BR112015025209A2 - sistema de recuperação e de conversão de energia cinética e de energia potencial em energia elétrica para aeronave - Google Patents

sistema de recuperação e de conversão de energia cinética e de energia potencial em energia elétrica para aeronave

Info

Publication number
BR112015025209A2
BR112015025209A2 BR112015025209A BR112015025209A BR112015025209A2 BR 112015025209 A2 BR112015025209 A2 BR 112015025209A2 BR 112015025209 A BR112015025209 A BR 112015025209A BR 112015025209 A BR112015025209 A BR 112015025209A BR 112015025209 A2 BR112015025209 A2 BR 112015025209A2
Authority
BR
Brazil
Prior art keywords
fairing
aircraft
turbine
energy
kinetic
Prior art date
Application number
BR112015025209A
Other languages
English (en)
Inventor
Roques Serge
Original Assignee
Labinal Power Systems
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 Labinal Power Systems filed Critical Labinal Power Systems
Publication of BR112015025209A2 publication Critical patent/BR112015025209A2/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
    • B64D41/00Power installations for auxiliary purposes
    • B64D41/007Ram air turbines
    • 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
    • B64D41/00Power installations for auxiliary purposes
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B60VEHICLES IN GENERAL
    • B60KARRANGEMENT OR MOUNTING OF PROPULSION UNITS OR OF TRANSMISSIONS IN VEHICLES; ARRANGEMENT OR MOUNTING OF PLURAL DIVERSE PRIME-MOVERS IN VEHICLES; AUXILIARY DRIVES FOR VEHICLES; INSTRUMENTATION OR DASHBOARDS FOR VEHICLES; ARRANGEMENTS IN CONNECTION WITH COOLING, AIR INTAKE, GAS EXHAUST OR FUEL SUPPLY OF PROPULSION UNITS IN VEHICLES
    • B60K16/00Arrangements in connection with power supply of propulsion units in vehicles from forces of nature, e.g. sun or wind
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F03MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
    • F03DWIND MOTORS
    • F03D1/00Wind motors with rotation axis substantially parallel to the air flow entering the rotor 
    • F03D1/04Wind motors with rotation axis substantially parallel to the air flow entering the rotor  having stationary wind-guiding means, e.g. with shrouds or channels
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F03MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
    • F03DWIND MOTORS
    • F03D1/00Wind motors with rotation axis substantially parallel to the air flow entering the rotor 
    • F03D1/06Rotors
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F03MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
    • F03DWIND MOTORS
    • F03D9/00Adaptations of wind motors for special use; Combinations of wind motors with apparatus driven thereby; Wind motors specially adapted for installation in particular locations
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F03MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
    • F03DWIND MOTORS
    • F03D9/00Adaptations of wind motors for special use; Combinations of wind motors with apparatus driven thereby; Wind motors specially adapted for installation in particular locations
    • F03D9/10Combinations of wind motors with apparatus storing energy
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F03MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
    • F03DWIND MOTORS
    • F03D9/00Adaptations of wind motors for special use; Combinations of wind motors with apparatus driven thereby; Wind motors specially adapted for installation in particular locations
    • F03D9/10Combinations of wind motors with apparatus storing energy
    • F03D9/11Combinations of wind motors with apparatus storing energy storing electrical energy
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F03MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
    • F03DWIND MOTORS
    • F03D9/00Adaptations of wind motors for special use; Combinations of wind motors with apparatus driven thereby; Wind motors specially adapted for installation in particular locations
    • F03D9/20Wind motors characterised by the driven apparatus
    • F03D9/25Wind motors characterised by the driven apparatus the apparatus being an electrical generator
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F03MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
    • F03DWIND MOTORS
    • F03D9/00Adaptations of wind motors for special use; Combinations of wind motors with apparatus driven thereby; Wind motors specially adapted for installation in particular locations
    • F03D9/30Wind motors specially adapted for installation in particular locations
    • F03D9/32Wind motors specially adapted for installation in particular locations on moving objects, e.g. vehicles
    • 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
    • B64D41/00Power installations for auxiliary purposes
    • B64D2041/002Mounting arrangements for auxiliary power units (APU's)
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05BINDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
    • F05B2220/00Application
    • F05B2220/30Application in turbines
    • F05B2220/31Application in turbines in ram-air turbines ("RATS")
    • YGENERAL 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02EREDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E10/00Energy generation through renewable energy sources
    • Y02E10/70Wind energy
    • Y02E10/72Wind turbines with rotation axis in wind direction
    • YGENERAL 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02EREDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E10/00Energy generation through renewable energy sources
    • Y02E10/70Wind energy
    • Y02E10/728Onshore wind turbines
    • YGENERAL 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02EREDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E70/00Other energy conversion or management systems reducing GHG emissions
    • Y02E70/30Systems combining energy storage with energy generation of non-fossil origin
    • YGENERAL 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00Aeronautics or air transport
    • Y02T50/50On board measures aiming to increase energy efficiency

