ATE317794T1 - Flugzeug mit schubumkehrvorrichtungen - Google Patents

Flugzeug mit schubumkehrvorrichtungen

Info

Publication number
ATE317794T1
ATE317794T1 AT04291981T AT04291981T ATE317794T1 AT E317794 T1 ATE317794 T1 AT E317794T1 AT 04291981 T AT04291981 T AT 04291981T AT 04291981 T AT04291981 T AT 04291981T AT E317794 T1 ATE317794 T1 AT E317794T1
Authority
AT
Austria
Prior art keywords
reversers
aircraft
engines
thrust reversers
throttles
Prior art date
Application number
AT04291981T
Other languages
English (en)
Inventor
Joan Andre
Laurent Andrieu
Original Assignee
Airbus France
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 Airbus France filed Critical Airbus France
Application granted granted Critical
Publication of ATE317794T1 publication Critical patent/ATE317794T1/de

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C9/00—Controlling gas-turbine plants; Controlling fuel supply in air- breathing jet-propulsion plants
    • F02C9/48—Control of fuel supply conjointly with another control of the plant
    • F02C9/56—Control of fuel supply conjointly with another control of the plant with power transmission control
    • 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
    • B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
    • B64D27/02—Aircraft characterised by the type or position of power plants
    • B64D27/16—Aircraft characterised by the type or position of power plants of jet type
    • B64D27/18—Aircraft characterised by the type or position of power plants of jet type within, or attached to, wings
    • 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
    • B64D31/00—Power plant control systems; Arrangement of power plant control systems in aircraft
    • B64D31/02—Initiating means
    • B64D31/06—Initiating means actuated automatically
    • B64D31/12—Initiating means actuated automatically for equalising or synchronising power plants
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C9/00—Controlling gas-turbine plants; Controlling fuel supply in air- breathing jet-propulsion plants
    • F02C9/26—Control of fuel supply
    • F02C9/28—Regulating systems responsive to plant or ambient parameters, e.g. temperature, pressure, rotor speed
    • F02C9/285—Mechanical command devices linked to the throttle lever
    • 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
    • F02K1/76—Control or regulation of thrust reversers
    • 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)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Control Of Vehicle Engines Or Engines For Specific Uses (AREA)
  • Combined Controls Of Internal Combustion Engines (AREA)
  • Electric Propulsion And Braking For Vehicles (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Retarders (AREA)
  • Output Control And Ontrol Of Special Type Engine (AREA)
AT04291981T 2003-09-03 2004-08-03 Flugzeug mit schubumkehrvorrichtungen ATE317794T1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0310417A FR2859176B1 (fr) 2003-09-03 2003-09-03 Aeronef pourvu d'inverseurs de poussee

Publications (1)

Publication Number Publication Date
ATE317794T1 true ATE317794T1 (de) 2006-03-15

Family

ID=34130730

Family Applications (1)

Application Number Title Priority Date Filing Date
AT04291981T ATE317794T1 (de) 2003-09-03 2004-08-03 Flugzeug mit schubumkehrvorrichtungen

Country Status (7)

Country Link
US (1) US7107757B2 (de)
EP (1) EP1512627B1 (de)
AT (1) ATE317794T1 (de)
CA (1) CA2478780C (de)
DE (1) DE602004000398T2 (de)
ES (1) ES2258756T3 (de)
FR (1) FR2859176B1 (de)

Families Citing this family (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2879562B1 (fr) * 2004-12-20 2008-05-16 Airbus France Sas Dispositif pour emettre une autorisation d'agir sur le fonctionnement d'un moteur d'aeronef et systeme de controle de moteur comportant un tel dispositif
FR2922959B1 (fr) * 2007-10-31 2009-12-04 Airbus France Systeme de controle et procede de controle.
FR2930973B1 (fr) * 2008-05-06 2010-04-23 Airbus France Procede et dispositif de mise en oeuvre des inverseurs de poussee d'un aeronef
FR2933072B1 (fr) 2008-06-30 2010-08-20 Airbus France Procede et dispositif pour la detection d'une dissymetrie de poussee d'un aeronef au freinage.
FR2946021B1 (fr) 2009-05-28 2012-09-28 Airbus France Procede et dispositif pour la detection d'une dissymetrie de poussee d'un aeronef lors d'un atterrissage
US10443540B2 (en) * 2015-05-08 2019-10-15 United Technologies Corporation Thrust reversal for turbofan gas turbine engine
US10343786B2 (en) * 2017-06-28 2019-07-09 General Electric Company System and method of operating a ducted fan propulsion system during aircraft taxi
US10703498B2 (en) * 2017-11-02 2020-07-07 The Boeing Company Methods and aircraft for optimized reverse thrust operation during landing
GB201817279D0 (en) * 2018-10-24 2018-12-05 Rolls Royce Plc Supersonic jet aircraft

Family Cites Families (33)

