BR0304677B1 - inversor de empuxo para turborreator. - Google Patents

inversor de empuxo para turborreator.

Info

Publication number
BR0304677B1
BR0304677B1 BRPI0304677-0A BR0304677A BR0304677B1 BR 0304677 B1 BR0304677 B1 BR 0304677B1 BR 0304677 A BR0304677 A BR 0304677A BR 0304677 B1 BR0304677 B1 BR 0304677B1
Authority
BR
Brazil
Prior art keywords
turborreator
thrust inverter
thrust
inverter
Prior art date
Application number
BRPI0304677-0A
Other languages
English (en)
Other versions
BR0304677A (pt
Inventor
Baptiste Colotte
Alexandre Courpied
Marc Croixmarie
Patrick Joland
Gouellec Gilles Le
Marion Michau
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 BR0304677A publication Critical patent/BR0304677A/pt
Publication of BR0304677B1 publication Critical patent/BR0304677B1/pt

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
    • F02K1/54—Nozzles having means for reversing jet thrust
    • F02K1/76—Control or regulation of thrust reversers
    • F02K1/766—Control or regulation of thrust reversers with blocking systems or locking devices; Arrangement of locking devices for thrust reversers
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2270/00—Control
    • F05D2270/01—Purpose of the control system
    • F05D2270/09—Purpose of the control system to cope with emergencies
    • F05D2270/094—Purpose of the control system to cope with emergencies by using back-up controls

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Lock And Its Accessories (AREA)
  • Power-Operated Mechanisms For Wings (AREA)
  • Electric Propulsion And Braking For Vehicles (AREA)
  • Control Of Multiple Motors (AREA)
  • Control Of Turbines (AREA)
BRPI0304677-0A 2002-10-25 2003-10-23 inversor de empuxo para turborreator. BR0304677B1 (pt)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0213410A FR2846378B1 (fr) 2002-10-25 2002-10-25 Inverseur de poussee electromecanique pour turboreacteur a synchronisation des dispositifs de verrouillage

Publications (2)

Publication Number Publication Date
BR0304677A BR0304677A (pt) 2004-08-31
BR0304677B1 true BR0304677B1 (pt) 2012-06-26

Family

ID=32050684

Family Applications (1)

Application Number Title Priority Date Filing Date
BRPI0304677-0A BR0304677B1 (pt) 2002-10-25 2003-10-23 inversor de empuxo para turborreator.

Country Status (11)

Country Link
US (1) US7278257B2 (pt)
EP (1) EP1413737B1 (pt)
JP (1) JP4015605B2 (pt)
CN (1) CN100350146C (pt)
BR (1) BR0304677B1 (pt)
CA (1) CA2445851C (pt)
DE (1) DE60314351T2 (pt)
ES (1) ES2287429T3 (pt)
FR (1) FR2846378B1 (pt)
RU (1) RU2313682C2 (pt)
UA (1) UA82463C2 (pt)

Families Citing this family (26)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7409820B2 (en) * 2004-11-16 2008-08-12 Honeywell International Inc. Electrical thrust reverser tertiary lock system including a voltage limiting circuit
FR2887301B1 (fr) * 2005-06-16 2007-08-31 Aircelle Sa Systeme de commande electronique pour nacelle
US7513101B2 (en) * 2005-10-28 2009-04-07 Honeywell International Inc. Synchronized motor thrust reverser actuation system
US7721551B2 (en) * 2006-06-29 2010-05-25 United Technologies Corporation Fan variable area nozzle for a gas turbine engine fan nacelle
FR2912470B1 (fr) * 2007-02-14 2009-03-20 Aircelle Sa Procede de controle des moteurs electriques d'un inverseur de poussee
FR2920204B1 (fr) * 2007-08-20 2009-10-30 Aircelle Sa Procede et systeme de commande d'au moins un actionneur de capots d'un inverseur de poussee pour turboreacteur
FR2920202B1 (fr) * 2007-08-20 2009-10-30 Aircelle Sa Systeme de commande d'au moins un actionneur de capots d'un inverseur de poussee pour turboreacteur
FR2922959B1 (fr) * 2007-10-31 2009-12-04 Airbus France Systeme de controle et procede de controle.
FR2927309B1 (fr) * 2008-02-13 2010-04-16 Aircelle Sa Systeme de commande pour nacelle de turboreacteur
FR2927310B1 (fr) * 2008-02-13 2010-07-30 Aircelle Sa Systeme de commande pour nacelle de turboreacteur
FR2927663B1 (fr) * 2008-02-15 2013-05-24 Hispano Suiza Sa Systeme de commande d'une pluralite de fonctions d'un turboreacteur.
FR2928681B1 (fr) * 2008-03-14 2013-11-22 Aircelle Sa Systeme d'actionnement et de controle d'un capot mobile de nacelle de turboreacteur
FR2932226B1 (fr) * 2008-06-06 2013-08-23 Aircelle Sa Procede de synchronisation des actionneurs d'un capot mobile d'inverseur de poussee
US8170771B2 (en) * 2008-06-30 2012-05-01 Honeywell International Inc. Fluid-powered thrust reverser actuation system speed control
FR2944563B1 (fr) * 2009-04-16 2011-04-22 Aircelle Sa Dispositif d'inversion de poussee
FR2944564B1 (fr) * 2009-04-16 2011-04-22 Aircelle Sa Systeme de controle pour nacelle de turboreacteur
FR2944509B1 (fr) 2009-04-16 2012-10-19 Aircelle Sa Systeme d'actionnement pour nacelle de turboreacteur
FR2958979B1 (fr) * 2010-04-20 2012-03-16 Aircelle Sa Systeme de commande de type hydraulique pour dispositif d'inversion de poussee
FR2966617B1 (fr) * 2010-10-22 2013-06-14 Snecma Procede et dispositif de surveillance d'une boucle d'asservissement d'un systeme d'actionnement de geometries variables d'un turboreacteur
FR2974597B1 (fr) * 2011-04-27 2019-05-10 Safran Nacelles Ensemble de verrouillage tertiaire pour dispositif d'inversion de poussee
US8615982B2 (en) * 2011-07-05 2013-12-31 Hamilton Sundstrand Corporation Integrated electric variable area fan nozzle thrust reversal actuation system
FR2978801B1 (fr) * 2011-08-05 2016-03-04 Snecma Procede de surveillance des moyens de verrouillage d'un systeme electrique d'inversion de poussee pour turbomachine
FR3005488B1 (fr) * 2013-05-07 2015-05-29 Airbus Operations Sas Dispositif de commande d'une tuyere a section variable d'un aeronef
FR3008741B1 (fr) 2013-07-17 2017-04-28 Aircelle Sa Systeme inverseur de poussee electrique pour nacelle de moteur d'aeronef et nacelle de moteur d'aeronef ainsi equipee
FR3012167B1 (fr) * 2013-10-18 2015-12-18 Snecma Procede de surveillance d'un systeme de verrouillage
FR3028295B1 (fr) * 2014-11-06 2020-01-17 Safran Electronics & Defense Systeme d'actionnement d'une structure mobile d'un inverseur de poussee d'un aeronef, inverseur de poussee et reacteur comprenant un tel systeme.

