BE600698A - Jet diverter device - Google Patents

Jet diverter device

Info

Publication number
BE600698A
BE600698A BE600698A BE600698A BE600698A BE 600698 A BE600698 A BE 600698A BE 600698 A BE600698 A BE 600698A BE 600698 A BE600698 A BE 600698A BE 600698 A BE600698 A BE 600698A
Authority
BE
Belgium
Prior art keywords
diverter device
jet diverter
jet
diverter
Prior art date
Application number
BE600698A
Other languages
French (fr)
Inventor
Max Andre Jacques Morel
Louis Jules Bauger
Andre Anatole Augustin Bardin
Original Assignee
Snecma
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 Snecma filed Critical Snecma
Publication of BE600698A publication Critical patent/BE600698A/en

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
    • F02K1/28—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto using fluid jets to influence the jet flow
    • F02K1/32—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto using fluid jets to influence the jet flow for reversing thrust
    • 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
    • F02K1/54—Nozzles having means for reversing jet thrust
    • F02K1/64—Reversing fan flow
    • F02K1/70—Reversing fan flow using thrust reverser flaps or doors mounted on the fan housing
    • F02K1/72—Reversing fan flow using thrust reverser flaps or doors mounted on the fan housing the aft end of the fan housing being movable to uncover openings in the fan housing for the reversed flow
BE600698A 1960-03-07 1961-02-27 Jet diverter device BE600698A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR820594A FR1260040A (en) 1960-03-07 1960-03-07 Jet diverter device

Publications (1)

Publication Number Publication Date
BE600698A true BE600698A (en) 1961-08-28

Family

ID=8726538

Family Applications (1)

Application Number Title Priority Date Filing Date
BE600698A BE600698A (en) 1960-03-07 1961-02-27 Jet diverter device

Country Status (3)

Country Link
BE (1) BE600698A (en)
FR (1) FR1260040A (en)
GB (1) GB925010A (en)

Families Citing this family (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1386232A (en) * 1971-03-31 1975-03-05 Short Brothers & Harland Ltd Fluid propulsion systems
GB2189550A (en) * 1986-04-25 1987-10-28 Rolls Royce A gas turbine engine powerplant with flow control devices
FR2812035B1 (en) * 2000-07-24 2003-08-29 Hurel Dubois Avions IMPROVEMENTS ON DRIVE INVERTERS FOR JET ENGINES OF THE GRID TYPE
GB0321139D0 (en) 2003-09-10 2003-10-08 Short Brothers Plc A device
US9970387B2 (en) 2007-08-08 2018-05-15 Rohr, Inc. Variable area fan nozzle with bypass flow
US9759087B2 (en) 2007-08-08 2017-09-12 Rohr, Inc. Translating variable area fan nozzle providing an upstream bypass flow exit
US8109466B2 (en) 2008-06-23 2012-02-07 Rohr, Inc. Thrust reverser cascade assembly and AFT cascade ring with flow deflector portion
EP2278147B1 (en) * 2009-06-16 2014-06-25 Rohr, Inc. Translating variable area fan nozzle providing an upstream bypass flow exit
US8875486B2 (en) 2010-05-17 2014-11-04 Rohr, Inc. Guide system for nacelle assembly
US8511973B2 (en) 2010-06-23 2013-08-20 Rohr, Inc. Guide system for nacelle assembly
US9086034B2 (en) * 2011-10-13 2015-07-21 Rohr, Inc. Thrust reverser cascade assembly with flow deflection shelf
US9657686B2 (en) * 2013-05-06 2017-05-23 Rohr, Inc. System, apparatus, and method for a virtual blocker
DE102015203219A1 (en) * 2015-02-23 2016-08-25 Rolls-Royce Deutschland Ltd & Co Kg Engine cowling of a gas turbine with thrust reverser and adjustable in cross-section exhaust nozzle

Also Published As

Publication number Publication date
GB925010A (en) 1963-05-01
FR1260040A (en) 1961-05-05

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