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Mechanical Engineering (AREA)
  • Combustion & Propulsion (AREA)
  • Sustainable Development (AREA)
  • Sustainable Energy (AREA)
  • Life Sciences & Earth Sciences (AREA)
  • General Engineering & Computer Science (AREA)
  • Power Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Transportation (AREA)
  • Connection Of Motors, Electrical Generators, Mechanical Devices, And The Like (AREA)
  • Other Liquid Machine Or Engine Such As Wave Power Use (AREA)

Abstract

resumo “sistema de recuperação e de conversão de energia cinética e de energia potencial em energia elétrica para aeronave” a invenção se refere a um sistema de geração de energia elétrica (20) para aeronave (10) que compreende uma carenagem aerodinâmica (21) que contém pelo menos uma turbina (23) alojada na parte dianteira (21a) da carenagem (21) e um gerador de energia elétrica (23) ligado à dita turbina. a parte dianteira (21a) da carenagem (21) é equipada com meios de admissão de ar (26) que são móveis entre uma posição de abertura na qual a turbina (22) é exposta ao fluxo de ar externo à carenagem (21) e uma posição de fechamento na qual a turbina (22) é mascarada dentro da carenagem. a invenção permite reduzir a resistência ao avanço aerodinâmica habitualmente criada por turbilhoes presentes na ponta da asa no caso de um velame clássico de bordas nítidas durante as fases de decolagem, subida e cruzeiro e recuperar por ocasião das fases de descida as energias cinética e potencial acumuladas pela aeronave no decorrer das fases de subida e de cruzeiro.
BR112015025209A 2013-04-02 2014-04-01 sistema de recuperação e de conversão de energia cinética e de energia potencial em energia elétrica para aeronave BR112015025209A2 (pt)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1352953A FR3003845B1 (fr) 2013-04-02 2013-04-02 Systeme de recuperation et de conversion d'energie cinetique et d'energie potentielle en energie electrique pour aeronef
PCT/FR2014/050775 WO2014162092A1 (fr) 2013-04-02 2014-04-01 Systeme de recuperation et de conversion d'energie cinetique et d'energie potentielle en energie electrique pour aeronef

Publications (1)

Publication Number Publication Date
BR112015025209A2 true BR112015025209A2 (pt) 2017-07-18

Family

ID=48521336

Family Applications (1)

Application Number Title Priority Date Filing Date
BR112015025209A BR112015025209A2 (pt) 2013-04-02 2014-04-01 sistema de recuperação e de conversão de energia cinética e de energia potencial em energia elétrica para aeronave

Country Status (8)

Country Link
US (1) US9828110B2 (pt)
EP (1) EP2981470B1 (pt)
CN (1) CN105228904B (pt)
BR (1) BR112015025209A2 (pt)
CA (1) CA2908469C (pt)
FR (1) FR3003845B1 (pt)
RU (1) RU2657083C2 (pt)
WO (1) WO2014162092A1 (pt)

