CH354627A - Tuyère de propulsion réglable - Google Patents

Tuyère de propulsion réglable

Info

Publication number
CH354627A
CH354627A CH354627DA CH354627A CH 354627 A CH354627 A CH 354627A CH 354627D A CH354627D A CH 354627DA CH 354627 A CH354627 A CH 354627A
Authority
CH
Switzerland
Prior art keywords
propulsion nozzle
adjustable propulsion
adjustable
nozzle
propulsion
Prior art date
Application number
Other languages
English (en)
Inventor
Hirsch Brown William
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
Publication of CH354627A publication Critical patent/CH354627A/fr

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
    • 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)
  • Nozzles (AREA)
  • Quick-Acting Or Multi-Walled Pipe Joints (AREA)
  • Control Of Turbines (AREA)
CH354627D 1955-02-11 1956-02-09 Tuyère de propulsion réglable CH354627A (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US487677A US2928234A (en) 1955-02-11 1955-02-11 Exhaust nozzle

Publications (1)

Publication Number Publication Date
CH354627A true CH354627A (fr) 1961-05-31

Family

ID=23936697

Family Applications (1)

Application Number Title Priority Date Filing Date
CH354627D CH354627A (fr) 1955-02-11 1956-02-09 Tuyère de propulsion réglable

Country Status (5)

Country Link
US (1) US2928234A (fr)
CH (1) CH354627A (fr)
DE (1) DE1045734B (fr)
FR (1) FR1141221A (fr)
GB (1) GB826407A (fr)

Families Citing this family (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3024599A (en) * 1958-07-14 1962-03-13 Rolls Royce Variable area jet propulsion nozzles
FR1177253A (fr) * 1958-07-14 1959-04-22 Rolls Royce Perfectionnements apportés aux tuyères de propulsion à réaction à section variable
DE1230620B (de) * 1963-01-09 1966-12-15 Rolls Royce Vertikalhubtriebwerksanlage fuer Flugzeuge
US3243126A (en) * 1963-09-18 1966-03-29 United Aircraft Corp Variable area exhaust nozzle
US3690561A (en) * 1970-11-05 1972-09-12 Rohr Corp Thrust controlling system
US4311276A (en) * 1978-06-24 1982-01-19 Rolls-Royce Limited Variable area nozzle for a gas turbine engine
US9856956B2 (en) 2015-01-20 2018-01-02 United Technologies Corporation Rod-and-bracket connector system for securing a pivoting member to a guide anchor moveably secured within a guide track
GB201609071D0 (en) 2016-05-24 2016-07-06 Rolls Royce Plc Aircraft gas turbine engine nacelle
FR3082562B1 (fr) * 2018-06-19 2020-06-12 Safran Aircraft Engines Anneau de commande de portes de decharge pour une turbomachine d'aeronef et turbomachine le comportant

Family Cites Families (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1387364A (en) * 1920-09-30 1921-08-09 Dever Christy Johnson Pump-jack
US2569497A (en) * 1948-10-07 1951-10-02 Ervin E Schiesel Combined variable area nozzle and after-burner control for jet motors
US2697907A (en) * 1948-11-12 1954-12-28 Gen Motors Corp Multiplate variable area jet nozzle
US2693078A (en) * 1949-03-18 1954-11-02 Westinghouse Electric Corp Exhaust orifice control for jet engines
US2694289A (en) * 1949-10-14 1954-11-16 Gen Electric Control device for gas turbines having fluid injection augmentation systems
FR998358A (fr) * 1949-10-31 1952-01-17 Cem Comp Electro Mec Tuyères d'éjection pour turbo-réacteurs
US2778190A (en) * 1950-06-08 1957-01-22 Republic Aviat Corp Variable area nozzle for jet engines
FR1055997A (fr) * 1950-09-27 1954-02-23 Rolls Royce Perfectionnements aux appareillages de combustion des moteurs à combustion interne
US2682147A (en) * 1951-06-16 1954-06-29 Rohr Aircraft Corp Adjustable nozzle for exhaust gas
GB716385A (en) * 1951-12-06 1954-10-06 Havilland Engine Co Ltd Improvements in or relating to propulsion nozzle constructions for jet propulsion apparatus
US2770944A (en) * 1952-04-26 1956-11-20 United Aircraft Corp Variable area reaction nozzle movable from convergent to convergent-di-vergent form
FR1071851A (fr) * 1952-11-12 1954-09-06 Materiels Hispano Suiza S A So Perfectionnements apportés aux dispositifs pour le réglage de la section de sortie d'un conduit traversé par un fluide, notamment d'une tuyère de moteur à réaction
FR1075062A (fr) * 1953-02-26 1954-10-12 Materiels Hispano Suiza S A So Perfectionnements apportés aux moteurs à réaction, notamment aux turbo-réacteurs à rechauffe, à tuyère de section de sortie réglable

Also Published As

Publication number Publication date
US2928234A (en) 1960-03-15
DE1045734B (de) 1958-12-04
GB826407A (en) 1960-01-06
FR1141221A (fr) 1957-08-28

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