) 2004-06-17
JPH1172003A (ja) 1999-03-16
RU2146766C1 (ru) 2000-03-20
US5993156A (en) 1999-11-30
EP0887515A1 (de) 1998-12-30
JP3735201B2 (ja) 2006-01-18
FR2765265B1 (fr) 1999-08-20
FR2765265A1 (fr) 1998-12-31
EP0887515B1 (de) 2003-08-13

Similar Documents

Publication Publication Date Title
DE69817094D1 (de) Beschaufelung mit einer schraubenförmigen Rampe mit serieller Prallkühlung durch ein doppelwandiges Rippensystem
DE60016474D1 (de) Strömungsmaschine mit einem mit einer Abkühlvorrichtung versehenen Untersetzungsgetriebe
GB2356669B (en) Fan case for turbofan engine having a fan decoupler
DE29614444U1 (de) Kupplungsanordnung für ein Fahrzeug
DE59602649D1 (de) Fluggasturbinen-triebwerk mit einem flüssigkeits-luft-wärmetauscher
DE69802948T2 (de) Ein getaperter stegwellenleiter
DE69729362D1 (de) Ein Verbinder
DE69823658D1 (de) Ein laser
DE9413972U1 (de) Lagerungselement für ein im wesentlichen plattenförmiges Bauteil
DE69838236D1 (de) Ein Verbinder mit Verriegelung
DE69507142T2 (de) Wasserstrahlantrieb für ein wasserfahrzeug
DE69506123T2 (de) Ein getriebe aufweisender bausatz
GB2295381B (en) A collapsible flatrack with ramp end walls
NO973834D0 (no) Styrebånd for et prosjektil
DE69815907D1 (de) Zünder mit einer Sprengwand
DE69510301T2 (de) Ein Flächenbelag
KR100275296B1 (en) Method for repairing and/or reinforcing a bulkhead for a bulkhead type heat exchanger
DE50103900D1 (de) Verbrennungssystem für ein gargerät sowie gargerät mit solch einem verbrennungssystem
DE29618522U1 (de) Bausatz für ein Fertigteilhaus
DE69921733D1 (de) Mikroprozessorschnittstelle mit einem durch ein Vordekodierungssystem optimierten externen Speicher
DE29612824U1 (de) Drehmoment übertragendes Bauteil mit einer Sollbruchstelle
ATA81794A (de) Tauchwandanordnung in einer regenwasseranlage
DE59706485D1 (de) Verriegelungs-Baugruppe bei einem Startgerät für Flugkörper
DE29623252U1 (de) Wärmespeicherofen mit einem Latentwärmespeicher
DE29606558U1 (de) Lösbare Stangenverbindung bei einem Stangenverschluß

Legal Events

Date Code Title Description
8364 No opposition during term of opposition
8327 Change in the person/name/address of the patent owner

Owner name: SNECMA, PARIS, FR