BE682005A - - Google Patents

Info

Publication number
BE682005A
BE682005A BE682005DA BE682005A BE 682005 A BE682005 A BE 682005A BE 682005D A BE682005D A BE 682005DA BE 682005 A BE682005 A BE 682005A
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.)
Filing date
Publication date
Application filed filed Critical
Publication of BE682005A publication Critical patent/BE682005A/xx

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C25/00—Alighting gear
    • B64C25/32—Alighting gear characterised by elements which contact the ground or similar surface 
    • B64C25/42—Arrangement or adaptation of brakes
    • B64C25/423—Braking devices acting by reaction of gaseous medium
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C11/00—Propellers, e.g. of ducted type; Features common to propellers and rotors for rotorcraft
    • B64C11/001—Shrouded propellers
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D33/00—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for
    • B64D33/04—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of exhaust outlets or jet pipes
    • 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
    • F02K1/68—Reversers mounted on the engine housing downstream of the fan exhaust section
    • 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
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Control Of Turbines (AREA)
BE682005D 1965-06-07 1966-06-02 BE682005A (xx)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US462791A US3262269A (en) 1965-06-07 1965-06-07 Thrust reverser

Publications (1)

Publication Number Publication Date
BE682005A true BE682005A (xx) 1966-11-14

Family

ID=23837766

Family Applications (1)

Application Number Title Priority Date Filing Date
BE682005D BE682005A (xx) 1965-06-07 1966-06-02

Country Status (6)

Country Link
US (1) US3262269A (xx)
BE (1) BE682005A (xx)
CH (1) CH446078A (xx)
DE (1) DE1287444B (xx)
GB (1) GB1147351A (xx)
NL (1) NL6607772A (xx)

Families Citing this family (20)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1127828A (en) * 1966-06-29 1968-09-18 Rolls Royce Fan thrust reverser for jet propulsion plant
DE1964976C3 (de) * 1969-12-24 1973-01-04 Motoren- Und Turbinen-Union Muenchen Gmbh, 8000 Muenchen Schubumkehrvorrichtung für ein Turbinenstrahltriebwerk eines Flugzeuges
US3717304A (en) * 1970-05-06 1973-02-20 Rolls Royce Thrust reverser for fluid flow engine
GB1388406A (en) * 1971-12-15 1975-03-26 Rolls Royce Gas turbine ducted fan engines
US3814324A (en) * 1972-06-19 1974-06-04 Gen Electric Propulsion nozzle and actuator system employed therein
US3981450A (en) * 1975-09-22 1976-09-21 The United States Of America As Represented By The Secretary Of The Air Force In-flight modulating thrust reverser
US5615834A (en) * 1995-01-31 1997-04-01 Osman; Medhat A. Ultra thrust reverser system
FR2830051B1 (fr) * 2001-09-27 2003-11-07 Hurel Hispano Le Havre Systeme de verrouillage sur un inverseur de poussee a grilles
FR2900980B1 (fr) * 2006-05-10 2011-08-19 Aircelle Sa Nacelle pour turboreacteur double flux a grand taux de dilution
EP2074308B1 (en) * 2006-10-12 2011-12-21 United Technologies Corporation Integrated variable area nozzle and thrust reversing mechanism
FR2929998B1 (fr) * 2008-04-14 2011-08-12 Aircelle Sa Nacelle de turboreacteur a double flux
FR2939477A1 (fr) * 2008-12-10 2010-06-11 Aircelle Sa Nacelle de turboreacteur a section de tuyere variable
US8109467B2 (en) * 2009-04-24 2012-02-07 United Technologies Corporation Thrust reverser assembly with shaped drag links
FR2946094B1 (fr) * 2009-06-02 2014-04-18 Aircelle Sa Inverseur de poussee pour nacelle de turboreacteur double flux.
FR2952128B1 (fr) * 2009-11-05 2011-11-04 Aircelle Sa Dispositif d'inverseur de poussee
US9650992B2 (en) * 2013-10-17 2017-05-16 Rohr, Inc. Core cowl thrust reverser system and apparatus
FR3031725B1 (fr) 2015-01-21 2018-06-01 Safran Nacelles Nacelle de turboreacteur d’aeronef
US20160305370A1 (en) * 2015-04-16 2016-10-20 Honeywell International Inc. Translating cowl thrust reverser with door pivots aft of reverse flow path
US10533519B2 (en) * 2016-01-13 2020-01-14 Rohr, Inc. Translating cascade hidden blocker door thrust reverser
US10563614B2 (en) 2016-08-17 2020-02-18 Honeywell International Inc. Composite translating cowl assembly for a thrust reverser system

Family Cites Families (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
BE524592A (xx) * 1952-11-25
US2950595A (en) * 1954-11-01 1960-08-30 Marquardt Corp Thrust reverser
US2847823A (en) * 1955-03-15 1958-08-19 Curtiss Wright Corp Reverse thrust nozzle construction
DE1054848B (de) * 1956-04-27 1959-04-09 Armstrong Siddeley Motors Ltd Vorrichtung zur Schubumkehr bei einem Strahltriebwerk eines Flugzeugs
US3113428A (en) * 1957-03-13 1963-12-10 Rolls Royce Silenced jet propulsion nozzle with thrust reversing means
FR1286886A (fr) * 1961-01-27 1962-03-09 Nord Aviation Dispositif d'inversion de poussée pour propulseurs comportant un turbo-réacteur àdouble flux
NL247267A (xx) * 1958-04-02
US2938335A (en) * 1958-04-14 1960-05-31 Boeing Co Noise suppressor and thrust reverser
US3068646A (en) * 1959-01-28 1962-12-18 Rolls Royce Improvements in by-pass type gas turbine engines
US3036431A (en) * 1959-09-08 1962-05-29 Boeing Co Thrust reverser for jet engines
DE1127725B (de) * 1960-01-12 1962-04-12 Rolls Royce Strahltriebwerk mit Mitteln zur Strahlumkehr
DE1187491B (de) * 1960-03-07 1965-02-18 Moteuers D Aviat Soc Nat D Etu Stroemungskanal mit ringfoermigem Querschnitt und seitlichen Strahlumlenkungsoeffnungen

Also Published As

Publication number Publication date
DE1287444B (de) 1969-01-16
CH446078A (de) 1967-10-31
US3262269A (en) 1966-07-26
GB1147351A (en) 1969-04-02
NL6607772A (xx) 1966-12-08

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