CH615729A5 - - Google Patents

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Publication number
CH615729A5
CH615729A5 CH1511676A CH1511676A CH615729A5 CH 615729 A5 CH615729 A5 CH 615729A5 CH 1511676 A CH1511676 A CH 1511676A CH 1511676 A CH1511676 A CH 1511676A CH 615729 A5 CH615729 A5 CH 615729A5
Authority
CH
Switzerland
Prior art keywords
blade
vane
cooling air
insert
membrane
Prior art date
Application number
CH1511676A
Other languages
German (de)
English (en)
Inventor
Svante Bengt Goesta Stenfors
Original Assignee
Stal Laval Turbin Ab
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 Stal Laval Turbin Ab filed Critical Stal Laval Turbin Ab
Publication of CH615729A5 publication Critical patent/CH615729A5/de

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
    • F01D5/188—Convection cooling with an insert in the blade cavity to guide the cooling fluid, e.g. forming a separation wall
    • F01D5/189—Convection 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
CH1511676A 1976-01-19 1976-12-01 CH615729A5 (en:Method)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
SE7600473A SE395934B (sv) 1976-01-19 1976-01-19 Kyld-ihalig ledskovel for gasturbin

Publications (1)

Publication Number Publication Date
CH615729A5 true CH615729A5 (en:Method) 1980-02-15

Family

ID=20326757

Family Applications (1)

Application Number Title Priority Date Filing Date
CH1511676A CH615729A5 (en:Method) 1976-01-19 1976-12-01

Country Status (4)

Country Link
US (1) US4086021A (en:Method)
CH (1) CH615729A5 (en:Method)
GB (1) GB1565743A (en:Method)
SE (1) SE395934B (en:Method)

Families Citing this family (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH0756201B2 (ja) * 1984-03-13 1995-06-14 株式会社東芝 ガスタービン翼
JP2862536B2 (ja) * 1987-09-25 1999-03-03 株式会社東芝 ガスタービンの翼
US5328331A (en) * 1993-06-28 1994-07-12 General Electric Company Turbine airfoil with double shell outer wall
US5484258A (en) * 1994-03-01 1996-01-16 General Electric Company Turbine airfoil with convectively cooled double shell outer wall
US5516260A (en) * 1994-10-07 1996-05-14 General Electric Company Bonded turbine airfuel with floating wall cooling insert
ITTO20020607A1 (it) * 2002-07-12 2004-01-12 Fiatavio Spa Metodo per la realizzazione ed il montaggio di un dispositivo di raffreddamento in una paletta di una turbina assiale a gas e paletta per un
EP2584145A1 (en) 2011-10-20 2013-04-24 Siemens Aktiengesellschaft A cooled turbine guide vane or blade for a turbomachine
CN112554962B (zh) * 2020-12-02 2022-11-22 中国航发沈阳发动机研究所 一种涡轮导向冷却叶片缘板尾端的冷却结构

Family Cites Families (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2920866A (en) * 1954-12-20 1960-01-12 A V Roe Canada Ltd Hollow air cooled sheet metal turbine blade
US3540810A (en) * 1966-03-17 1970-11-17 Gen Electric Slanted partition for hollow airfoil vane insert
US3963368A (en) * 1967-12-19 1976-06-15 General Motors Corporation Turbine cooling
US3560107A (en) * 1968-09-25 1971-02-02 Gen Motors Corp Cooled airfoil
US3698834A (en) * 1969-11-24 1972-10-17 Gen Motors Corp Transpiration cooling
BE755567A (fr) * 1969-12-01 1971-02-15 Gen Electric Structure d'aube fixe, pour moteur a turbines a gaz et arrangement de reglage de temperature associe
GB1304678A (en:Method) * 1971-06-30 1973-01-24
US3726604A (en) * 1971-10-13 1973-04-10 Gen Motors Corp Cooled jet flap vane
US3806275A (en) * 1972-08-30 1974-04-23 Gen Motors Corp Cooled airfoil
US3806276A (en) * 1972-08-30 1974-04-23 Gen Motors Corp Cooled turbine blade
CH584347A5 (en:Method) * 1974-11-08 1977-01-31 Bbc Sulzer Turbomaschinen
US4153386A (en) * 1974-12-11 1979-05-08 United Technologies Corporation Air cooled turbine vanes

Also Published As

Publication number Publication date
GB1565743A (en) 1980-04-23
US4086021A (en) 1978-04-25
SE7600473L (sv) 1977-07-20
SE395934B (sv) 1977-08-29

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PL Patent ceased
PL Patent ceased