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

    • 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
    • B64D29/00—Power-plant nacelles, fairings, or cowlings
    • B64D29/08—Inspection panels for power plants
    • 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
    • B64D29/00—Power-plant nacelles, fairings, or cowlings
    • B64D29/06—Attaching of nacelles, fairings or cowlings
    • 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
    • G—PHYSICS
    • G06—COMPUTING; CALCULATING OR COUNTING
    • G06F—ELECTRIC DIGITAL DATA PROCESSING
    • G06F3/00—Input 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
    • G06F3/01—Input arrangements or combined input and output arrangements for interaction between user and computer
    • G06F3/011—Arrangements 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)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Human Computer Interaction (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
EP2829474B1 (en) 2013-07-22 2018-11-21 Airbus Defence and Space SA Monitoring system for monitoring a two-part-cowl lock unit
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
FR2928681A1 (fr) 2009-09-18
WO2009115662A8 (fr) 2009-12-30
EP2254794B1 (fr) 2015-08-26
CN101959760A (zh) 2011-01-26
FR2928681B1 (fr) 2013-11-22
CN101959760B (zh) 2015-06-03
ES2553752T3 (es) 2015-12-11
WO2009115662A2 (fr) 2009-09-24
RU2010141390A (ru) 2012-04-20
RU2494016C2 (ru) 2013-09-27
US20110017843A1 (en) 2011-01-27
EP2254794A2 (fr) 2010-12-01
WO2009115662A3 (fr) 2009-11-12

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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.