BR112013002327A2 - dispositivo de acionamento elétrico para uma aeronave - Google Patents
dispositivo de acionamento elétrico para uma aeronaveInfo
- Publication number
- BR112013002327A2 BR112013002327A2 BR112013002327A BR112013002327A BR112013002327A2 BR 112013002327 A2 BR112013002327 A2 BR 112013002327A2 BR 112013002327 A BR112013002327 A BR 112013002327A BR 112013002327 A BR112013002327 A BR 112013002327A BR 112013002327 A2 BR112013002327 A2 BR 112013002327A2
- Authority
- BR
- Brazil
- Prior art keywords
- dynamoelectric machine
- aircraft
- rotor
- electric drive
- drive device
- Prior art date
Links
- 239000003507 refrigerant Substances 0.000 abstract 1
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
- B64D35/00—Transmitting power from power plants to propellers or rotors; Arrangements of transmissions
- B64D35/02—Transmitting power from power plants to propellers or rotors; Arrangements of transmissions specially adapted for specific power plants
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/04—Helicopters
- B64C27/12—Rotor drives
-
- 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
- B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
- B64D27/02—Aircraft characterised by the type or position of power plants
- B64D27/24—Aircraft characterised by the type or position of power plants using steam or spring force
-
- 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
- B64D35/00—Transmitting power from power plants to propellers or rotors; Arrangements of transmissions
- B64D35/02—Transmitting power from power plants to propellers or rotors; Arrangements of transmissions specially adapted for specific power plants
- B64D35/021—Transmitting power from power plants to propellers or rotors; Arrangements of transmissions specially adapted for specific power plants for electric power plants
-
- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02K—DYNAMO-ELECTRIC MACHINES
- H02K16/00—Machines with more than one rotor or stator
- H02K16/04—Machines with one rotor and two stators
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/04—Helicopters
-
- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02K—DYNAMO-ELECTRIC MACHINES
- H02K7/00—Arrangements for handling mechanical energy structurally associated with dynamo-electric machines, e.g. structural association with mechanical driving motors or auxiliary dynamo-electric machines
- H02K7/08—Structural association with bearings
- H02K7/09—Structural association with bearings with magnetic bearings
-
- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02K—DYNAMO-ELECTRIC MACHINES
- H02K7/00—Arrangements for handling mechanical energy structurally associated with dynamo-electric machines, e.g. structural association with mechanical driving motors or auxiliary dynamo-electric machines
- H02K7/10—Structural association with clutches, brakes, gears, pulleys or mechanical starters
- H02K7/116—Structural association with clutches, brakes, gears, pulleys or mechanical starters with gears
-
- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02K—DYNAMO-ELECTRIC MACHINES
- H02K9/00—Arrangements for cooling or ventilating
-
- 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)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Power Engineering (AREA)
- Connection Of Motors, Electrical Generators, Mechanical Devices, And The Like (AREA)
- Motor Or Generator Cooling System (AREA)
- Permanent Magnet Type Synchronous Machine (AREA)
- Retarders (AREA)
Abstract
dispositivo de acionamento elétrico para uma aeronave. a presente invenção refere-se a um acionamento elétrico (1) para uma aeronave, especialmente para um helicóptero (20) compreendendo pelo menos um rotor (23) que é diretamente acionado por uma máquina dinamoelétrica (2). a máquina dinamoelétrica (2) é incorporada em um arranjo duplex, um rotor (6) arranjado em um espaço de ar (12), compreendendo magnetos permanentes (13) em um dispositivo transportador (14), e os estatores (4, 5) da máquina dinamoelétrica (2) e/ou o rotor (6) compreendendo um refrigerante. a engrenagem planetária (3) é especialmente proporcionada entre o rotor acionado e a máquina dinamoelétrica (2), preferivelmente na extensão axial da máquina dinamoelétrica (2).
