BRPI1008282A2 - sistema gerador de força para integração em um sistema de aeronave - Google Patents

sistema gerador de força para integração em um sistema de aeronave

Info

Publication number
BRPI1008282A2
BRPI1008282A2 BRPI1008282A BRPI1008282A BRPI1008282A2 BR PI1008282 A2 BRPI1008282 A2 BR PI1008282A2 BR PI1008282 A BRPI1008282 A BR PI1008282A BR PI1008282 A BRPI1008282 A BR PI1008282A BR PI1008282 A2 BRPI1008282 A2 BR PI1008282A2
Authority
BR
Brazil
Prior art keywords
integration
power generator
aircraft
generator system
aircraft system
Prior art date
Application number
BRPI1008282A
Other languages
English (en)
Inventor
Sten Gatzke
Original Assignee
Airbus Operations Gmbh
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 Gmbh filed Critical Airbus Operations Gmbh
Publication of BRPI1008282A2 publication Critical patent/BRPI1008282A2/pt

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F03—MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
    • F03D—WIND MOTORS
    • F03D9/00—Adaptations of wind motors for special use; Combinations of wind motors with apparatus driven thereby; Wind motors specially adapted for installation in particular locations
    • F03D9/30—Wind motors specially adapted for installation in particular locations
    • F03D9/32—Wind motors specially adapted for installation in particular locations on moving objects, e.g. vehicles
    • 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
    • B64D41/00—Power installations for auxiliary purposes
    • B64D41/007—Ram air turbines
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F03—MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
    • F03D—WIND MOTORS
    • F03D1/00—Wind motors with rotation axis substantially parallel to the air flow entering the rotor 
    • F03D1/04—Wind motors with rotation axis substantially parallel to the air flow entering the rotor  having stationary wind-guiding means, e.g. with shrouds or channels
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F03—MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
    • F03D—WIND MOTORS
    • F03D17/00—Monitoring or testing of wind motors, e.g. diagnostics
    • 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
    • B64D2241/00—NACA type air intakes
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F03—MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
    • F03D—WIND MOTORS
    • F03D9/00—Adaptations of wind motors for special use; Combinations of wind motors with apparatus driven thereby; Wind motors specially adapted for installation in particular locations
    • F03D9/20—Wind motors characterised by the driven apparatus
    • F03D9/25—Wind motors characterised by the driven apparatus the apparatus being an electrical generator
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05B—INDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
    • F05B2220/00—Application
    • F05B2220/50—Application for auxiliary power units (APU's)
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05B—INDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
    • F05B2240/00—Components
    • F05B2240/90—Mounting on supporting structures or systems
    • F05B2240/92—Mounting on supporting structures or systems on an airbourne structure
    • F05B2240/921—Mounting on supporting structures or systems on an airbourne structure kept aloft due to aerodynamic effects
    • 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
    • Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E10/00—Energy generation through renewable energy sources
    • Y02E10/70—Wind energy
    • Y02E10/72—Wind turbines with rotation axis in wind direction
    • 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
    • Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E10/00—Energy generation through renewable energy sources
    • Y02E10/70—Wind energy
    • Y02E10/728—Onshore wind turbines

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Sustainable Development (AREA)
  • Sustainable Energy (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Life Sciences & Earth Sciences (AREA)
  • General Engineering & Computer Science (AREA)
  • Power Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Wind Motors (AREA)
  • Connection Of Motors, Electrical Generators, Mechanical Devices, And The Like (AREA)
  • Stand-By Power Supply Arrangements (AREA)
  • Lock And Its Accessories (AREA)
BRPI1008282A 2009-02-24 2010-02-24 sistema gerador de força para integração em um sistema de aeronave BRPI1008282A2 (pt)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US15499009P 2009-02-24 2009-02-24
DE102009010243A DE102009010243A1 (de) 2009-02-24 2009-02-24 Leistungserzeugungs-Vorrichtung sowie Rumpf-Bauteil mit einer solchen Leistungserzeugungs-Vorrichtung
PCT/EP2010/001151 WO2010097213A2 (de) 2009-02-24 2010-02-24 Leistungserzeugungs-system zur integration in einer flugzeugsystem

