BRPI0908328A2 - processo de aplicação dos inversores de propulsão, dispositivo de comando e aeronave - Google Patents

processo de aplicação dos inversores de propulsão, dispositivo de comando e aeronave

Info

Publication number
BRPI0908328A2
BRPI0908328A2 BRPI0908328A BRPI0908328A BRPI0908328A2 BR PI0908328 A2 BRPI0908328 A2 BR PI0908328A2 BR PI0908328 A BRPI0908328 A BR PI0908328A BR PI0908328 A BRPI0908328 A BR PI0908328A BR PI0908328 A2 BRPI0908328 A2 BR PI0908328A2
Authority
BR
Brazil
Prior art keywords
control device
application process
aircraft application
inverters
propulsion
Prior art date
Application number
BRPI0908328A
Other languages
English (en)
Inventor
Phillipe Abrial
Phillipe Feiullard
Original Assignee
Airbus Operations Sas
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 Operations Sas filed Critical Airbus Operations Sas
Publication of BRPI0908328A2 publication Critical patent/BRPI0908328A2/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
    • 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
    • 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
    • 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
    • F05D2270/30—Control parameters, e.g. input parameters
    • F05D2270/304—Spool rotational speed

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Retarders (AREA)
  • Combined Controls Of Internal Combustion Engines (AREA)
  • Control Of Transmission Device (AREA)
  • Electrical Control Of Air Or Fuel Supplied To Internal-Combustion Engine (AREA)
  • Control Of Turbines (AREA)
BRPI0908328A 2008-05-06 2009-04-30 processo de aplicação dos inversores de propulsão, dispositivo de comando e aeronave BRPI0908328A2 (pt)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR0802511A FR2930973B1 (fr) 2008-05-06 2008-05-06 Procede et dispositif de mise en oeuvre des inverseurs de poussee d'un aeronef
PCT/FR2009/000516 WO2009138598A2 (fr) 2008-05-06 2009-04-30 Procédé et dispositif de mise en oeuvre des inverseurs de poussée d'un aéronef

Publications (1)

Publication Number Publication Date
BRPI0908328A2 true BRPI0908328A2 (pt) 2016-07-05

Family

ID=40011094

Family Applications (1)

Application Number Title Priority Date Filing Date
BRPI0908328A BRPI0908328A2 (pt) 2008-05-06 2009-04-30 processo de aplicação dos inversores de propulsão, dispositivo de comando e aeronave

Country Status (9)

Country Link
US (1) US8733698B2 (pt)
EP (1) EP2297438B1 (pt)
JP (1) JP5480888B2 (pt)
CN (1) CN102105666B (pt)
BR (1) BRPI0908328A2 (pt)
CA (1) CA2721378C (pt)
FR (1) FR2930973B1 (pt)
RU (1) RU2449153C1 (pt)
WO (1) WO2009138598A2 (pt)

Families Citing this family (19)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
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.
FR2958978B1 (fr) * 2010-04-20 2014-04-18 Aircelle Sa Agencement de bielles de volets d'inversion de poussee sur la structure interne fixe d'une nacelle de turboreacteur
FR2992685B1 (fr) 2012-07-02 2016-05-27 Aircelle Sa Procede de commande d'une section de tuyere variable d'un aeronef
CN102787994B (zh) * 2012-08-25 2014-06-11 冯益安 喷气式汽车喷气减速动力机
FR2999656B1 (fr) * 2012-12-17 2017-11-17 Snecma Optimisation de la disponibilite d'un inverseur de poussee
US9650994B2 (en) * 2014-07-30 2017-05-16 The Boeing Company Thrust reverser actuator systems
US10443540B2 (en) 2015-05-08 2019-10-15 United Technologies Corporation Thrust reversal for turbofan gas turbine engine
US10497271B2 (en) * 2016-12-12 2019-12-03 The Boeing Company Runway exiting systems and methods for aircraft
FR3064602B1 (fr) * 2017-03-29 2019-06-07 Airbus Operations Mode de fonctionnement degrade d'un groupe propulseur d'aeronef permettant le deplafonnement d'une consigne de poussee
US10343786B2 (en) * 2017-06-28 2019-07-09 General Electric Company System and method of operating a ducted fan propulsion system during aircraft taxi
US10119495B1 (en) * 2017-06-28 2018-11-06 General Electric Company System and method of operating a ducted fan propulsion system inflight
US10703498B2 (en) * 2017-11-02 2020-07-07 The Boeing Company Methods and aircraft for optimized reverse thrust operation during landing
FR3092819A1 (fr) * 2019-02-18 2020-08-21 Airbus Operations Nacelle d’un turboreacteur comportant une porte de blocage et un systeme de deploiement de la porte de blocage
FR3093993B1 (fr) * 2019-03-21 2021-02-26 Safran Aircraft Engines Procédé de contrôle du freinage des roues d’un avion et contrôleur de freinage de roues associé
US11414175B2 (en) 2019-04-01 2022-08-16 Pratt & Whitney Canada Corp. Method and system for operating an aircraft powerplant
US20200370510A1 (en) * 2019-05-21 2020-11-26 Pratt & Whitney Canada Corp. Method and system for operating an aircraft powerplant
RU2719778C1 (ru) * 2019-09-05 2020-04-23 Акционерное общество "Объединенная двигателестроительная корпорация" (АО "ОДК") Способ управления реверсивным устройством авиационного двигателя при торможении самолета
FR3105804B1 (fr) * 2019-12-30 2021-12-03 Safran Nacelles Système de pilotage d’un moyen d’inversion de poussée d’un aéronef
CN111679691A (zh) * 2020-07-16 2020-09-18 深圳市澳玛禾经贸有限公司 一种飞行器的避障控制系统、方法及飞行器

