FR1075062A - Improvements made to jet engines, in particular to heated turbo-reactors, with adjustable outlet section nozzle - Google Patents

Improvements made to jet engines, in particular to heated turbo-reactors, with adjustable outlet section nozzle

Info

Publication number
FR1075062A
FR1075062A FR1075062DA FR1075062A FR 1075062 A FR1075062 A FR 1075062A FR 1075062D A FR1075062D A FR 1075062DA FR 1075062 A FR1075062 A FR 1075062A
Authority
FR
France
Prior art keywords
turbo
reactors
heated
outlet section
improvements made
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)
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.)
Societe dExplotation des Materiels Hispano Suiza
Original Assignee
Societe dExplotation des Materiels Hispano Suiza
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 Societe dExplotation des Materiels Hispano Suiza filed Critical Societe dExplotation des Materiels Hispano Suiza
Application granted granted Critical
Publication of FR1075062A publication Critical patent/FR1075062A/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
    • F02K1/78—Other construction of jet pipes
    • F02K1/80—Couplings or connections
    • F02K1/805—Sealing devices therefor, e.g. for movable parts of jet pipes or nozzle flaps
    • 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
    • F02K1/11—Varying effective area of jet pipe or nozzle by means of pivoted eyelids
FR1075062D 1953-02-26 1953-02-26 Improvements made to jet engines, in particular to heated turbo-reactors, with adjustable outlet section nozzle Expired FR1075062A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1075062T 1953-02-26

Publications (1)

Publication Number Publication Date
FR1075062A true FR1075062A (en) 1954-10-12

Family

ID=9606939

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1075062D Expired FR1075062A (en) 1953-02-26 1953-02-26 Improvements made to jet engines, in particular to heated turbo-reactors, with adjustable outlet section nozzle

Country Status (1)

Country Link
FR (1) FR1075062A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1045734B (en) * 1955-02-11 1958-12-04 United Aircraft Corp Thrust nozzle with changeable area for a guide channel with a number of nozzle flaps
FR2604482A1 (en) * 1986-09-25 1988-04-01 Fage Etienne THRUST INVERTER FOR AIRCRAFT REACTION ENGINE AND AIRCRAFT ENGINE EQUIPPED WITH SAID THRUST INVERTER
EP0744543A1 (en) * 1995-05-25 1996-11-27 United Technologies Corporation Cooled gas turbine engine augmentor

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1045734B (en) * 1955-02-11 1958-12-04 United Aircraft Corp Thrust nozzle with changeable area for a guide channel with a number of nozzle flaps
FR2604482A1 (en) * 1986-09-25 1988-04-01 Fage Etienne THRUST INVERTER FOR AIRCRAFT REACTION ENGINE AND AIRCRAFT ENGINE EQUIPPED WITH SAID THRUST INVERTER
EP0744543A1 (en) * 1995-05-25 1996-11-27 United Technologies Corporation Cooled gas turbine engine augmentor

Similar Documents

Publication Publication Date Title
CH324310A (en) Exhaust nozzle with variable cross-sectional area
FR1138877A (en) Improvements to jet thrusters
FR1075062A (en) Improvements made to jet engines, in particular to heated turbo-reactors, with adjustable outlet section nozzle
CH354627A (en) Adjustable propulsion nozzle
FR1099647A (en) Improvements to jet propelled planes
NL184560B (en) MANUAL NOZZLE.
FR1013507A (en) Improvements to variable section ejector nozzles ?? gas turbine engines
FR1105967A (en) Improvements to injection molding machines
FR1075063A (en) Improvements made to jet engines, especially those equipped with a heating system
FR1066580A (en) Improvements made to jet engines, in particular turbojets, equipped with a heating system
FR1131802A (en) forced exhaust by high speed air injection
FR1082598A (en) Improvement in jet thrusters
FR1117148A (en) Improvements relating to plastics
FR1051499A (en) Improvements relating to plastics
FR1066592A (en) Improvements made to jet engines, in particular turbojets, equipped with a heating system
FR1105799A (en) Variable section propellant nozzle
FR1091754A (en) Rotary jet engine
FR1167038A (en) Improvements relating to variable section nozzles
FR1075613A (en) Composite plane
FR1161189A (en) Jet engine
FR1108759A (en) Improvements to jet propulsion nozzles
FR64721E (en) Improvement in jet thrusters
FR1091899A (en) Advanced jet thruster
FR1035912A (en) Improvements to jet engines
FR1061781A (en) Advanced training in aerodynamic valve pulso-reactor groups