BRPI0908912A2 - sistema para acionamento e controle de carenagem mével de nacela de motor turbojato e nacela para motor turbojato - Google Patents

sistema para acionamento e controle de carenagem mével de nacela de motor turbojato e nacela para motor turbojato

Info

Publication number
BRPI0908912A2
BRPI0908912A2 BRPI0908912A BRPI0908912A BRPI0908912A2 BR PI0908912 A2 BRPI0908912 A2 BR PI0908912A2 BR PI0908912 A BRPI0908912 A BR PI0908912A BR PI0908912 A BRPI0908912 A BR PI0908912A BR PI0908912 A2 BRPI0908912 A2 BR PI0908912A2
Authority
BR
Brazil
Prior art keywords
turbojet engine
engine nacelle
control system
fairing drive
mobile fairing
Prior art date
Application number
BRPI0908912A
Other languages
English (en)
Inventor
Gerome Marc
Pierre Germain Le Coq Vincent
Original Assignee
Aircelle Sa
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 Aircelle Sa filed Critical Aircelle Sa
Publication of BRPI0908912A2 publication Critical patent/BRPI0908912A2/pt

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D29/00Power-plant nacelles, fairings, or cowlings
    • B64D29/08Inspection panels for power plants
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D29/00Power-plant nacelles, fairings, or cowlings
    • B64D29/06Attaching of nacelles, fairings or cowlings
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02KJET-PROPULSION PLANTS
    • F02K1/00Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/54Nozzles having means for reversing jet thrust
    • F02K1/76Control or regulation of thrust reversers
    • F02K1/766Control or regulation of thrust reversers with blocking systems or locking devices; Arrangement of locking devices for thrust reversers
    • GPHYSICS
    • G06COMPUTING; CALCULATING OR COUNTING
    • G06FELECTRIC DIGITAL DATA PROCESSING
    • G06F3/00Input arrangements for transferring data to be processed into a form capable of being handled by the computer; Output arrangements for transferring data from processing unit to output unit, e.g. interface arrangements
    • G06F3/01Input arrangements or combined input and output arrangements for interaction between user and computer
    • G06F3/011Arrangements for interaction with the human body, e.g. for user immersion in virtual reality

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Theoretical Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Human Computer Interaction (AREA)
  • General Physics & Mathematics (AREA)
  • Physics & Mathematics (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Output Control And Ontrol Of Special Type Engine (AREA)
  • Control Of Vehicle Engines Or Engines For Specific Uses (AREA)
BRPI0908912A 2008-03-14 2009-02-04 sistema para acionamento e controle de carenagem mével de nacela de motor turbojato e nacela para motor turbojato BRPI0908912A2 (pt)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR0801396A FR2928681B1 (fr) 2008-03-14 2008-03-14 Systeme d'actionnement et de controle d'un capot mobile de nacelle de turboreacteur
PCT/FR2009/000125 WO2009115662A2 (fr) 2008-03-14 2009-02-04 Systeme d'actionnement et de controle d'un capot mobile de nacelle de turboreacteur

Publications (1)

Publication Number Publication Date
BRPI0908912A2 true BRPI0908912A2 (pt) 2019-09-24

Family

ID=39869672

Family Applications (1)

Application Number Title Priority Date Filing Date
BRPI0908912A BRPI0908912A2 (pt) 2008-03-14 2009-02-04 sistema para acionamento e controle de carenagem mével de nacela de motor turbojato e nacela para motor turbojato

Country Status (8)

Country Link
US (1) US20110017843A1 (pt)
EP (1) EP2254794B1 (pt)
CN (1) CN101959760B (pt)
BR (1) BRPI0908912A2 (pt)
ES (1) ES2553752T3 (pt)
FR (1) FR2928681B1 (pt)
RU (1) RU2494016C2 (pt)
WO (1) WO2009115662A2 (pt)

