SE0400477L - En komponent som innefattar en ledskena eller ett rotorblad för en gasturbin - Google Patents

En komponent som innefattar en ledskena eller ett rotorblad för en gasturbin

Info

Publication number
SE0400477L
SE0400477L SE0400477A SE0400477A SE0400477L SE 0400477 L SE0400477 L SE 0400477L SE 0400477 A SE0400477 A SE 0400477A SE 0400477 A SE0400477 A SE 0400477A SE 0400477 L SE0400477 L SE 0400477L
Authority
SE
Sweden
Prior art keywords
component
guide rail
gas turbine
rotor blade
rotor
Prior art date
Application number
SE0400477A
Other languages
English (en)
Other versions
SE0400477D0 (sv
SE526847C2 (sv
Inventor
Sergey Shukin
Andrey Shukin
Mats Annerfeldt
Original Assignee
Demag Delaval Ind Turbomachine
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 Demag Delaval Ind Turbomachine filed Critical Demag Delaval Ind Turbomachine
Priority to SE0400477A priority Critical patent/SE526847C2/sv
Publication of SE0400477D0 publication Critical patent/SE0400477D0/sv
Priority to EP05716798.3A priority patent/EP1718845B1/en
Priority to CNB2005800135065A priority patent/CN100557198C/zh
Priority to US10/590,463 priority patent/US7674092B2/en
Priority to CA002557493A priority patent/CA2557493C/en
Priority to RU2006134287/06A priority patent/RU2341661C2/ru
Priority to PCT/EP2005/050804 priority patent/WO2005083235A1/en
Publication of SE0400477L publication Critical patent/SE0400477L/sv
Publication of SE526847C2 publication Critical patent/SE526847C2/sv

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
    • 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
    • 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
    • F05D2250/00—Geometry
    • F05D2250/70—Shape
    • F05D2250/71—Shape curved
    • 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
    • F05D2260/00—Function
    • F05D2260/20—Heat transfer, e.g. cooling
    • F05D2260/221—Improvement of heat transfer
    • F05D2260/2214—Improvement of heat transfer by increasing the heat transfer surface
    • F05D2260/22141—Improvement of heat transfer by increasing the heat transfer surface using fins or ribs

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)
SE0400477A 2004-02-27 2004-02-27 En komponent som innefattar en ledskena eller ett rotorblad för en gasturbin SE526847C2 (sv)

Priority Applications (7)

Application Number Priority Date Filing Date Title
SE0400477A SE526847C2 (sv) 2004-02-27 2004-02-27 En komponent som innefattar en ledskena eller ett rotorblad för en gasturbin
EP05716798.3A EP1718845B1 (en) 2004-02-27 2005-02-25 Blade or vane for a turbomachine
CNB2005800135065A CN100557198C (zh) 2004-02-27 2005-02-25 涡轮机的叶片或翼片
US10/590,463 US7674092B2 (en) 2004-02-27 2005-02-25 Blade or vane for a turbomachine
CA002557493A CA2557493C (en) 2004-02-27 2005-02-25 Blade or vane for a turbomachine
RU2006134287/06A RU2341661C2 (ru) 2004-02-27 2005-02-25 Лопасть или лопатка для турбомашины
PCT/EP2005/050804 WO2005083235A1 (en) 2004-02-27 2005-02-25 Blade or vane for a turbomachine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
SE0400477A SE526847C2 (sv) 2004-02-27 2004-02-27 En komponent som innefattar en ledskena eller ett rotorblad för en gasturbin

Publications (3)

Publication Number Publication Date
SE0400477D0 SE0400477D0 (sv) 2004-02-27
SE0400477L true SE0400477L (sv) 2005-08-28
SE526847C2 SE526847C2 (sv) 2005-11-08

Family

ID=31989634

Family Applications (1)

Application Number Title Priority Date Filing Date
SE0400477A SE526847C2 (sv) 2004-02-27 2004-02-27 En komponent som innefattar en ledskena eller ett rotorblad för en gasturbin

Country Status (7)

