IT1007077B - Turbina a gas perfezionata per volo subsonico - Google Patents

Turbina a gas perfezionata per volo subsonico

Info

Publication number
IT1007077B
IT1007077B IT19780/74A IT1978074A IT1007077B IT 1007077 B IT1007077 B IT 1007077B IT 19780/74 A IT19780/74 A IT 19780/74A IT 1978074 A IT1978074 A IT 1978074A IT 1007077 B IT1007077 B IT 1007077B
Authority
IT
Italy
Prior art keywords
perfected
gas turbine
subsonic flight
subsonic
flight
Prior art date
Application number
IT19780/74A
Other languages
English (en)
Italian (it)
Original Assignee
United Aircraft Corp
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 United Aircraft Corp filed Critical United Aircraft Corp
Application granted granted Critical
Publication of IT1007077B publication Critical patent/IT1007077B/it

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K3/00—Plants including a gas turbine driving a compressor or a ducted fan
    • F02K3/02—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber
    • F02K3/04—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type
    • F02K3/06—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type with front fan
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • 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)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Control Of Turbines (AREA)
IT19780/74A 1973-02-08 1974-01-25 Turbina a gas perfezionata per volo subsonico IT1007077B (it)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US33079273A 1973-02-08 1973-02-08

Publications (1)

Publication Number Publication Date
IT1007077B true IT1007077B (it) 1976-10-30

Family

ID=23291354

Family Applications (1)

Application Number Title Priority Date Filing Date
IT19780/74A IT1007077B (it) 1973-02-08 1974-01-25 Turbina a gas perfezionata per volo subsonico

Country Status (6)

Country Link
JP (1) JPS49111014A (enrdf_load_stackoverflow)
CA (1) CA986319A (enrdf_load_stackoverflow)
DE (1) DE2401212C2 (enrdf_load_stackoverflow)
FR (1) FR2217559B1 (enrdf_load_stackoverflow)
GB (1) GB1447144A (enrdf_load_stackoverflow)
IT (1) IT1007077B (enrdf_load_stackoverflow)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2236804A (en) * 1989-07-26 1991-04-17 Anthony Reginald Robins Compound nozzle
FR2983917B1 (fr) * 2011-12-07 2013-12-27 Snecma Tuyere convergente-divergente de turbomachine

Family Cites Families (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3044258A (en) * 1958-11-25 1962-07-17 Gen Electric Adjustable converging-diverging nozzle
US3520138A (en) * 1969-02-27 1970-07-14 United Aircraft Corp Convertible enginf

Also Published As

Publication number Publication date
CA986319A (en) 1976-03-30
FR2217559A1 (enrdf_load_stackoverflow) 1974-09-06
DE2401212A1 (de) 1974-08-15
GB1447144A (en) 1976-08-25
JPS49111014A (enrdf_load_stackoverflow) 1974-10-23
FR2217559B1 (enrdf_load_stackoverflow) 1977-08-19
DE2401212C2 (de) 1983-08-18

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