IT1068291B - BLADE OR BLADE FOR A GAS TURBINE ENGINE - Google Patents

BLADE OR BLADE FOR A GAS TURBINE ENGINE

Info

Publication number
IT1068291B
IT1068291B IT27790/76A IT2779076A IT1068291B IT 1068291 B IT1068291 B IT 1068291B IT 27790/76 A IT27790/76 A IT 27790/76A IT 2779076 A IT2779076 A IT 2779076A IT 1068291 B IT1068291 B IT 1068291B
Authority
IT
Italy
Prior art keywords
blade
gas turbine
turbine engine
engine
gas
Prior art date
Application number
IT27790/76A
Other languages
Italian (it)
Original Assignee
Rolls Royce 1971 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 Rolls Royce 1971 Ltd filed Critical Rolls Royce 1971 Ltd
Application granted granted Critical
Publication of IT1068291B publication Critical patent/IT1068291B/en

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
    • F01D9/00Stators
    • F01D9/02Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
    • F01D9/04Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2240/00Components
    • F05D2240/80Platforms for stationary or moving blades
    • F05D2240/81Cooled platforms

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
IT27790/76A 1975-10-02 1976-09-29 BLADE OR BLADE FOR A GAS TURBINE ENGINE IT1068291B (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB40245/75A GB1605219A (en) 1975-10-02 1975-10-02 Stator vane for a gas turbine engine

Publications (1)

Publication Number Publication Date
IT1068291B true IT1068291B (en) 1985-03-21

Family

ID=10413945

Family Applications (1)

Application Number Title Priority Date Filing Date
IT27790/76A IT1068291B (en) 1975-10-02 1976-09-29 BLADE OR BLADE FOR A GAS TURBINE ENGINE

Country Status (2)

Country Link
GB (1) GB1605219A (en)
IT (1) IT1068291B (en)

Families Citing this family (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2723144B1 (en) * 1984-11-29 1996-12-13 Snecma TURBINE DISTRIBUTOR
US5197852A (en) * 1990-05-31 1993-03-30 General Electric Company Nozzle band overhang cooling
WO2000012869A1 (en) * 1998-08-31 2000-03-09 Siemens Aktiengesellschaft Turbine guide blade
US6341939B1 (en) * 2000-07-31 2002-01-29 General Electric Company Tandem cooling turbine blade
EP1329593B1 (en) * 2002-01-17 2005-03-23 Siemens Aktiengesellschaft Turbine blade with a hot gas suporting platform and a mechanical load suporting platform
WO2012144242A1 (en) * 2011-04-19 2012-10-26 三菱重工業株式会社 Turbine stator vane and gas turbine
US8961134B2 (en) * 2011-06-29 2015-02-24 Siemens Energy, Inc. Turbine blade or vane with separate endwall

Also Published As

Publication number Publication date
GB1605219A (en) 1984-08-30

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