IT8424117A0 - INPUT GUIDE BLADE ESPECIALLY FOR AGAS TURBO ENGINES. - Google Patents

INPUT GUIDE BLADE ESPECIALLY FOR AGAS TURBO ENGINES.

Info

Publication number
IT8424117A0
IT8424117A0 IT8424117A IT2411784A IT8424117A0 IT 8424117 A0 IT8424117 A0 IT 8424117A0 IT 8424117 A IT8424117 A IT 8424117A IT 2411784 A IT2411784 A IT 2411784A IT 8424117 A0 IT8424117 A0 IT 8424117A0
Authority
IT
Italy
Prior art keywords
agas
guide blade
input guide
turbo engines
blade especially
Prior art date
Application number
IT8424117A
Other languages
Italian (it)
Inventor
George Steele Irons
John Paul Petrowicz
Verna E Irons
Original Assignee
Gen Electric
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 Gen Electric filed Critical Gen Electric
Publication of IT8424117A0 publication Critical patent/IT8424117A0/en

Links

Classifications

    • 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
    • F02C9/00—Controlling gas-turbine plants; Controlling fuel supply in air- breathing jet-propulsion plants
    • F02C9/16—Control of working fluid flow
    • F02C9/20—Control of working fluid flow by throttling; by adjusting vanes
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
IT8424117A 1983-12-27 1984-12-18 INPUT GUIDE BLADE ESPECIALLY FOR AGAS TURBO ENGINES. IT8424117A0 (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US56607983A 1983-12-27 1983-12-27

Publications (1)

Publication Number Publication Date
IT8424117A0 true IT8424117A0 (en) 1984-12-18

Family

ID=24261385

Family Applications (1)

Application Number Title Priority Date Filing Date
IT8424117A IT8424117A0 (en) 1983-12-27 1984-12-18 INPUT GUIDE BLADE ESPECIALLY FOR AGAS TURBO ENGINES.

Country Status (6)

Country Link
JP (1) JPS60175706A (en)
CA (1) CA1237587A (en)
DE (1) DE3446206A1 (en)
FR (1) FR2557201A1 (en)
GB (1) GB2152150A (en)
IT (1) IT8424117A0 (en)

Families Citing this family (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4883404A (en) * 1988-03-11 1989-11-28 Sherman Alden O Gas turbine vanes and methods for making same
US5197852A (en) * 1990-05-31 1993-03-30 General Electric Company Nozzle band overhang cooling
JP3068227B2 (en) * 1991-03-25 2000-07-24 三菱重工業株式会社 Aircraft engine
US5220785A (en) * 1991-07-15 1993-06-22 United Technologies Corporation Side discharge anti-ice manifold
EP1167689A1 (en) * 2000-06-21 2002-01-02 Siemens Aktiengesellschaft Configuration of a coolable turbine blade
JP5344165B2 (en) * 2009-07-14 2013-11-20 株式会社Ｉｈｉ Gas turbine engine
FR2980537B1 (en) * 2011-09-26 2015-04-24 Snecma DAWN FOR TURBOMACHINE AND METHOD FOR MANUFACTURING SUCH A DAWN
CN102418603A (en) * 2011-10-19 2012-04-18 中国航空动力机械研究所 Blade anti-icing device and blade anti-icing system with same
US9322291B2 (en) 2012-12-14 2016-04-26 United Technologies Corporation Anti-ice supply system for inlet guide vanes
GB201416928D0 (en) * 2014-09-25 2014-11-12 Rolls Royce Plc A gas turbine and a method of washing a gas turbine engine
FR3028494B1 (en) * 2014-11-17 2018-05-25 Safran Aircraft Engines TURBOMACHINE BLADE, COMPRISING PONTETS EXTENDING FROM THE WALL OF INTRADOS TO THE WALL OF EXTRADOS
GB2553331A (en) * 2016-09-02 2018-03-07 Rolls Royce Plc Gas turbine engine
CN106762147B (en) * 2017-02-22 2019-04-23 中国航发沈阳发动机研究所 A kind of engine anti-icing system
RU177516U1 (en) * 2017-07-21 2018-02-28 Научно-производственная ассоциация "Технопарк Авиационных Технологий" Paddle for adjustable inlet guide vane
CN108591123B (en) * 2018-05-24 2023-07-21 中国科学院工程热物理研究所 Compressor inlet guide vane structure with gas heat anti-icing function
CN113530888B (en) * 2021-08-24 2022-08-09 中国航发湖南动力机械研究所 Multi-cavity integrated guide vane casing structure with anti-icing function

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB669130A (en) * 1949-08-22 1952-03-26 Rolls Royce Improvements in precision casting
FR1307299A (en) * 1961-09-11 1962-10-26 Creusot Forges Ateliers Manufacturing process of refractory molds for precision foundry
FR2476207A1 (en) * 1980-02-19 1981-08-21 Snecma IMPROVEMENT TO AUBES OF COOLED TURBINES

Also Published As

Publication number Publication date
CA1237587A (en) 1988-06-07
DE3446206A1 (en) 1985-07-11
JPS60175706A (en) 1985-09-09
GB2152150A (en) 1985-07-31
GB8428338D0 (en) 1984-12-19
FR2557201A1 (en) 1985-06-28

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