Publications (1)

Publication Number Publication Date
BRPI1008282A2 true BRPI1008282A2 (pt) 2016-03-15

Family

ID=42371675

Family Applications (1)

Application Number Title Priority Date Filing Date
BRPI1008282A BRPI1008282A2 (pt) 2009-02-24 2010-02-24 sistema gerador de força para integração em um sistema de aeronave

Country Status (9)

Country Link
US (1) US8967530B2 (pt)
EP (1) EP2401203B1 (pt)
JP (1) JP5216146B2 (pt)
CN (1) CN102333699B (pt)
BR (1) BRPI1008282A2 (pt)
CA (1) CA2753122A1 (pt)
DE (1) DE102009010243A1 (pt)
RU (1) RU2489323C2 (pt)
WO (1) WO2010097213A2 (pt)

Families Citing this family (32)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP3013300B2 (ja) 1997-07-25 2000-02-28 アキレス株式会社 板状複合断熱材
DE102009010243A1 (de) 2009-02-24 2010-09-02 Airbus Deutschland Gmbh Leistungserzeugungs-Vorrichtung sowie Rumpf-Bauteil mit einer solchen Leistungserzeugungs-Vorrichtung
FR2946955B1 (fr) * 2009-06-17 2012-09-21 Airbus Aeronef pourvu d'un systeme de pile a combustible.
TR201901397T4 (tr) 2011-05-13 2019-02-21 Leigh Aerosystems Corp Karadan fırlatılan roket güdüm sistemi.
US20120301273A1 (en) * 2011-05-24 2012-11-29 Justak John F Adjustable exhaust apparatus for a ram air turbine generating system
ES2398316B1 (es) * 2011-07-18 2014-04-29 Airbus Operations, S.L. Sistema versátil de potencia en aeronaves
US8678310B2 (en) * 2011-08-22 2014-03-25 Honeywell International Inc. Ducted ram air generator assembly
US9051057B2 (en) * 2011-12-28 2015-06-09 Embraer S.A. Aircraft air inlet diverter assemblies with improved aerodynamic characteristics
US20130181448A1 (en) * 2012-01-17 2013-07-18 Hamilton Sundstrand Corporation Electric actuators in aircraft systems
FR2993536B1 (fr) * 2012-07-23 2015-03-20 Hispano Suiza Sa Dispositif d'alimentation de secours pour aeronef et aeronef pourvu d'un tel dispositif
US9371739B2 (en) 2013-01-04 2016-06-21 Raytheon Company Power producing device with control mechanism
US9416730B2 (en) * 2013-01-31 2016-08-16 The Boeing Company Bi-directional ventilation systems for use with aircraft and related methods
FR3003845B1 (fr) * 2013-04-02 2016-04-15 Labinal Systeme de recuperation et de conversion d'energie cinetique et d'energie potentielle en energie electrique pour aeronef
WO2017035126A1 (en) 2015-08-24 2017-03-02 Leigh Aerosystems Corporation Ground-projectile guidance system
US10280786B2 (en) * 2015-10-08 2019-05-07 Leigh Aerosystems Corporation Ground-projectile system
FR3042237B1 (fr) * 2015-10-09 2017-11-03 Labinal Power Systems Dispositif d'actionnement pour systeme d'eolienne de secours d'aeronef
US10273823B2 (en) * 2016-05-20 2019-04-30 United Technologies Corporation Inlet door state control system
CN106285795A (zh) * 2016-09-05 2017-01-04 中国商用飞机有限责任公司 冲压空气涡轮发电系统
US10118715B2 (en) 2017-02-20 2018-11-06 Pratt & Whitney Canada Corp. System and method for auxiliary power unit inlet door testing
US10239632B2 (en) 2017-02-20 2019-03-26 Pratt & Whitney Canada Corp. System and method for controlling an auxiliary power unit inlet door
US10435168B2 (en) 2017-02-20 2019-10-08 Pratt & Whitney Canada Corp. System and method for controlling a position of an auxiliary power unit inlet door
US10232951B2 (en) 2017-02-20 2019-03-19 Pratt & Whitney Canada Corp. System and method for selecting an opening angle of an auxiliary power unit inlet door
US20180257788A1 (en) * 2017-03-09 2018-09-13 United Technologies Corporation Air intake assembly with horizontal door for an aircraft auxiliary power unit
EP3492386A1 (de) * 2017-12-01 2019-06-05 Dietmar Posch Flugzeug mit stromversorgung
CN108275273B (zh) * 2018-03-08 2024-04-02 东莞理工学院 无人机
CN111268150B (zh) * 2018-12-04 2023-01-24 中国航空工业集团公司金城南京机电液压工程研究中心 一种涵道式冲压空气涡轮应急能源系统
DE102021113818B4 (de) 2021-05-28 2023-06-15 Elektro-Metall Export Gesellschaft mit beschränkter Haftung Flugzeug, insbesondere Passagier-Flugzeug
EP4282765B1 (en) * 2022-05-27 2025-07-02 Airbus Operations, S.L.U. Auxiliary power unit system of an aircraft
CN114872908B (zh) * 2022-06-08 2024-03-26 中国航空发动机研究院 一种喷管装置及航空发动机
CN114954964B (zh) * 2022-06-08 2024-04-16 中国航空发动机研究院 一种喷管装置及航空发动机
US11784536B1 (en) 2022-07-14 2023-10-10 Daniel Webb Method and apparatus for collecting thrust to generate power or useful energy
US20260092580A1 (en) * 2024-09-30 2026-04-02 Hamilton Sundstrand Corporation Ram air turbine fixed within aircraft