Families Citing this family (22)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20170373560A1 (en) * 2014-08-15 2017-12-28 Mohamed Sharkas Mechanical Battery
US9646505B2 (en) 2014-12-23 2017-05-09 Ge Aviation Systems Llc Method of automatically controlling the descent phase of an aircraft using aircraft avionics executing a descent algorithm
CN105173090A (zh) * 2015-07-31 2015-12-23 江苏宏基环电有限公司 一种飞机空调系统
US11371814B2 (en) 2015-08-24 2022-06-28 Leigh Aerosystems Corporation Ground-projectile guidance system
WO2017062563A1 (en) * 2015-10-08 2017-04-13 Leigh Aerosystems Corporation Ground-projectile system
US10227137B2 (en) * 2016-03-22 2019-03-12 Ge Aviation Systems Llc Hybrid power system for an aircraft
RU177509U1 (ru) * 2016-11-25 2018-02-28 Общество С Ограниченной Ответственностью "Ультраконденсаторы Феникс" Электропривод постоянного тока с системой аварийного питания
US10822100B2 (en) * 2017-06-26 2020-11-03 General Electric Company Hybrid electric propulsion system for an aircraft
EP3492386A1 (de) * 2017-12-01 2019-06-05 Dietmar Posch Flugzeug mit stromversorgung
EP3722787B1 (en) 2017-12-07 2024-03-27 Yokogawa Electric Corporation Spectroscopic analyzer
US11465769B2 (en) 2018-01-11 2022-10-11 Hamilton Sundstrand Corporation Electric aircraft having ram air turbines
US10322815B1 (en) 2018-03-22 2019-06-18 Hamilton Sundstrand Corporation Stored electrical energy assisted ram air turbine (RAT) system
CN111216901A (zh) * 2018-11-26 2020-06-02 本田技研工业株式会社 电源装置以及飞行体
EA039004B1 (ru) * 2019-04-01 2021-11-19 Игорь Павлович Константинов Установка воздушно-силовая для летательного аппарата
GB2593416A (en) * 2019-10-02 2021-09-29 Advanced Mobility Res And Development Ltd Systems and methods for aircraft
GB2587668A (en) * 2019-10-02 2021-04-07 Advanced Mobility Res And Development Ltd Systems and methods for aircraft
GB201915634D0 (en) * 2019-10-29 2019-12-11 Univ Coventry An aerodynamic device
US11840353B2 (en) * 2020-09-23 2023-12-12 Zsm Holdings Llc Ram air turbine installation allowing low speed flight
FR3123051A1 (fr) 2021-05-20 2022-11-25 Safran Aircraft Engines Procede et dispositif d’optimisation d’energie electrique d’un aeronef a motorisation hybride
CN113374629B (zh) * 2021-06-16 2023-01-03 上海汉未科技有限公司 一种弹载惯性控制风能采集转换装置及弹载电源
US20220250763A1 (en) * 2022-04-06 2022-08-11 Elijah Abron Charging Wing System for Aircraft
CN114893342B (zh) * 2022-05-18 2024-06-18 中航沈飞民用飞机有限责任公司 一种进气式垂直轴冲压空气涡轮应急能源系统

Family Cites Families (28)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3066889A (en) * 1960-08-22 1962-12-04 Lockheed Aircraft Corp Vtol aircraft
US3130942A (en) * 1963-02-26 1964-04-28 United Aircraft Corp Boundary layer control
US4477040A (en) * 1978-10-19 1984-10-16 Grumman Aerospace Corporation Aircraft wind energy device
DE3208150C2 (de) * 1982-03-06 1983-12-22 Dr.Ing.H.C. F. Porsche Ag, 7000 Stuttgart Betätigungseinrichtung, insbesondere zur Inbetriebnahme einer Stauluftturbine eines Flugzeuges
US5150859A (en) * 1986-12-22 1992-09-29 Sundstrand Corporation Wingtip turbine
US4917332A (en) * 1987-01-05 1990-04-17 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Wingtip vortex turbine
IT1219726B (it) * 1988-06-15 1990-05-24 Fimac Spa Turbina ad elevato rendimento,in particolare per lo sfruttamento di energia eolica per sorgenti ausiliarie di energia in impieghi aeronautici
RU2046735C1 (ru) * 1992-07-30 1995-10-27 Азриэль Ицкович Сарный Летательный аппарат
US5297764A (en) * 1993-03-15 1994-03-29 Haney William R Air foil providing vortex attenuation
US5505587A (en) * 1995-01-05 1996-04-09 Northrop Grumman Corporation RAM air turbine generating apparatus
US5934612A (en) * 1998-03-11 1999-08-10 Northrop Grumman Corporation Wingtip vortex device for induced drag reduction and vortex cancellation
ATE331120T1 (de) * 1998-12-14 2006-07-15 Ghetzler Aero Power Corp Ummanteltes stauluftturbine-generator-system und dessen kühlung
RU2268843C1 (ru) * 2004-04-19 2006-01-27 Тамбовский военный авиационный инженерный институт Система энергетического обеспечения летательного аппарата
US7270214B1 (en) * 2004-06-16 2007-09-18 Westerngeco L.L.C. Method and apparatus for reducing and extracting wing-tip vortex energy
US7922117B2 (en) * 2004-08-30 2011-04-12 Hamilton Sundstrand Corporation Primary panel and motor controller integration for aircraft power distribution system
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
FR2913935B1 (fr) * 2007-03-20 2009-05-15 Airbus France Sas Procede et dispositif de freinage aerodynamique a accumulation d'energie
FR2922520B1 (fr) * 2007-10-22 2010-04-23 Airbus France Procede de reduction de la trainee de compressibilite d'une voilure et conteneur mettant en oeuvre ce procede
GB2461057A (en) * 2008-06-19 2009-12-23 Rolls Royce Plc Ram air turbine
DE102009006242A1 (de) * 2009-01-27 2010-07-29 Friedrich Bock ASPG-AirStreamPowerGeneration
DE102009010243A1 (de) 2009-02-24 2010-09-02 Airbus Deutschland Gmbh Leistungserzeugungs-Vorrichtung sowie Rumpf-Bauteil mit einer solchen Leistungserzeugungs-Vorrichtung
US20110033280A1 (en) * 2009-08-06 2011-02-10 Justak John F Hybrid ram air turbine with inlet guide vanes
US8814081B2 (en) * 2010-12-27 2014-08-26 Rolls-Royce North American Technologies, Inc. Aircraft and external pod for aircraft
US8653688B2 (en) * 2011-05-24 2014-02-18 Advanced Technologies Group, Inc. Submerged ram air turbine generating system
US20120301273A1 (en) * 2011-05-24 2012-11-29 Justak John F Adjustable exhaust apparatus for a ram air turbine generating system
US8678310B2 (en) * 2011-08-22 2014-03-25 Honeywell International Inc. Ducted ram air generator assembly
US9371739B2 (en) * 2013-01-04 2016-06-21 Raytheon Company Power producing device with control mechanism
FR3030453B1 (fr) * 2014-12-19 2018-09-28 Airbus Operations Dispositif auxiliaire de puissance amovible pour aeronef et aeronef adapte a utiliser au moins un tel dispositif.

