Nothing Special   »   [go: up one dir, main page]

FR1018650A - Adjustable ejection nozzle for jet thrusters, including aerodyne engines - Google Patents

Adjustable ejection nozzle for jet thrusters, including aerodyne engines

Info

Publication number
FR1018650A
FR1018650A FR1018650DA FR1018650A FR 1018650 A FR1018650 A FR 1018650A FR 1018650D A FR1018650D A FR 1018650DA FR 1018650 A FR1018650 A FR 1018650A
Authority
FR
France
Prior art keywords
aerodyne
engines
ejection nozzle
adjustable ejection
jet thrusters
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
Hermann Oestrich
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 filed Critical
Application granted granted Critical
Publication of FR1018650A publication Critical patent/FR1018650A/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
    • F02K1/06—Varying effective area of jet pipe or nozzle
    • F02K1/12—Varying effective area of jet pipe or nozzle by means of pivoted flaps
    • 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)
FR1018650D 1950-03-14 1950-03-14 Adjustable ejection nozzle for jet thrusters, including aerodyne engines Expired FR1018650A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1018650T 1950-03-14

Publications (1)

Publication Number Publication Date
FR1018650A true FR1018650A (en) 1953-01-09

Family

ID=9575160

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1018650D Expired FR1018650A (en) 1950-03-14 1950-03-14 Adjustable ejection nozzle for jet thrusters, including aerodyne engines

Country Status (1)

Country Link
FR (1) FR1018650A (en)

Cited By (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1035976B (en) * 1952-10-25 1958-08-07 United Aircraft Corp Thrust nozzle of variable cross-section
US2846844A (en) * 1956-01-24 1958-08-12 Ryan Aeronautical Co Variable area thrust deflectoraugmenter for jet engines
US2870602A (en) * 1956-02-13 1959-01-27 Robert G Glenn Afterburner exhaust nozzle variable area
US2931169A (en) * 1956-05-15 1960-04-05 Westinghouse Electric Corp Variable convergent-divergent exhaust nozzle
US2932164A (en) * 1955-08-03 1960-04-12 Lockheed Aircraft Corp Thrust reverser and control mechanism therefor
US2969641A (en) * 1955-10-17 1961-01-31 Gen Electric Aerodynamic nozzle
US2972226A (en) * 1955-10-06 1961-02-21 United Aircraft Corp Variable area converging-diverging nozzle
US3028730A (en) * 1956-07-30 1962-04-10 Bristol Siddeley Engines Ltd Propulsion nozzles
US3068644A (en) * 1955-06-28 1962-12-18 Gen Electric Aerodynamic jet nozzle
US3081596A (en) * 1953-05-25 1963-03-19 Curtiss Wright Corp Variable area nozzle and shroud combination

Cited By (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1035976B (en) * 1952-10-25 1958-08-07 United Aircraft Corp Thrust nozzle of variable cross-section
US3081596A (en) * 1953-05-25 1963-03-19 Curtiss Wright Corp Variable area nozzle and shroud combination
US3068644A (en) * 1955-06-28 1962-12-18 Gen Electric Aerodynamic jet nozzle
US2932164A (en) * 1955-08-03 1960-04-12 Lockheed Aircraft Corp Thrust reverser and control mechanism therefor
US2972226A (en) * 1955-10-06 1961-02-21 United Aircraft Corp Variable area converging-diverging nozzle
US2969641A (en) * 1955-10-17 1961-01-31 Gen Electric Aerodynamic nozzle
US2846844A (en) * 1956-01-24 1958-08-12 Ryan Aeronautical Co Variable area thrust deflectoraugmenter for jet engines
US2870602A (en) * 1956-02-13 1959-01-27 Robert G Glenn Afterburner exhaust nozzle variable area
US2931169A (en) * 1956-05-15 1960-04-05 Westinghouse Electric Corp Variable convergent-divergent exhaust nozzle
US3028730A (en) * 1956-07-30 1962-04-10 Bristol Siddeley Engines Ltd Propulsion nozzles

Similar Documents

Publication Publication Date Title
FR999513A (en) Advanced nozzle for jet engines
FR1019001A (en) Exhaust port control device for jet engines
FR995173A (en) Propulsion nozzle for supersonic speeds
CH324032A (en) Jet thruster
FR994841A (en) Device for adjusting the outlet section of the jet thruster
CH294838A (en) Thrust jet nozzle.
FR998358A (en) Ejection nozzles for turbo-reactors
FR1018650A (en) Adjustable ejection nozzle for jet thrusters, including aerodyne engines
CA486078A (en) Exit area control for jet engines
FR1225736A (en) Adjustable nozzle for jet thruster
FR1077693A (en) Improvements to ejection nozzles for jet propulsion units
FR995748A (en) Flame stabilizers, in particular for post-combustion installations of aerodyne jet engines
CH357923A (en) Jet thruster fitted with a device for adjusting the section of the propellant jet
FR1004139A (en) Injection valve for rocket propulsion apparatus
FR1012341A (en) Improvements made to reactive nozzle devices, in particular to post-combustion turbomachines for aerodynes
FR1506309A (en) Adjustable nozzle for jet aircraft
FR1247562A (en) Jet Nozzles for Jet Engines
FR1063453A (en) Improvement in devices for adjusting the section of a nozzle, in particular a reactor nozzle
FR1007694A (en) Improvements to jet thrusters, especially those for aerodynes
AT182911B (en) Nozzle for jet propulsion (rockets)
FR1012004A (en) Improvements to jet thrusters, especially those for aerodynes
CH326310A (en) Jet propulsion nozzle
FR1013174A (en) Adjustable air injection jet, for agricultural sprayers
FR1025565A (en) Pressurized continuous jet injector
FR1078306A (en) Jet thruster