Family Cites Families (25)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1032033B (de) 1956-07-12 1958-06-12 Plessey Co Ltd Stauluftturbine als Kraftquelle fuer Hilfsapparate bei einem Gasturbinenflugzeug
US4418879A (en) * 1980-12-29 1983-12-06 The Boeing Company Scoop and inlet for auxiliary power units and method
JPS57131845A (en) * 1981-02-06 1982-08-14 Nissan Motor Co Ltd Ram rocket
US4456204A (en) * 1981-09-29 1984-06-26 The Boeing Company Deployable inlet for aeroplane center boost engine
SU1817623A1 (ru) * 1991-04-29 1995-09-20 Авиационный научно-технический комплекс им.А.Н.Туполева Система электроснабжения летательного аппарата
JPH1179096A (ja) * 1997-09-04 1999-03-23 Toyota Motor Corp 航空機用揚力増加装置
US6272838B1 (en) * 1999-02-25 2001-08-14 Alliedsignal, Inc. Method and apparatus for controlling the inlet duct leading to an auxiliary power unit
US6247668B1 (en) * 1999-07-15 2001-06-19 The Boeing Company Auxiliary power and thrust unit
GB9926354D0 (en) * 1999-11-08 2000-01-12 Rolls Royce Plc Power supply system for an aircraft
US6651929B2 (en) * 2001-10-29 2003-11-25 Pratt & Whitney Canada Corp. Passive cooling system for auxiliary power unit installation
US7210653B2 (en) 2002-10-22 2007-05-01 The Boeing Company Electric-based secondary power system architectures for aircraft
US7014144B2 (en) * 2003-07-22 2006-03-21 Honeywell International, Inc. Dual action inlet door and method for use thereof
DE10335482B4 (de) * 2003-08-02 2008-04-03 Airbus Deutschland Gmbh Staulufteinlass eines Flugzeuges
US7364116B2 (en) * 2004-09-27 2008-04-29 The Boeing Company Automatic control systems for aircraft auxiliary power units, and associated methods
US7344107B2 (en) 2004-10-26 2008-03-18 The Boeing Company Dual flow APU inlet and associated systems and methods
CN101171147B (zh) 2005-03-18 2011-07-06 看门人系统公司 轮式物体的动力发电系统和方法
US7469545B2 (en) * 2005-09-27 2008-12-30 Honeywell International Inc. Auxiliary power unit inlet door position control system and method
DE102006003138A1 (de) * 2006-01-24 2007-08-02 Airbus Deutschland Gmbh Notversorgungsaggregat mit einer durch einen Luftstrom antreibbaren Staudruckturbine und mit einem Energiewandler für Luftfahrzeuge
US7540142B2 (en) * 2006-02-21 2009-06-02 Honeywell International Inc. Multiple auxiliary power unit system inlet ducts controlled by a single actuator
US7600714B2 (en) * 2006-04-20 2009-10-13 Honeywell International Inc. Diffusing air inlet door assembly
JP2008080934A (ja) * 2006-09-27 2008-04-10 Honeywell Internatl Inc 補助動力装置の取入口ドア位置制御の装置及び方法
US7775147B2 (en) * 2008-03-17 2010-08-17 Raytheon Company Dual redundant electro explosive device latch mechanism
US8141816B2 (en) * 2008-04-30 2012-03-27 Honeywell International Inc. AFT inlet duct mounted door actuator
DE102009010243A1 (de) 2009-02-24 2010-09-02 Airbus Deutschland Gmbh Leistungserzeugungs-Vorrichtung sowie Rumpf-Bauteil mit einer solchen Leistungserzeugungs-Vorrichtung
US8882028B2 (en) * 2009-09-21 2014-11-11 Aerion Corporation Aircraft emergency and backup secondary power apparatus

