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CH288549A - Stator vane for a gas turbine. - Google Patents

Stator vane for a gas turbine.

Info

Publication number
CH288549A
CH288549A CH288549DA CH288549A CH 288549 A CH288549 A CH 288549A CH 288549D A CH288549D A CH 288549DA CH 288549 A CH288549 A CH 288549A
Authority
CH
Switzerland
Prior art keywords
gas turbine
stator vane
vane
stator
turbine
Prior art date
Application number
Other languages
French (fr)
Inventor
Limited Armstrong Sidde Motors
Original Assignee
Armstrong Siddeley Motors Ltd
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 Armstrong Siddeley Motors Ltd filed Critical Armstrong Siddeley Motors Ltd
Publication of CH288549A publication Critical patent/CH288549A/en

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
    • 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
    • F01D9/042—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector fixing blades to stators

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
CH288549D 1949-08-27 1950-07-18 Stator vane for a gas turbine. CH288549A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB288549X 1949-08-27

Publications (1)

Publication Number Publication Date
CH288549A true CH288549A (en) 1953-01-31

Family

ID=10282240

Family Applications (1)

Application Number Title Priority Date Filing Date
CH288549D CH288549A (en) 1949-08-27 1950-07-18 Stator vane for a gas turbine.

Country Status (4)

Country Link
BE (1) BE498667A (en)
CH (1) CH288549A (en)
FR (1) FR1021265A (en)
GB (1) GB666536A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0811753A1 (en) * 1996-06-06 1997-12-10 United Technologies Corporation Method and apparatus for replacing a vane assembly in a turbine engine

Families Citing this family (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2709893A (en) * 1949-08-06 1955-06-07 Laval Steam Turbine Co Gas turbine power plant with heat exchanger and cooling means
BE517285A (en) * 1952-02-13
GB723505A (en) * 1952-11-18 1955-02-09 Parsons & Marine Eng Turbine Improvements in or relating to turbine nozzles
GB753224A (en) * 1953-04-13 1956-07-18 Rolls Royce Improvements in or relating to blading for turbines or compressors
BE529252A (en) * 1953-06-01
DE1055884B (en) * 1954-03-02 1959-04-23 Bristol Aero Engines Ltd Flame tube for a combustion chamber of a gas turbine engine
US2956772A (en) * 1955-08-19 1960-10-18 John C Freche Liquid-spray cooling method
FR1177035A (en) * 1957-05-28 1959-04-20 Snecma Method and device for cooling machine parts
DE1174329B (en) * 1959-08-24 1964-07-23 Zakl Mech Im Gen K S Idler vane floor for steam or gas turbines
DE1210254B (en) * 1962-03-26 1966-02-03 Rolls Royce Gas turbine engine with cooled turbine blades
US3346235A (en) * 1963-12-23 1967-10-10 Papst Hermann Boundary layer control
US3301527A (en) * 1965-05-03 1967-01-31 Gen Electric Turbine diaphragm structure
US3341114A (en) * 1966-03-04 1967-09-12 Gen Electric Anti-icing means
US3365125A (en) * 1966-08-03 1968-01-23 Gen Motors Corp Turbomachinery
US4162136A (en) * 1974-04-05 1979-07-24 Rolls-Royce Limited Cooled blade for a gas turbine engine
FR2654463A1 (en) * 1989-11-15 1991-05-17 Snecma TURBOMACHINE STATOR ELEMENT.

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0811753A1 (en) * 1996-06-06 1997-12-10 United Technologies Corporation Method and apparatus for replacing a vane assembly in a turbine engine

Also Published As

Publication number Publication date
BE498667A (en)
FR1021265A (en) 1953-02-17
GB666536A (en) 1952-02-13

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