Country Link
US (1) US7674092B2 (sv)
EP (1) EP1718845B1 (sv)
CN (1) CN100557198C (sv)
CA (1) CA2557493C (sv)
RU (1) RU2341661C2 (sv)
SE (1) SE526847C2 (sv)
WO (1) WO2005083235A1 (sv)

Families Citing this family (24)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20070227706A1 (en) * 2005-09-19 2007-10-04 United Technologies Corporation Compact heat exchanger
EP1925780A1 (en) 2006-11-23 2008-05-28 Siemens Aktiengesellschaft Blade for an axial-flow turbine
US8342797B2 (en) * 2009-08-31 2013-01-01 Rolls-Royce North American Technologies Inc. Cooled gas turbine engine airflow member
WO2011050025A2 (en) * 2009-10-20 2011-04-28 Siemens Energy, Inc. Airfoil incorporating tapered cooling structures defining cooling passageways
US8636463B2 (en) * 2010-03-31 2014-01-28 General Electric Company Interior cooling channels
US8585365B1 (en) * 2010-04-13 2013-11-19 Florida Turbine Technologies, Inc. Turbine blade with triple pass serpentine cooling
EP2378073A1 (en) 2010-04-14 2011-10-19 Siemens Aktiengesellschaft Blade or vane for a turbomachine
US8894363B2 (en) 2011-02-09 2014-11-25 Siemens Energy, Inc. Cooling module design and method for cooling components of a gas turbine system
EP2418355A1 (en) 2010-08-13 2012-02-15 Siemens Aktiengesellschaft Gas turbine vane
US10060264B2 (en) * 2010-12-30 2018-08-28 Rolls-Royce North American Technologies Inc. Gas turbine engine and cooled flowpath component therefor
US8790084B2 (en) * 2011-10-31 2014-07-29 General Electric Company Airfoil and method of fabricating the same
CN103946483A (zh) 2011-11-25 2014-07-23 西门子公司 具有冷却通路的翼
US9206695B2 (en) * 2012-09-28 2015-12-08 Solar Turbines Incorporated Cooled turbine blade with trailing edge flow metering
US9228439B2 (en) 2012-09-28 2016-01-05 Solar Turbines Incorporated Cooled turbine blade with leading edge flow redirection and diffusion
US9314838B2 (en) 2012-09-28 2016-04-19 Solar Turbines Incorporated Method of manufacturing a cooled turbine blade with dense cooling fin array
JP6036424B2 (ja) * 2013-03-14 2016-11-30 株式会社Ihi 冷却促進構造
WO2014186109A1 (en) * 2013-05-15 2014-11-20 United Technologies Corporation Gas turbine engine airfoil cooling passage turbulator pedestal
US9133716B2 (en) * 2013-12-02 2015-09-15 Siemens Energy, Inc. Turbine endwall with micro-circuit cooling
EP3123000B1 (en) * 2014-03-27 2019-02-06 Siemens Aktiengesellschaft Blade for a gas turbine and method of cooling the blade
FR3029242B1 (fr) * 2014-11-28 2016-12-30 Snecma Aube de turbomachine, comprenant des cloisons entrecroisees pour la circulation d'air en direction du bord de fuite
JP6898104B2 (ja) * 2017-01-18 2021-07-07 川崎重工業株式会社 タービン翼の冷却構造
JP6906332B2 (ja) * 2017-03-10 2021-07-21 川崎重工業株式会社 タービン翼の冷却構造
US10822963B2 (en) * 2018-12-05 2020-11-03 Raytheon Technologies Corporation Axial flow cooling scheme with castable structural rib for a gas turbine engine
JP2021050688A (ja) * 2019-09-26 2021-04-01 川崎重工業株式会社 タービン翼

