BR112014027471A2 - sistema de controle para o reversor de empuxo com elementos móveis e nacela compreendendo pelo menos um elemento móvel e um sistema de controle. - Google Patents

sistema de controle para o reversor de empuxo com elementos móveis e nacela compreendendo pelo menos um elemento móvel e um sistema de controle.

Info

Publication number
BR112014027471A2
BR112014027471A2 BR112014027471A BR112014027471A BR112014027471A2 BR 112014027471 A2 BR112014027471 A2 BR 112014027471A2 BR 112014027471 A BR112014027471 A BR 112014027471A BR 112014027471 A BR112014027471 A BR 112014027471A BR 112014027471 A2 BR112014027471 A2 BR 112014027471A2
Authority
BR
Brazil
Prior art keywords
control system
movable
thrust reverser
movable element
nacelle thrust
Prior art date
Application number
BR112014027471A
Other languages
English (en)
Inventor
Nourrisson Alain
Maalioune Hakim
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 BR112014027471A2 publication Critical patent/BR112014027471A2/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
    • F02K1/763—Control or regulation of thrust reversers with actuating systems or actuating devices; Arrangement of actuators for thrust reversers
    • 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
    • H—ELECTRICITY
    • H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02P—CONTROL OR REGULATION OF ELECTRIC MOTORS, ELECTRIC GENERATORS OR DYNAMO-ELECTRIC CONVERTERS; CONTROLLING TRANSFORMERS, REACTORS OR CHOKE COILS
    • H02P3/00—Arrangements for stopping or slowing electric motors, generators, or dynamo-electric converters
    • H02P3/06—Arrangements for stopping or slowing electric motors, generators, or dynamo-electric converters for stopping or slowing an individual dynamo-electric motor or dynamo-electric converter
    • H02P3/18—Arrangements for stopping or slowing electric motors, generators, or dynamo-electric converters for stopping or slowing an individual dynamo-electric motor or dynamo-electric converter for stopping or slowing an ac motor
    • H02P3/22—Arrangements for stopping or slowing electric motors, generators, or dynamo-electric converters for stopping or slowing an individual dynamo-electric motor or dynamo-electric converter for stopping or slowing an ac motor by short-circuit or resistive braking
    • 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
    • F05D2260/00—Function
    • F05D2260/90—Braking
    • F05D2260/903—Braking using electrical or magnetic forces
    • 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
    • F05D2270/02—Purpose of the control system to control rotational speed (n)
    • F05D2270/021—Purpose of the control system to control rotational speed (n) to prevent overspeed
    • 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
    • F05D2270/50—Control logic embodiments
    • F05D2270/52—Control logic embodiments by electrical means, e.g. relays or switches
    • 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
    • F05D2270/60—Control system actuates means
    • F05D2270/62—Electrical actuators
    • 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)
  • Power Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Stopping Of Electric Motors (AREA)
  • Electric Propulsion And Braking For Vehicles (AREA)
BR112014027471A 2012-05-04 2013-05-02 sistema de controle para o reversor de empuxo com elementos móveis e nacela compreendendo pelo menos um elemento móvel e um sistema de controle. BR112014027471A2 (pt)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1254099A FR2990248B1 (fr) 2012-05-04 2012-05-04 Systeme de commande pour inverseur de poussee
PCT/FR2013/050969 WO2013164546A1 (fr) 2012-05-04 2013-05-02 Système de commande pour inverseur de poussée

Publications (1)

Publication Number Publication Date
BR112014027471A2 true BR112014027471A2 (pt) 2017-09-19

Family

ID=48468652

Family Applications (1)

Application Number Title Priority Date Filing Date
BR112014027471A BR112014027471A2 (pt) 2012-05-04 2013-05-02 sistema de controle para o reversor de empuxo com elementos móveis e nacela compreendendo pelo menos um elemento móvel e um sistema de controle.

Country Status (8)

Country Link
US (1) US9482183B2 (pt)
EP (1) EP2844860B1 (pt)
CN (1) CN104285055A (pt)
BR (1) BR112014027471A2 (pt)
CA (1) CA2871729A1 (pt)
FR (1) FR2990248B1 (pt)
RU (1) RU2014147908A (pt)
WO (1) WO2013164546A1 (pt)

Families Citing this family (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
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
FR3021300A1 (fr) * 2014-10-20 2015-11-27 Aircelle Sa Systeme d’actionnement pour inverseur de poussee
US10443540B2 (en) 2015-05-08 2019-10-15 United Technologies Corporation Thrust reversal for turbofan gas turbine engine
US10371091B2 (en) * 2017-01-09 2019-08-06 Honeywell International Inc. Electric thrust reverser actuation system with controlled brake assist
RU175530U1 (ru) * 2017-04-12 2017-12-07 Акционерное общество "Диаконт" Высоконадёжный отказобезопасный электропривод реверсивного устройства
US10862408B2 (en) 2018-07-12 2020-12-08 Parker-Hannifin Corporation Electric motor regenerated energy management method
US11414175B2 (en) 2019-04-01 2022-08-16 Pratt & Whitney Canada Corp. Method and system for operating an aircraft powerplant
US11618553B2 (en) * 2019-11-19 2023-04-04 Ge Aviation Systems Limited Method and process of creating qualifiable parameter data item (PDI) to define the function of a power system controller
CN111240236A (zh) * 2019-12-30 2020-06-05 扬州曙光光电自控有限责任公司 一种基于泵升耗能电阻的负载紧急制动系统及方法
FR3115078B1 (fr) * 2020-10-13 2022-09-09 Safran Nacelles Système d’inversion de poussée pour un aéronef et aéronef comportant un tel système
CN112532116A (zh) * 2020-12-09 2021-03-19 金华市科欣医疗科技有限公司 一种电机电磁刹车的控制电路
FR3129435B1 (fr) 2021-11-25 2024-03-08 Safran Nacelles Ensemble pour aéronef muni d’au moins un système d’actionnement d’inversion de poussée fonctionnant à l’hydrogène.