Also Published As

Publication number Publication date
US20120006938A1 (en) 2012-01-12
EP2401203A2 (de) 2012-01-04
US8967530B2 (en) 2015-03-03
EP2401203B1 (de) 2013-02-13
WO2010097213A2 (de) 2010-09-02
DE102009010243A1 (de) 2010-09-02
CN102333699B (zh) 2015-06-03
CA2753122A1 (en) 2010-09-02
WO2010097213A3 (de) 2010-11-25
RU2489323C2 (ru) 2013-08-10
JP5216146B2 (ja) 2013-06-19
JP2012518569A (ja) 2012-08-16
RU2011138959A (ru) 2013-04-10
CN102333699A (zh) 2012-01-25

Similar Documents

Publication Publication Date Title
BRPI1008282A2 (pt) sistema gerador de força para integração em um sistema de aeronave
CU24141B1 (es) Sistema generador de energía
BR112012018333A2 (pt) aquecedor alongado para um sistema de geração de aerossol de aquecedor elétrico
BR112012017210A2 (pt) método de geração de energia elétrica, sistema de geração de energia elétrica, método de uso de um sistema
GB0912340D0 (en) Aircraft power management system
BR112012001369A2 (pt) sistema de gerenciamento de energia
BRPI0922404A2 (pt) automação de alimentador para um sistema de distribuição de potência elétrica
BR112013011093A2 (pt) sistema de fornecimento de energia para veículo incluindo o mesmo
BRPI0922859A2 (pt) sistema autônomo de potência elétrica distribuída
BRPI1007681A2 (pt) sistema de para ventos
BRPI1012304A2 (pt) sistema para auxílio de subida
DK2312744T3 (da) Effektfordelingssystemer
IL263732A (en) System and method for energy conversion
DE102011005729A8 (de) Fahrzeugenergiesystem
BR112012003082A2 (pt) articulação para uma unidade de sistema de distribuição de potência de aeronave e unidade de sistema de distribuição de potência para uma aeronave
BRPI1005983A2 (pt) sistema para conrole de unidade de equipamento eletrico
BRPI1100017A2 (pt) sistema de gerador de turbina eolica, e, gerador de turbina eolica
BR112012006991A2 (pt) método para configurar um dispositivo de entretenimento
BRPI1008754A2 (pt) sistema de alimentação central
BRPI0906171A2 (pt) Nacela de aeronave
BRPI1006835A2 (pt) sistema para gerar energia elétrica por meio de elementos fotovoltaicos
BR112013015888A2 (pt) sistema de unidade extraível para um dispositivo disjuntor elétrico.
BR112014000233A2 (pt) sistema de flape para uma aeronave
BRPI1013186A2 (pt) sistema de comando, notadamente de vôo para aeronave
BR112013030445A2 (pt) sistema de geração de energia.

Legal Events

Date Code Title Description
B08F Application fees: application dismissed [chapter 8.6 patent gazette]

Free format text: REFERENTE AS 4A, 5A E 6A ANUIDADES.

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 2383 DE 06-09-2016 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.