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FR1260040A - Jet diverter device - Google Patents

Jet diverter device

Info

Publication number
FR1260040A
FR1260040A FR820594A FR820594A FR1260040A FR 1260040 A FR1260040 A FR 1260040A FR 820594 A FR820594 A FR 820594A FR 820594 A FR820594 A FR 820594A FR 1260040 A FR1260040 A FR 1260040A
Authority
FR
France
Prior art keywords
diverter device
jet diverter
jet
diverter
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
FR820594A
Other languages
French (fr)
Inventor
Max-Andre-Jacques Morel
Louis-Jules Bauger
Andre-Anatole-August Bardin
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.)
Safran Aircraft Engines SAS
Original Assignee
Societe Nationale dEtude et de Construction de Moteurs dAviation SNECMA
SNECMA SAS
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 Nationale dEtude et de Construction de Moteurs dAviation SNECMA, SNECMA SAS filed Critical Societe Nationale dEtude et de Construction de Moteurs dAviation SNECMA
Priority to FR820594A priority Critical patent/FR1260040A/en
Priority to BE600698A priority patent/BE600698A/en
Priority to GB734661A priority patent/GB925010A/en
Application granted granted Critical
Publication of FR1260040A publication Critical patent/FR1260040A/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
    • F02K1/28—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

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Sampling And Sample Adjustment (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
FR820594A 1960-03-07 1960-03-07 Jet diverter device Expired FR1260040A (en)

Priority Applications (3)

Application Number Priority Date Filing Date Title
FR820594A FR1260040A (en) 1960-03-07 1960-03-07 Jet diverter device
BE600698A BE600698A (en) 1960-03-07 1961-02-27 Jet diverter device
GB734661A GB925010A (en) 1960-03-07 1961-02-28 Improvements in or relating to turbo-fan units

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
FR1260040A true FR1260040A (en) 1961-05-05

Family

ID=8726538

Family Applications (1)

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

Country Status (3)

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

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2132380A1 (en) * 1971-03-31 1972-11-17 Short Brothers & Harland Ltd
FR2597925A1 (en) * 1986-04-25 1987-10-30 Rolls Royce MOTOR PROPELLER GROUP OF GAS TURBINE ENGINE PROVIDED WITH FLOW CONTROL DEVICES
FR2812035A1 (en) * 2000-07-24 2002-01-25 Hurel Dubois Avions IMPROVEMENTS ON DRIVE INVERTERS FOR JET ENGINES OF THE GRID TYPE
US20160245230A1 (en) * 2015-02-23 2016-08-25 Rolls-Royce Deutschland Ltd & Co Kg Engine cowling of a gas turbine with thrust-reversing device and cross-sectionally adjustable outlet nozzle
EP2581593A3 (en) * 2011-10-13 2017-10-11 Rohr, Inc. Thrust Reverser Cascade Assembly with Flow Deflection Shelf

Families Citing this family (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB0321139D0 (en) 2003-09-10 2003-10-08 Short Brothers Plc A device
FR2900980B1 (en) * 2006-05-10 2011-08-19 Aircelle Sa NACELLE FOR DOUBLE FLOW TURBOREACTOR WITH HIGH DILUTION RATE
EP2181262B1 (en) 2007-08-08 2012-05-16 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
US9657686B2 (en) * 2013-05-06 2017-05-23 Rohr, Inc. System, apparatus, and method for a virtual blocker

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2132380A1 (en) * 1971-03-31 1972-11-17 Short Brothers & Harland Ltd
FR2597925A1 (en) * 1986-04-25 1987-10-30 Rolls Royce MOTOR PROPELLER GROUP OF GAS TURBINE ENGINE PROVIDED WITH FLOW CONTROL DEVICES
FR2812035A1 (en) * 2000-07-24 2002-01-25 Hurel Dubois Avions IMPROVEMENTS ON DRIVE INVERTERS FOR JET ENGINES OF THE GRID TYPE
EP1176302A1 (en) * 2000-07-24 2002-01-30 Hurel-Hispano Meudon Thrust reverser for a jet engine
US6438942B2 (en) 2000-07-24 2002-08-27 Societe De Construction Des Avions Hurel-Dubois (Societe Anonyme) Cascade-type reversers for jet engines
EP2581593A3 (en) * 2011-10-13 2017-10-11 Rohr, Inc. Thrust Reverser Cascade Assembly with Flow Deflection Shelf
US20160245230A1 (en) * 2015-02-23 2016-08-25 Rolls-Royce Deutschland Ltd & Co Kg Engine cowling of a gas turbine with thrust-reversing device and cross-sectionally adjustable outlet nozzle
US10151270B2 (en) * 2015-02-23 2018-12-11 Rolls-Royce Deutschland Ltd & Co Kg Engine cowling of a gas turbine with thrust-reversing device and cross-sectionally adjustable outlet nozzle

Also Published As

Publication number Publication date
BE600698A (en) 1961-08-28
GB925010A (en) 1963-05-01

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