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
EP10171433A EP2413483A1 (de) | 2010-07-30 | 2010-07-30 | Elektrische Antriebsvorrichtung für ein Luftfahrzeug |
PCT/EP2011/062633 WO2012013594A2 (de) | 2010-07-30 | 2011-07-22 | Elektrische antriebsvorrichtung für ein luftfahrzeug |
Publications (2)
Publication Number | Publication Date |
---|---|
BR112013002327A2 true BR112013002327A2 (pt) | 2016-05-24 |
BR112013002327A8 BR112013002327A8 (pt) | 2016-10-18 |
Family
ID=43530693
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
BR112013002327A BR112013002327A8 (pt) | 2010-07-30 | 2011-07-22 | dispositivo de acionamento elétrico para uma aeronave |
Country Status (6)
Country | Link |
---|---|
US (1) | US20130126669A1 (pt) |
EP (2) | EP2413483A1 (pt) |
CN (1) | CN103026600B (pt) |
BR (1) | BR112013002327A8 (pt) |
RU (1) | RU2547938C2 (pt) |
WO (1) | WO2012013594A2 (pt) |
Families Citing this family (31)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE102012206144A1 (de) | 2012-04-16 | 2013-10-17 | Siemens Aktiengesellschaft | Antriebsvorrichtung für einen Kraftwagen |
FR2993727B1 (fr) * | 2012-07-19 | 2017-07-21 | Eurocopter France | Machine electrique reversible pour aeronef |
GB2515766A (en) * | 2013-07-02 | 2015-01-07 | David Rodger | Reducing bearing forces in an electrical machine |
EP3038904B1 (en) * | 2013-08-28 | 2018-08-08 | Sikorsky Aircraft Corporation | Propeller gearbox oil cooler for a rotary wing aircraft |
DE102013219724A1 (de) * | 2013-09-30 | 2015-04-02 | Siemens Aktiengesellschaft | Elektrisch angetriebenes Flugzeug |
JP5887634B2 (ja) | 2014-02-20 | 2016-03-16 | 北田 保雄 | 電気回転機 |
DE102015105787A1 (de) * | 2015-04-15 | 2016-10-20 | Johann Schwöller | Elektroantrieb für ein Luftfahrzeug und Hybridsystem für ein Luftfahrzeug |
CA2932102C (en) | 2015-06-10 | 2024-04-30 | Rolls-Royce Corporation | Fault identification and isolation in an electric propulsion system |
EP3104519B1 (en) | 2015-06-11 | 2021-08-04 | Rolls-Royce North American Technologies, Inc. | Varying quantities of motor poles for noise reduction |
US11186363B2 (en) | 2015-10-21 | 2021-11-30 | Sikorsky Aircraft Corporation | Electric propulsion system for a rotary wing aircraft |
US9828089B2 (en) * | 2016-01-29 | 2017-11-28 | Sikorsky Aircraft Corporation | Rotor drive systems for rotorcraft |
WO2018029227A1 (de) * | 2016-08-10 | 2018-02-15 | Siemens Aktiengesellschaft | Stationäres hubschrauber-trainingsgerät |
WO2018056561A1 (ko) * | 2016-09-23 | 2018-03-29 | 탁승호 | 무정지 모터 |
US10752343B2 (en) * | 2016-10-18 | 2020-08-25 | Sikorsky Aircraft Corporation | Electric propulsion system for a rotary wing aircraft |
DE102016223038A1 (de) | 2016-11-22 | 2018-05-24 | Volkswagen Aktiengesellschaft | Kühleinrichtung für elektrische Maschine |
US10577090B2 (en) * | 2017-02-16 | 2020-03-03 | Sikorsky Aircraft Corporation | Electric propulsion system with overrunning clutch for a rotary-wing aircraft |
GB201708297D0 (en) * | 2017-05-24 | 2017-07-05 | Rolls Royce Plc | Preventing electrical breakdown |
GB201708289D0 (en) | 2017-05-24 | 2017-07-05 | Rolls Royce Plc | Preventing electrical breakdown |
US10676182B2 (en) | 2017-07-20 | 2020-06-09 | Sikorsky Aircraft Corporation | Tilting coaxial rotor for a rotary wing aircraft |
US10974824B2 (en) | 2017-07-20 | 2021-04-13 | Sikorsky Aircraft Corporation | Electric powered direct drive rotor motor |
US10443620B2 (en) * | 2018-01-02 | 2019-10-15 | General Electric Company | Heat dissipation system for electric aircraft engine |
US10407166B2 (en) | 2018-01-08 | 2019-09-10 | Sikorsky Aircraft Corporation | Yaw moment supplement for directional control |
DE102018202172A1 (de) * | 2018-02-13 | 2019-08-14 | Siemens Aktiengesellschaft | Antriebsvorrichtung für ein Luftfahrzeug mit elektrischer Maschine und Kühleinrichtung |
CN109263863A (zh) * | 2018-08-23 | 2019-01-25 | 陈国宝 | 风洞推进器 |
US11735988B2 (en) * | 2019-01-31 | 2023-08-22 | General Electric Company | Dual rotor electric machine |
CH715823A1 (de) * | 2019-02-07 | 2020-08-14 | Kopter Group Ag | Antriebseinheit, insbesondere für den Hauptrotor eines Drehflüglers. |
