CA986319A - Gas turbine engine for subsonic flight - Google Patents

Gas turbine engine for subsonic flight

Info

Publication number
CA986319A
CA986319A CA191,122A CA191122A CA986319A CA 986319 A CA986319 A CA 986319A CA 191122 A CA191122 A CA 191122A CA 986319 A CA986319 A CA 986319A
Authority
CA
Canada
Prior art keywords
gas turbine
turbine engine
subsonic flight
subsonic
flight
Prior art date
Legal status (The legal status 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 status listed.)
Expired
Application number
CA191,122A
Other versions
CA191122S (en
Inventor
Martin S. Slatkin
Vincent J. Disabato
David L. Motycka
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Raytheon Technologies Corp
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 CA986319A publication Critical patent/CA986319A/en
Expired legal-status Critical Current

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
CA191,122A 1973-02-08 1974-01-25 Gas turbine engine for subsonic flight Expired CA986319A (en)

Applications Claiming Priority (1)

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

Publications (1)

Publication Number Publication Date
CA986319A true CA986319A (en) 1976-03-30

Family

ID=23291354

Family Applications (1)

Application Number Title Priority Date Filing Date
CA191,122A Expired CA986319A (en) 1973-02-08 1974-01-25 Gas turbine engine for subsonic flight

Country Status (6)

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

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 (en) * 2011-12-07 2013-12-27 Snecma CONVERGENT-DIVERGENT TUYERE OF 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
FR2217559B1 (en) 1977-08-19
IT1007077B (en) 1976-10-30
GB1447144A (en) 1976-08-25
DE2401212A1 (en) 1974-08-15
FR2217559A1 (en) 1974-09-06
JPS49111014A (en) 1974-10-23
DE2401212C2 (en) 1983-08-18

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