NL262125A - - Google Patents

Info

Publication number
NL262125A
NL262125A NL262125DA NL262125A NL 262125 A NL262125 A NL 262125A NL 262125D A NL262125D A NL 262125DA NL 262125 A NL262125 A NL 262125A
Authority
NL
Netherlands
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 NL262125A publication Critical patent/NL262125A/xx
Priority claimed from CH37161A external-priority patent/CH391385A/de

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
    • F02K1/1261—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 substantially axially movable structure
    • 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
    • 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
NL262125D 1960-04-01 NL262125A (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US19421A US3098352A (en) 1960-04-01 1960-04-01 Adjustable jet propulsion nozzle with secondary air flow control
CH37161A CH391385A (de) 1961-01-12 1961-01-12 Einstellbare Schubdüse

Publications (1)

Publication Number Publication Date
NL262125A true NL262125A (fr)

Family

ID=25684374

Family Applications (1)

Application Number Title Priority Date Filing Date
NL262125D NL262125A (fr) 1960-04-01

Country Status (5)

Country Link
US (1) US3098352A (fr)
CH (1) CH412474A (fr)
FR (1) FR1280852A (fr)
GB (1) GB907526A (fr)
NL (1) NL262125A (fr)

Families Citing this family (26)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB985192A (en) * 1960-05-13 1965-03-03 Bristol Siddeley Engines Ltd Improvements in aircraft propulsion power plants
US3229457A (en) * 1962-10-15 1966-01-18 James R Rowe Variable area ratio rocket nozzle
DE1262682B (de) * 1963-08-22 1968-03-07 Rolls Royce Mantelstromgasturbinentriebwerk
US3258913A (en) * 1963-09-20 1966-07-05 Boeing Co Method and apparatus for varying the area of an air flow device
GB1008322A (en) * 1964-08-04 1965-10-27 Rolls Royce Gas turbine engine
GB1068746A (en) * 1964-11-27 1967-05-10 Rolls Royce Jet propulsion engine
US3662957A (en) * 1970-10-28 1972-05-16 United Aircraft Corp Low friction track bearing assembly
US3897001A (en) * 1974-06-12 1975-07-29 Gen Electric Nozzle and auxiliary inlet arrangement for gas turbine engine
US4074523A (en) * 1976-12-08 1978-02-21 The United States Of America As Represented By The Secretary Of The Air Force Pressure actuated collapsible curtain liners for a gas turbine engine nozzle
US4587806A (en) * 1981-05-11 1986-05-13 United Technologies Corporation Area two-dimensional converging/diverging nozzle
FR2608680B1 (fr) * 1986-12-17 1989-03-17 Snecma Tuyere bidimensionnelle reglable, notamment pour reacteur d'avion
FR2637017B1 (fr) * 1988-09-28 1990-11-30 Snecma Structure de tuyere pour propulseur combine turbo-stato-fusee
FR2670177B1 (fr) * 1990-12-05 1993-01-22 Snecma Joint d'etancheite entre l'arriere du fuselage d'un avion et les volets exterieurs de son turboreacteur.
US5351888A (en) * 1993-05-14 1994-10-04 General Electric Company Multi-axis vectorable exhaust nozzle
US5431344A (en) * 1993-11-12 1995-07-11 United Technologies Corporation Sliding throat gas turbine engine nozzle
FR2715192B1 (fr) * 1994-01-20 1996-02-16 Snecma Tuyère d'éjection de turboréacteur.
FR2790791B1 (fr) * 1999-03-10 2001-04-13 Snecma Tuyere d'ejection de turboreacteur axisymetrique et a orientation globale
US8572986B2 (en) * 2009-07-27 2013-11-05 United Technologies Corporation Retainer for suspended thermal protection elements in a gas turbine engine
AU2012222857B2 (en) * 2011-03-01 2016-02-25 Grollo Aerospace Engine for use in an aerial vehicle
US9581109B1 (en) * 2013-04-11 2017-02-28 Geoffrey P. Pinto Axially translating and radially tilting fan nozzle segments with combined actuation and position sensing
US10464668B2 (en) 2015-09-02 2019-11-05 Jetoptera, Inc. Configuration for vertical take-off and landing system for aerial vehicles
USD868627S1 (en) 2018-04-27 2019-12-03 Jetoptera, Inc. Flying car
ES2964957T3 (es) 2015-09-02 2024-04-10 Jetoptera Inc Sistema de propulsión fluídica
GB2588651A (en) 2019-10-31 2021-05-05 Rolls Royce Plc An exhaust nozzle
GB2588652A (en) 2019-10-31 2021-05-05 Rolls Royce Plc An exhaust nozzle
GB2588653A (en) * 2019-10-31 2021-05-05 Rolls Royce Plc An exhaust nozzle

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2729937A (en) * 1951-03-20 1956-01-10 United Aircraft Corp Retractable flameholders for afterburners
US2770944A (en) * 1952-04-26 1956-11-20 United Aircraft Corp Variable area reaction nozzle movable from convergent to convergent-di-vergent form
GB733383A (en) * 1953-02-05 1955-07-13 British Thomson Houston Co Ltd Improvements in and relating to fuel-reaction-chambers
FR1006139A (fr) * 1954-11-25 1952-04-21 Cem Comp Electro Mec Procédé et dispositif de réglage des turbo-réacteurs
US2910828A (en) * 1956-08-24 1959-11-03 United Aircraft Company Convergent-divergent variable area propulsion nozzle
GB872195A (en) * 1957-05-21 1961-07-05 English Electric Co Ltd Improvements in and relating to jet propulsion nozzles
US3049873A (en) * 1958-02-04 1962-08-21 Westinghouse Electric Corp Exhaust nozzle having a flow area of variable convergency and divergency
US2984068A (en) * 1958-06-30 1961-05-16 Orenda Engines Ltd Propulsive nozzle system for reaction propulsion units

Also Published As

Publication number Publication date
US3098352A (en) 1963-07-23
CH412474A (de) 1966-04-30
FR1280852A (fr) 1962-01-08
GB907526A (en) 1962-10-03

Similar Documents

Publication Publication Date Title
FR1310193A (fr)
DE1213246C2 (fr)
DE1234064C2 (fr)
FR88707E (fr)
FR127825A (fr)
DE1252378B (fr)
JPS3922688B1 (fr)
FR864M (fr)
FI42447B (fr)
FI40354B (fr)
FR927M (fr)
FR860M (fr)
FR837M (fr)
FR80805E (fr)
NL120092C (fr)
FR1599655A (fr)
FI48146B (fr)
FI46274B (fr)
DE1608578A1 (fr)
LU40158A1 (fr)
NL120080C (fr)
BE606151A (fr)
BE608910A (fr)
NL262125A (fr)
BE611467A (fr)