Families Citing this family (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
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
FR2989429B1 (fr) * 2012-04-17 2014-05-16 Airbus Operations Sas Dispositif de commande d'une tuyere a section variable d'un aeronef
FR3007390B1 (fr) * 2013-06-19 2015-07-17 Airbus Operations Sas Mecanisme de verrouillage d'un capot d'aeronef integrant un capteur pour detecter l'etat non verrouille du capot
ES2716992T3 (es) 2013-07-22 2019-06-18 Airbus Defence And Space Sa Sistema de seguimiento para el seguimiento de una unidad de bloqueo de un capó de dos partes
FR3012167B1 (fr) * 2013-10-18 2015-12-18 Snecma Procede de surveillance d'un systeme de verrouillage
FR3020040B1 (fr) * 2014-04-17 2018-06-29 Societe Lorraine De Construction Aeronautique Ensemble propulsif pour aeronef
US9702176B2 (en) 2014-07-07 2017-07-11 Itt Manufacturing Enterprises Llc Spring loaded actuator assembly
FR3044718B1 (fr) * 2015-12-08 2017-12-22 Snecma Moteur d'aeronef comprenant un equipement externe monte coulissant pour faciliter son acces en maintenance
US11781503B2 (en) 2022-01-19 2023-10-10 Honeywell International Inc. Translating cowl thrust reverser primary lock system

Family Cites Families (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU1766020C (ru) * 1989-12-20 1994-08-15 Авиационный комплекс им.С.В.Ильюшина Створка гондолы двигателя летательного аппарата
GB9015373D0 (en) * 1990-07-12 1990-08-29 Rolls Royce Plc Gas turbine engine thrust reverser control
GB9301457D0 (en) * 1993-01-26 1993-03-17 Short Brothers Plc An aircraft propulsuve power unit
FR2731049B1 (fr) * 1995-02-28 1997-05-09 Aerospatiale Dispositif de fixation d'une bouche d'entree d'air sur un reacteur et reacteur comportant un tel dispositif
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
US6684623B2 (en) * 2002-02-27 2004-02-03 Honeywell International, Inc. Gearless electric thrust reverser actuators and actuation system incorporating same
US6622963B1 (en) * 2002-04-16 2003-09-23 Honeywell International Inc. System and method for controlling the movement of an aircraft engine cowl door
FR2846378B1 (fr) * 2002-10-25 2006-06-30 Hispano Suiza Sa Inverseur de poussee electromecanique pour turboreacteur a synchronisation des dispositifs de verrouillage
US7252311B2 (en) * 2003-09-17 2007-08-07 Hartwell Corporation Motor driven latch
FR2887301B1 (fr) * 2005-06-16 2007-08-31 Aircelle Sa Systeme de commande electronique pour nacelle
FR2890378B1 (fr) * 2005-09-08 2009-01-16 Airbus France Sas Capot de nacelle pour turboreacteur et nacelle comportant au moins un tel capot.
FR2905357B1 (fr) * 2006-08-31 2009-07-03 Aircelle Sa Systeme de verrouillage pour capot mobile de nacelle
FR2906568B1 (fr) 2006-10-02 2012-01-06 Aircelle Sa Structure d'entree d'air deposable pour nacelle de turboreacteur.
US7843363B2 (en) * 2007-07-12 2010-11-30 Rosemount Aerospace Inc. Mechanical latch locking detection sensors
US8096498B2 (en) * 2007-12-12 2012-01-17 Hamilton Sundstrand Corporation Rotating auxiliary power unit air inlet door
US8181905B2 (en) * 2008-12-17 2012-05-22 Rohr, Inc. Aircraft engine nacelle with translating inlet cowl

Also Published As

Publication number Publication date
RU2494016C2 (ru) 2013-09-27
EP2254794A2 (fr) 2010-12-01
RU2010141390A (ru) 2012-04-20
CN101959760B (zh) 2015-06-03
FR2928681A1 (fr) 2009-09-18
WO2009115662A3 (fr) 2009-11-12
EP2254794B1 (fr) 2015-08-26
WO2009115662A8 (fr) 2009-12-30
FR2928681B1 (fr) 2013-11-22
ES2553752T3 (es) 2015-12-11
US20110017843A1 (en) 2011-01-27
WO2009115662A2 (fr) 2009-09-24
CN101959760A (zh) 2011-01-26