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4391409A (en) * 1980-09-30 1983-07-05 The Boeing Company Positioning and control system for fan thrust reverser cowls in a turbofan engine
US4409884A (en) * 1981-03-25 1983-10-18 Mcdonnell Douglas Corporation Synchronization cylinder
FR2683860B1 (fr) * 1991-11-14 1995-04-28 Hurel Dubois Avions Installation de securite pour inverseur de poussee a portes equipant un avion et ensemble incorporant une telle installation.
US5720449A (en) * 1993-11-19 1998-02-24 Societe De Construction Des Avions Hurel-Dubois Thrust reverser with doors for aircraft engine, equipped with safety systems preventing the untimely opening of the doors
EP0763654B1 (en) * 1995-09-13 1999-12-29 SOCIETE DE CONSTRUCTION DES AVIONS HUREL-DUBOIS (société anonyme) Electro/hydraulic system for a 2 door thrust reverser
FR2755730B1 (fr) * 1996-11-14 1999-01-08 Hispano Suiza Sa Systeme de commande electrique pour inverseur de poussee de turboreacteur
US6439504B1 (en) * 2001-06-15 2002-08-27 Honeywell International, Inc. System and method for sustaining electric power during a momentary power interruption in an electric thrust reverser actuation system
US6655125B2 (en) * 2001-12-05 2003-12-02 Honeywell International Inc. System architecture for electromechanical thrust reverser actuation systems
FR2846377B1 (fr) * 2002-10-25 2006-06-30 Hispano Suiza Sa Inverseur de poussee electromecanique pour turboreacteur a controle permanent de position

Also Published As

Publication number Publication date
US7278257B2 (en) 2007-10-09
CA2445851C (fr) 2011-05-31
EP1413737B1 (fr) 2007-06-13
CN100350146C (zh) 2007-11-21
CA2445851A1 (fr) 2004-04-25
JP4015605B2 (ja) 2007-11-28
FR2846378A1 (fr) 2004-04-30
UA82463C2 (uk) 2008-04-25
BR0304677A (pt) 2004-08-31
EP1413737A1 (fr) 2004-04-28
JP2004156594A (ja) 2004-06-03
DE60314351T2 (de) 2008-02-21
DE60314351D1 (de) 2007-07-26
RU2313682C2 (ru) 2007-12-27
CN1515463A (zh) 2004-07-28
RU2003131386A (ru) 2005-04-10
FR2846378B1 (fr) 2006-06-30
US20040139725A1 (en) 2004-07-22
ES2287429T3 (es) 2007-12-16

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Legal Events

Date Code Title Description
B09A Decision: intention to grant [chapter 9.1 patent gazette]
B16A Patent or certificate of addition of invention granted

Free format text: PRAZO DE VALIDADE: 20 (VINTE) ANOS CONTADOS A PARTIR DE 23/10/2003, OBSERVADAS AS CONDICOES LEGAIS.

B21F Lapse acc. art. 78, item iv - on non-payment of the annual fees in time

Free format text: REFERENTE A 13A ANUIDADE.

B24J Lapse because of non-payment of annual fees (definitively: art 78 iv lpi, resolution 113/2013 art. 12)

Free format text: EM VIRTUDE DA EXTINCAO PUBLICADA NA RPI 2385 DE 20-09-2016 E CONSIDERANDO AUSENCIA DE MANIFESTACAO DENTRO DOS PRAZOS LEGAIS, INFORMO QUE CABE SER MANTIDA A EXTINCAO DA PATENTE E SEUS CERTIFICADOS, CONFORME O DISPOSTO NO ARTIGO 12, DA RESOLUCAO 113/2013.