FR1199372A - Improved nozzle for turbo-reactors or similar - Google Patents

Improved nozzle for turbo-reactors or similar

Info

Publication number
FR1199372A
FR1199372A FR1199372DA FR1199372A FR 1199372 A FR1199372 A FR 1199372A FR 1199372D A FR1199372D A FR 1199372DA FR 1199372 A FR1199372 A FR 1199372A
Authority
FR
France
Prior art keywords
turbo
reactors
similar
improved nozzle
nozzle
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
Other languages
French (fr)
Inventor
Louis Duthion
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.)
Bertin Technologies SAS
Original Assignee
Bertin et Cie SA
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 Bertin et Cie SA filed Critical Bertin et Cie SA
Application granted granted Critical
Publication of FR1199372A publication Critical patent/FR1199372A/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
    • F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/36—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto having an ejector
    • 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
    • F02K1/06—Varying effective area of jet pipe or nozzle
    • F02K1/12—Varying effective area of jet pipe or nozzle by means of pivoted flaps
    • F02K1/1207—Varying effective area of jet pipe or nozzle by means of pivoted flaps of one series of flaps hinged at their upstream ends on a fixed structure

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
FR1199372D 1958-02-21 1958-02-21 Improved nozzle for turbo-reactors or similar Expired FR1199372A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1199372T 1958-02-21

Publications (1)

Publication Number Publication Date
FR1199372A true FR1199372A (en) 1959-12-14

Family

ID=9670440

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1199372D Expired FR1199372A (en) 1958-02-21 1958-02-21 Improved nozzle for turbo-reactors or similar

Country Status (1)

Country Link
FR (1) FR1199372A (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1205340B (en) * 1961-06-07 1965-11-18 Rolls Royce Thrust nozzle arrangement for jet engine systems in supersonic aircraft
US3630452A (en) * 1968-09-14 1971-12-28 Rolls Royce Variable-area exhaust nozzles for gas turbine engines
FR2368614A1 (en) * 1976-10-21 1978-05-19 Svischev Georgy Jet engine thrust increasing device - has supplementary nozzle which surrounds split coned end of engine jet pipe
FR2524937A1 (en) * 1982-04-07 1983-10-14 Nightingale Douglas VARIABLE GEOMETRY EJECTION TUBE FOR TURBOMACHINES

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1205340B (en) * 1961-06-07 1965-11-18 Rolls Royce Thrust nozzle arrangement for jet engine systems in supersonic aircraft
US3630452A (en) * 1968-09-14 1971-12-28 Rolls Royce Variable-area exhaust nozzles for gas turbine engines
FR2368614A1 (en) * 1976-10-21 1978-05-19 Svischev Georgy Jet engine thrust increasing device - has supplementary nozzle which surrounds split coned end of engine jet pipe
FR2524937A1 (en) * 1982-04-07 1983-10-14 Nightingale Douglas VARIABLE GEOMETRY EJECTION TUBE FOR TURBOMACHINES

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