UA80246C2 - Лопатка турбіни та турбіна високого тиску турбомашини - Google Patents

Лопатка турбіни та турбіна високого тиску турбомашини Download PDF

Info

Publication number
UA80246C2
UA80246C2 UA2002129702A UA2002129702A UA80246C2 UA 80246 C2 UA80246 C2 UA 80246C2 UA 2002129702 A UA2002129702 A UA 2002129702A UA 2002129702 A UA2002129702 A UA 2002129702A UA 80246 C2 UA80246 C2 UA 80246C2
Authority
UA
Ukraine
Prior art keywords
blade
base
feather
closest
outlet
Prior art date
Application number
UA2002129702A
Other languages
English (en)
Russian (ru)
Ukrainian (uk)
Inventor
Крістіан Барйо
Жак Бурі
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 UA80246C2 publication Critical patent/UA80246C2/uk

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

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
UA2002129702A 2001-12-10 2002-12-04 Лопатка турбіни та турбіна високого тиску турбомашини UA80246C2 (uk)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0115904A FR2833298B1 (fr) 2001-12-10 2001-12-10 Perfectionnements apportes au comportement thermique du bord de fuite d'une aube de turbine haute-pression

Publications (1)

Publication Number Publication Date
UA80246C2 true UA80246C2 (uk) 2007-09-10

Family

ID=8870271

Family Applications (1)

Application Number Title Priority Date Filing Date
UA2002129702A UA80246C2 (uk) 2001-12-10 2002-12-04 Лопатка турбіни та турбіна високого тиску турбомашини

Country Status (9)

Country Link
US (1) US6830431B2 (fr)
EP (1) EP1318274B1 (fr)
JP (1) JP4012054B2 (fr)
CA (1) CA2412989C (fr)
DE (1) DE60201325T2 (fr)
ES (1) ES2225740T3 (fr)
FR (1) FR2833298B1 (fr)
RU (1) RU2297537C2 (fr)
UA (1) UA80246C2 (fr)

Families Citing this family (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2864990B1 (fr) * 2004-01-14 2008-02-22 Snecma Moteurs Perfectionnements apportes aux fentes d'evacuation de l'air de refroidissement d'aubes de turbine haute-pression
US7503749B2 (en) * 2005-04-01 2009-03-17 General Electric Company Turbine nozzle with trailing edge convection and film cooling
FR2887287B1 (fr) * 2005-06-21 2007-09-21 Snecma Moteurs Sa Circuits de refroidissement pour aube mobile de turbomachine
KR100847523B1 (ko) * 2006-12-29 2008-07-22 엘지전자 주식회사 터보팬
US8002525B2 (en) * 2007-11-16 2011-08-23 Siemens Energy, Inc. Turbine airfoil cooling system with recessed trailing edge cooling slot
FR2924156B1 (fr) * 2007-11-26 2014-02-14 Snecma Aube de turbomachine
US8157504B2 (en) * 2009-04-17 2012-04-17 General Electric Company Rotor blades for turbine engines
FR2954798B1 (fr) 2009-12-31 2012-03-30 Snecma Aube a ventilation interieure
US8608429B2 (en) * 2010-05-28 2013-12-17 General Electric Company System and method for enhanced turbine wake mixing via fluidic-generated vortices
US10107108B2 (en) 2015-04-29 2018-10-23 General Electric Company Rotor blade having a flared tip
DE102020207646A1 (de) * 2020-06-22 2021-12-23 Siemens Aktiengesellschaft Turbinenschaufel und Verfahren zum Bearbeiten einer solchen

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
BE794195A (fr) * 1972-01-18 1973-07-18 Bbc Sulzer Turbomaschinen Aube directrice refroidie pour des turbines a gaz
GB2121483B (en) * 1982-06-08 1985-02-13 Rolls Royce Cooled turbine blade for a gas turbine engine
US4601638A (en) * 1984-12-21 1986-07-22 United Technologies Corporation Airfoil trailing edge cooling arrangement
US5403158A (en) * 1993-12-23 1995-04-04 United Technologies Corporation Aerodynamic tip sealing for rotor blades
WO1998000627A1 (fr) * 1996-06-28 1998-01-08 United Technologies Corporation Aube pouvant etre refroidie pour moteur a turbine a gaz
CA2334071C (fr) * 2000-02-23 2005-05-24 Mitsubishi Heavy Industries, Ltd. Aube mobile de turbine a gaz

Also Published As

Publication number Publication date
CA2412989A1 (fr) 2003-06-05
JP4012054B2 (ja) 2007-11-21
JP2003193804A (ja) 2003-07-09
US20030108425A1 (en) 2003-06-12
EP1318274A1 (fr) 2003-06-11
FR2833298B1 (fr) 2004-08-06
ES2225740T3 (es) 2005-03-16
RU2297537C2 (ru) 2007-04-20
DE60201325T2 (de) 2005-03-17
DE60201325D1 (de) 2004-10-28
FR2833298A1 (fr) 2003-06-13
EP1318274B1 (fr) 2004-09-22
US6830431B2 (en) 2004-12-14
CA2412989C (fr) 2008-09-23

Similar Documents

Publication Publication Date Title
US7607891B2 (en) Turbine component with tip flagged pedestal cooling
JP4659206B2 (ja) 勾配付きフイルム冷却を備えるタービンノズル
US7547191B2 (en) Turbine airfoil cooling system with perimeter cooling and rim cavity purge channels
JP4416287B2 (ja) 内部冷却翼形部品並びに冷却方法
JP4540973B2 (ja) ベンチュリ出口を有するタービン翼形部
US6416284B1 (en) Turbine blade for gas turbine engine and method of cooling same
US7837441B2 (en) Impingement skin core cooling for gas turbine engine blade
US7004720B2 (en) Cooled turbine vane platform
JP4311919B2 (ja) ガスタービンエンジン用のタービン翼形部
US11389860B2 (en) Hollow turbine blade with reduced cooling air extraction
US20070128029A1 (en) Turbine airfoil cooling system with elbowed, diffusion film cooling hole
US10502093B2 (en) Turbine shroud cooling
EP1088964A2 (fr) Fente pour le refroidissement par impact du bord d'attaque d'une aube pour une turbomachine
JP2001003704A (ja) 内部冷却式タービン翼形部
US20080050241A1 (en) Turbine airfoil cooling system with axial flowing serpentine cooling chambers
US8668454B2 (en) Turbine airfoil fillet cooling system
KR20100076891A (ko) 교차-유동을 차단하는 터빈 로터 블레이드 팁
US6599092B1 (en) Methods and apparatus for cooling gas turbine nozzles
US7387492B2 (en) Methods and apparatus for cooling turbine blade trailing edges
US20190178103A1 (en) Turbine shroud cooling
JP4458772B2 (ja) ガスタービンエンジンのエーロフォイルの有効寿命を延ばすための方法及び装置
CN106968722B (zh) 涡轮翼型件后缘冷却通路
UA80246C2 (uk) Лопатка турбіни та турбіна високого тиску турбомашини
US20030138322A1 (en) Moving blade for a high pressure turbine, the blade having a trailing edge of improved thermal behavior
EP0623189B1 (fr) Ensemble d'etancheite d'air externe a refroidissement pour turbine