IT963220B - VANEL ON EDGE WITH BEVELLED ENTRANCE FOR NOISE REDUCTION COLARLY PARTS FOR TURBOVEN TILATOR REACTORS - Google Patents

VANEL ON EDGE WITH BEVELLED ENTRANCE FOR NOISE REDUCTION COLARLY PARTS FOR TURBOVEN TILATOR REACTORS

Info

Publication number
IT963220B
IT963220B IT27244/72A IT2724472A IT963220B IT 963220 B IT963220 B IT 963220B IT 27244/72 A IT27244/72 A IT 27244/72A IT 2724472 A IT2724472 A IT 2724472A IT 963220 B IT963220 B IT 963220B
Authority
IT
Italy
Prior art keywords
turboven
colarly
vanel
tilator
reactors
Prior art date
Application number
IT27244/72A
Other languages
Italian (it)
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
Application granted granted Critical
Publication of IT963220B publication Critical patent/IT963220B/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
    • 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
    • F02C7/045—Air intakes for gas-turbine plants or jet-propulsion plants having provisions for noise suppression
    • 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
    • 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
    • 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)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
IT27244/72A 1971-11-01 1972-07-21 VANEL ON EDGE WITH BEVELLED ENTRANCE FOR NOISE REDUCTION COLARLY PARTS FOR TURBOVEN TILATOR REACTORS IT963220B (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US19428571A 1971-11-01 1971-11-01

Publications (1)

Publication Number Publication Date
IT963220B true IT963220B (en) 1974-01-10

Family

ID=22716999

Family Applications (1)

Application Number Title Priority Date Filing Date
IT27244/72A IT963220B (en) 1971-11-01 1972-07-21 VANEL ON EDGE WITH BEVELLED ENTRANCE FOR NOISE REDUCTION COLARLY PARTS FOR TURBOVEN TILATOR REACTORS

Country Status (6)

Country Link
JP (1) JPS4853306A (en)
BE (1) BE787047A (en)
DE (1) DE2237154A1 (en)
FR (1) FR2158179B1 (en)
GB (1) GB1404665A (en)
IT (1) IT963220B (en)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE10064271A1 (en) * 2000-12-22 2002-07-04 Alstom Switzerland Ltd Device for impingement cooling of a component which is exposed to heat in a turbo engine and method therefor
DE102007002518B3 (en) * 2007-01-17 2008-07-31 Air Fertigung-Technologie Gmbh & Co.Kg Vane for e.g. water turbine, of ship machine, has blowing medium formed between cover and carrying structure, where measures are met to enable transfer of blowing medium from side of vane blade to other side of blade
CN111042922B (en) * 2019-12-27 2024-09-20 中国科学技术大学 Air inlet channel

Family Cites Families (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1872749A (en) * 1930-12-06 1932-08-23 Karageorge James Fan blade
US3347520A (en) * 1966-07-12 1967-10-17 Jerzy A Oweczarek Turbomachine blading

Also Published As

Publication number Publication date
FR2158179B1 (en) 1976-10-29
FR2158179A1 (en) 1973-06-15
DE2237154A1 (en) 1973-05-10
JPS4853306A (en) 1973-07-26
GB1404665A (en) 1975-09-03
BE787047A (en) 1972-12-01

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