Family Cites Families (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3168880A (en) * 1962-09-25 1965-02-09 Singer Co Stands for sewing machine cabinets
US3618880A (en) * 1970-05-11 1971-11-09 Boeing Co Speed brake system for aircraft spoilers
DE2354747A1 (de) * 1973-11-02 1975-05-07 Motoren Turbinen Union Vorrichtung zur steuerung einer schubumkehrvorrichtung
FR2580034B1 (pt) * 1985-04-03 1987-05-29 Aerospatiale
GB9015373D0 (en) * 1990-07-12 1990-08-29 Rolls Royce Plc Gas turbine engine thrust reverser control
US5259187A (en) * 1993-02-05 1993-11-09 General Electric Company Method of operating an aircraft bypass turbofan engine having variable fan outlet guide vanes
GB9418476D0 (en) * 1994-09-14 1994-11-02 Dunlop Ltd Sequential selective operation of aircraft brakes
FR2749041B1 (fr) * 1996-05-23 1998-06-26 Hispano Suiza Sa Inverseur de poussee de turboreacteur a double flux a obstacles lies au capot primaire
FR2755730B1 (fr) * 1996-11-14 1999-01-08 Hispano Suiza Sa Systeme de commande electrique pour inverseur de poussee de turboreacteur
FR2846375B1 (fr) * 2002-10-25 2006-06-30 Hispano Suiza Sa Inverseur de poussee electromacanique pour turboreacteur a asservissement du deplacement des portes
FR2846376B1 (fr) * 2002-10-25 2005-01-28 Hispano Suiza Sa Platine de maintenance et d'inhibition pour inverseur de poussee
FR2859176B1 (fr) * 2003-09-03 2005-10-28 Airbus France Aeronef pourvu d'inverseurs de poussee
FR2872223B1 (fr) * 2004-06-29 2006-08-25 Hurel Hispano Sa Procede de commande pour l'actionnement d'un inverseur de poussee
US9043050B2 (en) * 2008-08-13 2015-05-26 The Boeing Company Programmable reverse thrust detent system and method

Also Published As

Publication number Publication date
RU2449153C1 (ru) 2012-04-27
CA2721378C (fr) 2015-09-29
US20110108665A1 (en) 2011-05-12
CA2721378A1 (fr) 2009-11-19
CN102105666B (zh) 2013-10-02
JP5480888B2 (ja) 2014-04-23
US8733698B2 (en) 2014-05-27
EP2297438A2 (fr) 2011-03-23
JP2011519776A (ja) 2011-07-14
FR2930973B1 (fr) 2010-04-23
CN102105666A (zh) 2011-06-22
EP2297438B1 (fr) 2014-07-16
FR2930973A1 (fr) 2009-11-13
WO2009138598A3 (fr) 2010-01-07
WO2009138598A2 (fr) 2009-11-19

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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]
B350 Update of information on the portal [chapter 15.35 patent gazette]