Similar Documents

Publication Publication Date Title
BRPI0908912A2 (pt) sistema para acionamento e controle de carenagem mével de nacela de motor turbojato e nacela para motor turbojato
BRPI0717730A2 (pt) Nacela para motor turbojato de contorno, conjunto de propulsão e avião
BRPI0821504A2 (pt) nacela para motor de avião
BRPI0821929A2 (pt) Nacela para motor turbojato
BRPI1009069A2 (pt) sistema de arranque e geração para uso com um motor de aeronave e método de controle de um sistema de arranque e geraçao para uso com um motor de aeronave
BR112013007626A2 (pt) ''método para controle de um sistema de combustível de um mecanismo motor e sistema potência''
BRPI0922165A2 (pt) sistema de hélices contra-rotativas para turbomáquina de aeronave e turbomáquina para aeronave
BRPI0816889A2 (pt) Sistema de motor multimodal, segunda unidade de controle de motor, método para operar um motor, sistema de motor, e, método
BRPI0812844A2 (pt) Estribo de afixação para motor de aeronave, conjunto motor para aeronave, e, aeronave
BR112013006893A2 (pt) sistema de mecanismo motor e método
BRPI0908079A2 (pt) Conjunto motor para aeronave, e, aeronave
BRPI1011359A2 (pt) método para controlar o suprimento de um primeiro combustível e um segundo combustível a um motor, e, sistema de injeção de combustível para um motor
BRPI0907771A2 (pt) Conjunto motor para aeronave, e, aeronave
BRPI0921975A2 (pt) reversor de empuxo para nacela de motor turbofan, nacela de motor turbofan e aeronave.
BRPI0910935A2 (pt) desvio da nacela de motor turbojato e nacela
BR112012002777A2 (pt) dispositivo de reversor de empuxo para uma nacela de motor turbojato
BRPI1013147A2 (pt) dispositivo de inversão de empuxo e nacela de motor turbojato de duplo fluxo.
BRPI0822127A8 (pt) nacela para motor turbojato e aeronave
BR112014001224A2 (pt) nacela de motor turbojato compreendendo um dispositivo reversor de empuxo e um sistema de atuação para referido dispositivo reversor de empuxo
BR112014009939A2 (pt) dispositivo de reversão de empuxo para uma nacela de motor turbojato e nacela de um motor turbojato
BR112014002212A2 (pt) dispositivo reversor de empuxo de uma nacela e uma nacela de um motor turbo- ventilador
BRPI1007029A2 (pt) conjunto de suspensão para motor turbojato de aeronaves
BR112014028731A2 (pt) reversor de empuxo para uma nacela de motor turbojato e nacela de motor turbojato.
BRPI0906953A2 (pt) Entrada de ar para nacela de aeronave, conjunto compreendendo entrada de ar, conjunto de propulsão para aeronave
BRPI0822363A2 (pt) Nacela de motor turbojato

Legal Events

Date Code Title Description
B08F Application dismissed because of non-payment of annual fees [chapter 8.6 patent gazette]
B08K Patent lapsed as no evidence of payment of the annual fee has been furnished to inpi [chapter 8.11 patent gazette]

Free format text: EM VIRTUDE DO ARQUIVAMENTO PUBLICADO NA RPI 2543 DE 01-10-2019 E CONSIDERANDO AUSENCIA DE MANIFESTACAO DENTRO DOS PRAZOS LEGAIS, INFORMO QUE CABE SER MANTIDO O ARQUIVAMENTO DO PEDIDO DE PATENTE, CONFORME O DISPOSTO NO ARTIGO 12, DA RESOLUCAO 113/2013.