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5125468A (en) * 1989-06-02 1992-06-30 Coker Theodore R Electric control for wheelchair drive unit
US6684623B2 (en) * 2002-02-27 2004-02-03 Honeywell International, Inc. Gearless electric thrust reverser actuators and actuation system incorporating same
FR2872223B1 (fr) * 2004-06-29 2006-08-25 Hurel Hispano Sa Procede de commande pour l'actionnement d'un inverseur de poussee
FR2920196B1 (fr) * 2007-08-20 2013-08-09 Aircelle Sa Inverseur de poussee avec systeme de freinage des actionneurs
FR2956163B1 (fr) * 2010-02-10 2012-02-17 Aircelle Sa Systeme de commande d'un aeronef
FR2966434B1 (fr) * 2010-10-21 2013-05-31 Sagem Defense Securite Systeme d'actionnement pour un ensemble de propulsion d'un avion

Also Published As

Publication number Publication date
FR2990248B1 (fr) 2015-09-25
US9482183B2 (en) 2016-11-01
FR2990248A1 (fr) 2013-11-08
CN104285055A (zh) 2015-01-14
EP2844860A1 (fr) 2015-03-11
US20150097499A1 (en) 2015-04-09
WO2013164546A1 (fr) 2013-11-07
EP2844860B1 (fr) 2016-03-09
RU2014147908A (ru) 2016-06-27
CA2871729A1 (fr) 2013-11-07

Similar Documents

Publication Publication Date Title
BR112014027471A2 (pt) sistema de controle para o reversor de empuxo com elementos móveis e nacela compreendendo pelo menos um elemento móvel e um sistema de controle.
EP3260706A4 (en) Pyro-type actuator mechanism, injector and igniter assembly
BRPI1008968A2 (pt) sistema de comando de vôo para aeronave, e, aeronave
BR112015024828A2 (pt) método para controlar o fluxo de um poço, método, e sistema para controle de fluxo
BR112015002453A2 (pt) conjunto de superfície de controle, método para testar um conjunto de amortecimento e atuador de superfície de controle.
BR112014029884A2 (pt) sistemas de controle e método.
CL2013001929S1 (es) Accionador para dispositivo de aerosol
DK3079803T3 (da) Indretning til at bestråle styrtegods med accelererede elektroner.
BR112015006986A2 (pt) elemento constituindo uma nacela de aeronave formado de pelo menos uma estrutura compósita e um elemento de aquecimento e estrutura de bordo de ataque.
BRPI1013186A2 (pt) sistema de comando, notadamente de vôo para aeronave
BRPI1007122A2 (pt) bloqueamento de diferencial controlado eletronicamente, sistema de controle adaptado para controlar a operação de um bloqueamento de diferencial controlado eletronicamente
EP2971729A4 (en) VENTILATION SYSTEM WITH DAMAGED CONNECTIONS
BR112015006423A2 (pt) ''projétil, dispositivo lançador de projétil e método para controle de multidões''
BR112015005181A2 (pt) dispositivo reversor de empuxo para uma nacela de motor turbojato e nacela de motor turbojato.
FR3003841B1 (fr) Aeronef muni d'un cockpit a visibilite exterieure optimisee, et procede.
BR112014028465A2 (pt) sistema de controle.
EP3132533A4 (en) Integral preload mechanism for piezoelectric actuator
ITMI20131586A1 (it) Attuatore idraulico lineare interamente integrato
BR112017027338A2 (pt) atuador para válvula de estrangulamento.
EP3656663A4 (en) AIRCRAFT STEERING SYSTEM EQUIPPED WITH AN ELECTROMECHANICAL ACTUATOR
BR112015008102A2 (pt) unidade de ajuste com um atuador e um acionamento para um movimento do atuador e método para montagem do mesmo.
BR112016014138A2 (pt) sistema de acionador pneumático e método para controlar um sistema de acionador pneumático
BR112014024435A2 (pt) método e sistema para controle de pelo menos um regulador de velocidade
BR112015027136A2 (pt) elemento de artigos de entretenimento, sistema de construção que inclui diversos elementos e método para a utilização de um elemento
EP3022398A4 (en) Turbine clearance control utilizing low alpha material

Legal Events

Date Code Title Description
B08F Application fees: dismissal - article 86 of industrial property law
B08K Lapse as no evidence of payment of the annual fee has been furnished to inpi (acc. art. 87)