Also Published As

Publication number Publication date
EP2981470B1 (fr) 2017-06-21
CN105228904B (zh) 2017-12-19
CA2908469A1 (fr) 2014-10-09
US20160031567A1 (en) 2016-02-04
US9828110B2 (en) 2017-11-28
FR3003845A1 (fr) 2014-10-03
RU2015146660A (ru) 2017-05-11
CN105228904A (zh) 2016-01-06
FR3003845B1 (fr) 2016-04-15
EP2981470A1 (fr) 2016-02-10
CA2908469C (fr) 2021-11-23
WO2014162092A1 (fr) 2014-10-09
RU2657083C2 (ru) 2018-06-08

Similar Documents

Publication Publication Date Title
BR112015025209A2 (pt) sistema de recuperação e de conversão de energia cinética e de energia potencial em energia elétrica para aeronave
BR112018009344A2 (pt) veículo aéreo com componentes desdobráveis
BR112015013009A2 (pt) aeronave conversível dotada de dois rotores carenados na extremidade da asa e de uma ventoinha horizontal na fuselagem
EA201491529A1 (ru) Механизм регулировки крыльев
BR112016006370A2 (pt) método para controlar a operação de um mecanismo motor de turbopropulsor de aeronave e sistema de controle de turbopropulsor
EP2772817A3 (en) Formation flight control
BR112015020484A2 (pt) aeronave
GB2548480B (en) Aircraft engine assembly, comprising an engine attachment device equipped with structural movable cowls connected to the central box
ATE492468T1 (de) Luftfahrzeug
WO2014172719A3 (en) A transition arrangement for an aircraft
RU2015126335A (ru) Вспомогательное устройство для высотного самолета
ATE542739T1 (de) Flugzeugflügel
GB201818012D0 (en) Aerodynamic structure for aircraft wing
EP2971656A4 (en) AERODYNAMIC RAIL COVERING FOR THE VENTILATION GEAR OF A GAS TURBINE MOTOR
BR112014017741A8 (pt) Pá de rotor para uma turbina
EP3492374A3 (en) Retrofit flight control surface
BR112013025130A2 (pt) dispositivo de manutenção e de análise de sonda aerodinâmica
BR112012019422A2 (pt) sistema para transportar uma aeronave do local de estacionamento para o local de decolagem e do local de aterrissagem para o local de estacionamento.
EA201500683A1 (ru) Аэродинамическое устройство
BG111219A (en) FLIGHT DEVICE
ES1089054U (es) Pala para aerogeneradores
BR112017012870A2 (pt) dispositivo de separação de óleo destinado a separar gotículas de óleo a partir de um fluxo de gás
ME03099B (me) Uzdužno krilo za avione
RU2013105915A (ru) Способ посадки самолета при боковом ветре /варианты/
UA85001U (ru) Авиационно-космический комплекс

Legal Events

Date Code Title Description
B06F Objections, documents and/or translations needed after an examination request according [chapter 6.6 patent gazette]
B06U Preliminary requirement: requests with searches performed by other patent offices: procedure suspended [chapter 6.21 patent gazette]
B09A Decision: intention to grant [chapter 9.1 patent gazette]
B11D Dismissal acc. art. 38, par 2 of ipl - failure to pay fee after grant in time