BE537645A - - Google Patents

Info

Publication number
BE537645A
BE537645A BE537645DA BE537645A BE 537645 A BE537645 A BE 537645A BE 537645D A BE537645D A BE 537645DA BE 537645 A BE537645 A BE 537645A
Authority
BE
Belgium
Application number
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.)
Publication of BE537645A publication Critical patent/BE537645A/xx

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
    • F02K1/09—Varying effective area of jet pipe or nozzle by axially moving an external member, e.g. a shroud
    • 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
    • F02K1/04—Mounting of an exhaust cone in the jet pipe
    • 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
    • F02K1/52—Nozzles specially constructed for positioning adjacent to another nozzle or to a fixed member, e.g. fairing

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Nozzles (AREA)
BE537645D 1954-06-10 BE537645A (xx)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB17153/54A GB772363A (en) 1954-06-10 1954-06-10 Improvements in or relating to jet propulsion nozzles

Publications (1)

Publication Number Publication Date
BE537645A true BE537645A (xx)

Family

ID=10090219

Family Applications (1)

Application Number Title Priority Date Filing Date
BE537645D BE537645A (xx) 1954-06-10

Country Status (4)

Country Link
US (1) US2928235A (xx)
BE (1) BE537645A (xx)
FR (1) FR1131513A (xx)
GB (1) GB772363A (xx)

Families Citing this family (21)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB872195A (en) * 1957-05-21 1961-07-05 English Electric Co Ltd Improvements in and relating to jet propulsion nozzles
US3094072A (en) * 1957-12-09 1963-06-18 Arthur R Parilla Aircraft, missiles, missile weapons systems, and space ships
US3112612A (en) * 1958-07-21 1963-12-03 Gen Electric Rocket motor
US3060679A (en) * 1958-10-24 1962-10-30 Gen Electric Powerplant
US3080711A (en) * 1960-01-06 1963-03-12 James F Connors Penshape exhaust nozzle for supersonic engine
GB918189A (en) * 1960-07-01 1963-02-13 Rolls Royce Jet propulsion nozzle
US3156437A (en) * 1960-09-02 1964-11-10 S F E R M A Soc Fr D Entretien Fluid flow straightening device in a propelled body
DE1209810B (de) * 1961-11-27 1966-01-27 Rolls Royce Abgasleitung fuer Gasturbinenstrahltriebwerke
US3237864A (en) * 1962-12-03 1966-03-01 Gen Electric Low drag variable plug jet exhaust nozzle
GB1008322A (en) * 1964-08-04 1965-10-27 Rolls Royce Gas turbine engine
GB1009776A (en) * 1964-08-25 1965-11-10 Rolls Royce Supersonic jet propulsion nozzle
US3390837A (en) * 1965-12-08 1968-07-02 Gen Electric Convergent-divergent plug nozzle having a plurality of freely-floating tandem flaps
US4527388A (en) * 1982-07-12 1985-07-09 The Garrett Corporation Jet propulsion apparatus and methods
GB2236804A (en) * 1989-07-26 1991-04-17 Anthony Reginald Robins Compound nozzle
US6178740B1 (en) * 1999-02-25 2001-01-30 The Boeing Company Turbo fan engine nacelle exhaust system with concave primary nozzle plug
US6629416B1 (en) * 2002-04-25 2003-10-07 The United States Of America As Represented By The Secretary Of The Navy Afterburning aerospike rocket nozzle
GB2518942A (en) * 2013-07-24 2015-04-08 Snecma Biconical exhaust cone for a civil aviation jet engine
FR3009026B1 (fr) * 2013-07-24 2018-01-05 Safran Aircraft Engines Corps central d'echappement pour une turbomachine
US20200080435A1 (en) * 2018-09-10 2020-03-12 Pratt & Whitney Canada Corp. Turbine exhaust structure for a gas turbine engine
US11028778B2 (en) 2018-09-27 2021-06-08 Pratt & Whitney Canada Corp. Engine with start assist
US11512669B2 (en) * 2020-06-24 2022-11-29 Raytheon Company Distributed airfoil aerospike rocket nozzle

Family Cites Families (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR47412E (fr) * 1938-07-05 1937-05-05 Procédé de transformation de l'énergie calorifique en énergie cinétique ou potentielle
US2427845A (en) * 1941-07-08 1947-09-23 Fairey Aviat Co Ltd Periodically actuated jet motor
US2420323A (en) * 1943-07-21 1947-05-13 Westinghouse Electric Corp Wing-mounted jet-propulsion system with controllable discharge outlet
FR994841A (fr) * 1945-02-06 1951-11-22 Rateau Soc Dispositif de réglage de la section de sortie de la tuyère d'un propulseur à réaction
NL70849C (xx) * 1945-05-14
US2570629A (en) * 1945-10-05 1951-10-09 Anxionnaz Adjustable pipe for the intake of air and expansion of the driving gases in reactionjet propellers for projectiles and vehicles
US2523378A (en) * 1945-11-28 1950-09-26 Kollsman Paul Wing-mounted jet reaction engine for aircraft
US2481330A (en) * 1946-08-06 1949-09-06 Gen Electric Variable jet nozzle
BE498317A (xx) * 1949-10-06
NL161099C (nl) * 1951-05-10 1900-01-01 Tecalemit Group Services Limit Inrichting voor het smeren van een voertuig af- hankelijk van de afgelegde weg.
US2753685A (en) * 1951-08-02 1956-07-10 Rolls Royce Gas turbine engine with exhaust gas heating means

Also Published As

Publication number Publication date
US2928235A (en) 1960-03-15
GB772363A (en) 1957-04-10
FR1131513A (fr) 1957-02-22

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