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Publication number Priority date Publication date Assignee Title
US117582A (en) * 1871-08-01 Improvement in trimming-jacks for shoes and boots
US3286470A (en) * 1963-11-14 1966-11-22 Gen Electric Tip-turbine fan with thrust reverser
US3572155A (en) * 1969-06-30 1971-03-23 Boeing Co Interlock mechanism
US3614028A (en) * 1970-01-12 1971-10-19 Mc Donnell Douglas Corp Turbofan-powered stol aircraft
GB1258699A (de) * 1970-05-22 1971-12-30
US3774864A (en) * 1971-07-19 1973-11-27 Lockheed Aircraft Corp Cargo aircraft having increased payload capacity versus weight
US3887146A (en) * 1971-08-23 1975-06-03 Univ Rutgers Aircraft with combination stored energy and engine compressor power source for augmentation of lift, stability, control and propulsion
US3874620A (en) * 1973-03-09 1975-04-01 Boeing Co Reversing apparatus for a jet engine
US4311289A (en) * 1978-09-11 1982-01-19 The Dee Howard Company Modifications to jet aircraft having aft fuselage-mounted nacelles overlapping the wing assemblies
US4836469A (en) * 1987-05-29 1989-06-06 Valsan Partners Limited Partnership System for reducing aircraft noise and hush kit
US5100082A (en) * 1987-09-17 1992-03-31 The Boeing Company Hydraulic power supplies
US5230213A (en) * 1991-06-12 1993-07-27 Rohr, Inc. Aircraft turbine engine thrust reverser
US5379969A (en) * 1992-01-30 1995-01-10 The Boeing Company Hydraulic actuator with mechanical lock and installation
FR2694738B1 (fr) * 1992-08-14 1994-11-10 Aerospatiale Procédé de commande des gouvernes d'un avion pour compenser à basse vitesse une déviation latérale de trajectoire.
US5529263A (en) * 1992-10-21 1996-06-25 The Boeing Company Supersonic airplane with subsonic boost engine means and method of operating the same
US5443229A (en) * 1993-12-13 1995-08-22 General Electric Company Aircraft gas turbine engine sideways mount
US5667170A (en) * 1994-12-07 1997-09-16 Tracor Flight Systems, Inc. Pod mounted refueling system
EP0763653B1 (de) * 1995-09-13 2001-07-18 SOCIETE DE CONSTRUCTION DES AVIONS HUREL-DUBOIS (société anonyme) Strahlumkehrgitter für eine Schubumkehrvorrichtungsklappe
FR2756868B1 (fr) * 1996-12-05 1999-01-08 Hispano Suiza Sa Inverseur de poussee de turboreacteur a portes maintenues dans les lignes de nacelle
FR2760047B1 (fr) * 1997-02-27 1999-05-07 Hispano Suiza Sa Inverseur de poussee de turboreacteur a portes associees a un dispositif de synchronisation de commande
FR2764340B1 (fr) * 1997-06-05 1999-07-16 Hispano Suiza Sa Inverseur de poussee de turboreacteur a portes munies d'un becquet mobile a entrainement optimise
FR2770824B1 (fr) * 1997-11-12 2000-01-28 Aerospatiale Procede de commande des gouvernes d'un avion pour agir contre une deviation laterale de trajectoire au sol
US6233920B1 (en) * 1999-02-01 2001-05-22 Stage Iii Technologies, L.C. Contoured thrust reverser and lobed nozzle noise suppressor for gas turbine engines
US6311928B1 (en) * 2000-01-05 2001-11-06 Stage Iii Technologies, L.C. Jet engine cascade thrust reverser for use with mixer/ejector noise suppressor
US6264135B1 (en) * 2000-02-14 2001-07-24 John Dacosta Inflight aircraft visual monitoring apparatus
DE10062252A1 (de) * 2000-12-14 2002-07-11 Rolls Royce Deutschland Verfahren zur Regelung von Fluggasturbinen
US6575406B2 (en) * 2001-01-19 2003-06-10 The Boeing Company Integrated and/or modular high-speed aircraft
AU2002250133A1 (en) * 2001-02-16 2002-09-04 Hamilton Sundstrand Corporation Improved aircraft system architecture
FR2823259B1 (fr) * 2001-04-05 2003-06-27 Hispano Suiza Sa Systeme de verrouillage synchronise des portes d'un inverseur de poussee
US6802479B2 (en) * 2002-05-16 2004-10-12 The Boeing Company Flammable fluid line shroud
FR2850084B1 (fr) * 2003-01-21 2005-12-30 Airbus France Procede et systeme de commande d'une gouverne d'aeronef.
US6976352B2 (en) * 2003-03-22 2005-12-20 The Nordam Group, Inc. Toggle interlocked thrust reverser
US6978971B1 (en) * 2004-06-15 2005-12-27 The Boeing Company Methods and apparatuses for controlling airflow proximate to engine/airfoil systems

Also Published As

Publication number Publication date
DE602004000398T2 (de) 2006-10-19
EP1512627B1 (de) 2006-02-15
CA2478780C (fr) 2011-05-24
US20050116096A1 (en) 2005-06-02
CA2478780A1 (fr) 2005-03-03
FR2859176B1 (fr) 2005-10-28
EP1512627A1 (de) 2005-03-09
DE602004000398D1 (de) 2006-04-20
FR2859176A1 (fr) 2005-03-04
ES2258756T3 (es) 2006-09-01
US7107757B2 (en) 2006-09-19

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Legal Events

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RER Ceased as to paragraph 5 lit. 3 law introducing patent treaties