CH293778A - Hollow guide vane for turbo machinery. - Google Patents

Hollow guide vane for turbo machinery.

Info

Publication number
CH293778A
CH293778A CH293778DA CH293778A CH 293778 A CH293778 A CH 293778A CH 293778D A CH293778D A CH 293778DA CH 293778 A CH293778 A CH 293778A
Authority
CH
Switzerland
Prior art keywords
guide vane
hollow guide
turbo machinery
turbo
machinery
Prior art date
Application number
Other languages
German (de)
Inventor
Limited Rolls-Royce
Original Assignee
Rolls Royce
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 Rolls Royce filed Critical Rolls Royce
Publication of CH293778A publication Critical patent/CH293778A/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
    • F01D5/186—Film cooling
    • 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
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/04—Air intakes for gas-turbine plants or jet-propulsion plants
    • F02C7/047—Heating to prevent icing
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
CH293778D 1949-11-22 1950-11-21 Hollow guide vane for turbo machinery. CH293778A (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
GB293778X 1949-11-22
GB61150X 1950-11-06

Publications (1)

Publication Number Publication Date
CH293778A true CH293778A (en) 1953-10-15

Family

ID=26240444

Family Applications (1)

Application Number Title Priority Date Filing Date
CH293778D CH293778A (en) 1949-11-22 1950-11-21 Hollow guide vane for turbo machinery.

Country Status (3)

Country Link
CH (1) CH293778A (en)
FR (1) FR1027920A (en)
GB (1) GB685769A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3003347A1 (en) * 1979-12-20 1981-06-25 BBC AG Brown, Boveri & Cie., Baden, Aargau COOLED WALL
US5394687A (en) * 1993-12-03 1995-03-07 The United States Of America As Represented By The Department Of Energy Gas turbine vane cooling system

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
BE557503A (en) * 1956-05-15
DE1185415B (en) * 1962-02-03 1965-01-14 Gasturbinenbau Und Energiemasc Device for cooling turbine disks of a gas turbine
US3301527A (en) * 1965-05-03 1967-01-31 Gen Electric Turbine diaphragm structure
US3700348A (en) * 1968-08-13 1972-10-24 Gen Electric Turbomachinery blade structure
BR112015032787A2 (en) 2013-07-19 2017-08-22 Gen Electric TURBINE NOZZLE APPLIANCE

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3003347A1 (en) * 1979-12-20 1981-06-25 BBC AG Brown, Boveri & Cie., Baden, Aargau COOLED WALL
US5394687A (en) * 1993-12-03 1995-03-07 The United States Of America As Represented By The Department Of Energy Gas turbine vane cooling system

Also Published As

Publication number Publication date
GB685769A (en) 1953-01-14
FR1027920A (en) 1953-05-18

Similar Documents

Publication Publication Date Title
CH286626A (en) Blade for flow machines.
CH344800A (en) Turbo machine
CH266970A (en) Rotor for turbo machinery.
CH288242A (en) Axial flow machine.
CH268031A (en) Guide vane arrangement in gas turbines.
CH320493A (en) Turbine guide vane
CH298241A (en) Turbo-machine rotor.
CH272917A (en) Turbomachine rotor.
CH270936A (en) Turbomachine rotor.
CH282188A (en) Axial type gas turbine.
CH284189A (en) Axial turbine.
CH248083A (en) Rotor for turbo machines.
CH257531A (en) Runner for multi-stage turbo machines.
CH301451A (en) Lubricant.
CH274953A (en) Bearings.
CH293778A (en) Hollow guide vane for turbo machinery.
CH294839A (en) Turbojet.
CH306452A (en) Turbomachine with adjustable guide vanes.
CH275238A (en) Rotor for axial flow machines.
CH281555A (en) Gas turbine plant.
CH277706A (en) Missile detonators.
CH288841A (en) Combustion device for gas turbine plants.
CH285757A (en) Underwear for women.
AT172229B (en) Speed regulators, in particular for injection pumps
CH292526A (en) Blade carrier.