Family Cites Families (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3017159A (en) 1956-11-23 1962-01-16 Curtiss Wright Corp Hollow blade construction
US3635587A (en) * 1970-06-02 1972-01-18 Gen Motors Corp Blade cooling liner
GB1404757A (en) 1971-08-25 1975-09-03 Rolls Royce Gas turbine engine blades
GB1361256A (en) 1971-08-25 1974-07-24 Rolls Royce Gas turbine engine blades
GB1410014A (en) * 1971-12-14 1975-10-15 Rolls Royce Gas turbine engine blade
SU779590A1 (ru) * 1977-07-21 1980-11-15 Предприятие П/Я А-1469 Охлаждаема лопатка турбины
US4407632A (en) * 1981-06-26 1983-10-04 United Technologies Corporation Airfoil pedestaled trailing edge region cooling configuration
SU1228559A1 (ru) 1981-11-13 1996-10-10 Г.П. Нагога Рабочая лопатка газовой турбины
US4526512A (en) * 1983-03-28 1985-07-02 General Electric Co. Cooling flow control device for turbine blades
US5243759A (en) * 1991-10-07 1993-09-14 United Technologies Corporation Method of casting to control the cooling air flow rate of the airfoil trailing edge
RU2042833C1 (ru) 1993-06-29 1995-08-27 Авиамоторный научно-технический комплекс "Союз" Охлаждаемая лопатка газовой турбины
DE19634238A1 (de) * 1996-08-23 1998-02-26 Asea Brown Boveri Kühlbare Schaufel
SE512384C2 (sv) * 1998-05-25 2000-03-06 Abb Ab Komponent för en gasturbin

Also Published As

Publication number Publication date
SE0400477D0 (sv) 2004-02-27
CN1997811A (zh) 2007-07-11
CA2557493A1 (en) 2005-09-09
EP1718845B1 (en) 2017-02-01
US20070172354A1 (en) 2007-07-26
RU2006134287A (ru) 2008-04-10
RU2341661C2 (ru) 2008-12-20
CA2557493C (en) 2009-12-15
WO2005083235A1 (en) 2005-09-09
EP1718845A1 (en) 2006-11-08
CN100557198C (zh) 2009-11-04
SE526847C2 (sv) 2005-11-08
US7674092B2 (en) 2010-03-09

Similar Documents

Publication Publication Date Title
SE0400477L (sv) En komponent som innefattar en ledskena eller ett rotorblad för en gasturbin
DK1754886T3 (da) Rotorblad til en vindenergiturbine
GB0706205D0 (en) Stator blade airfoil profile for a compressor
NO20054322D0 (no) Rotorblad for forste trinn i en gassturbin
ATE501355T1 (de) Rotorblatt für eine windenergieanlage
ATE452289T1 (de) Rotorblatt für eine windenergieanlage
EP1984244A4 (en) AERODYNAMIC PROFILE FOR A HELICOPTER ROTOR BLADE
GB2445896B (en) Airfoil for a second stage nozzle guide vane
GB0510538D0 (en) A rotor blade containment assembly for a gas turbine engine
DE602006015740D1 (de) Kontrollsystem für verstellbaren Statorschaufelstufen einer Turbomaschine
GB0408825D0 (en) A rotor blade containment assembly for a gas turbine engine
PT1716333T (pt) Pá do rotor de uma turbina eólica
DE10301755A8 (de) Fanschaufel für ein Gasturbinentriebwerk
GB2407136B (en) Turbine rotor blade for gas turbine engine
DE10392111D2 (de) Rotorblatt für Windenergieanlagen
DK1788240T3 (da) Rotor til en vindenergiturbine
DE602006002050D1 (de) Halbmondförmiger Turbinenschaufel-/Plattformübergang
DE502004003477D1 (de) Filmgekühlte Turbinenschaufel
GB2413160B (en) Turbine rotor blades
DE602004006922D1 (de) Leitschaufelanordnung für ein Gasturbinentriebwerk
GB2437298B (en) A Seal Between Rotor Blade Platforms And Stator Vane Platforms, A Rotor Blade And A Stator Vane
GB0523469D0 (en) Blades for gas turbine engines
EP1893483A4 (en) ROTOR BLADE FOR HIGH-SPEED ROTATING SAIL AIRCRAFT
DE602006011089D1 (de) Kern für Turbinenschaufel
DE602006014902D1 (de) Kontrollanlage für verstellbare Leitschaufelstufen einer Turbomaschine