GB202019212D0 (en) * | 2020-12-07 | 2021-01-20 | J And M Ferranti Tech Limited | Propulsion systems for aircraft |
CN114838037B (zh) * | 2022-04-20 | 2022-10-25 | 北京理工大学 | 一种轮毂电液复合驱动总成及控制方法 |
DE102022118426B4 (de) | 2022-07-22 | 2024-05-23 | Auma Riester Gmbh & Co. Kg | Planetengetriebe |
US11787551B1 (en) | 2022-10-06 | 2023-10-17 | Archer Aviation, Inc. | Vertical takeoff and landing aircraft electric engine configuration |
CN117780894B (zh) * | 2024-02-23 | 2024-05-03 | 北京中科科美科技股份有限公司 | 一种真空设备中高扭矩密封传动装置 |
Family Cites Families (22)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS5479409A (en) | 1977-12-07 | 1979-06-25 | Mabuchi Motor Co | Rotary unit |
DE3915526A1 (de) | 1989-02-13 | 1990-08-16 | Rolf Hopf | Duplexelektromotor |
JPH03237295A (ja) | 1990-02-09 | 1991-10-23 | Shimadzu Corp | ターボ分子ポンプ |
KR0130534B1 (ko) * | 1994-07-12 | 1998-04-09 | 김광호 | 세탁기용 리니어 모터 |
US6308912B1 (en) * | 1997-10-21 | 2001-10-30 | Natural Colour Kari Kirjavainen Oy | Rotorcraft |
DE19856647B4 (de) | 1998-12-09 | 2007-03-01 | Canders, Wolf-R., Prof. Dr.-Ing. | Elektrischer Hochmomentmotor |
RU2266236C2 (ru) * | 2003-09-09 | 2005-12-20 | Хамин Иван Никифорович | Летательный аппарат с электроприводом |
US7154191B2 (en) * | 2004-06-30 | 2006-12-26 | General Electric Company | Electrical machine with double-sided rotor |
US7839048B2 (en) * | 2004-09-27 | 2010-11-23 | General Electric Company | Electrical machine with double-sided stator |
CN1909340A (zh) | 2005-08-01 | 2007-02-07 | 张孟杰 | 增效永磁发电机 |
JP2009506739A (ja) | 2005-08-24 | 2009-02-12 | クールマン−ウィルスドルフ・モーターズ・エルエルシー | Mp−a及びmp−tマシン、交流及び三相交流電流のための多極マシン |
US7750521B2 (en) | 2006-12-07 | 2010-07-06 | General Electric Company | Double-sided starter/generator for aircrafts |
CN201113670Y (zh) | 2007-10-25 | 2008-09-10 | 新疆金风科技股份有限公司 | 双定子半直驱式永磁同步风力发电机 |
DE202008002249U1 (de) * | 2008-02-18 | 2008-04-17 | Dill, Hans-Dieter | Fluggerät mit einer Brennkraftmaschine sowie einem Elektro-Antriebsmotor |
CN201206076Y (zh) * | 2008-03-20 | 2009-03-11 | 浙江西子富沃德电机有限公司 | 双定子永磁同步无齿轮曳引机 |
WO2009143669A1 (zh) | 2008-05-27 | 2009-12-03 | Tian Yu | 飞行器及其动力驱动系统 |
CN101337501B (zh) * | 2008-08-12 | 2011-05-18 | 卢旻 | 一种车轮、车辆、火车、飞行车和直升机 |
BRPI0823037A2 (pt) * | 2008-08-22 | 2015-07-28 | Smidth As F L | Disposição de acionamento de serviço pesado para um moinho que tem uma bacia de moedura giratória em torno da vertical que compreende um alojamento, um motor elétrico e uma disposição de engrenagem |
DE202008012191U1 (de) | 2008-09-15 | 2008-11-27 | Geiger Engineering | Elektrisches Antriebssystem |
US8183802B2 (en) * | 2009-01-05 | 2012-05-22 | Eric Stephane Quere | Composite electromechanical machines with controller |
US20110042967A1 (en) * | 2009-08-19 | 2011-02-24 | Winter Curt B | Electric generator driven by combustion engine and having fluid cooling |
JP5477161B2 (ja) * | 2010-05-20 | 2014-04-23 | 株式会社デンソー | ダブルステータ型モータ |
-
2010
- 2010-07-30 EP EP10171433A patent/EP2413483A1/de not_active Withdrawn
-
2011
- 2011-07-22 WO PCT/EP2011/062633 patent/WO2012013594A2/de active Application Filing
- 2011-07-22 EP EP11740869.0A patent/EP2599195A2/de not_active Withdrawn
- 2011-07-22 US US13/813,069 patent/US20130126669A1/en not_active Abandoned
- 2011-07-22 RU RU2013108825/11A patent/RU2547938C2/ru not_active IP Right Cessation
- 2011-07-22 CN CN201180036313.7A patent/CN103026600B/zh not_active Expired - Fee Related
- 2011-07-22 BR BR112013002327A patent/BR112013002327A8/pt not_active IP Right Cessation
Also Published As
Publication number | Publication date |
---|---|
WO2012013594A3 (de) | 2012-04-26 |
BR112013002327A8 (pt) | 2016-10-18 |
US20130126669A1 (en) | 2013-05-23 |
RU2547938C2 (ru) | 2015-04-10 |
CN103026600A (zh) | 2013-04-03 |
RU2013108825A (ru) | 2014-09-10 |
EP2599195A2 (de) | 2013-06-05 |
CN103026600B (zh) | 2016-03-09 |
EP2413483A1 (de) | 2012-02-01 |
WO2012013594A2 (de) | 2012-02-02 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
BR112013002327A2 (pt) | dispositivo de acionamento elétrico para uma aeronave | |
BR112015029439A2 (pt) | sistema de retroajuste para converter um veículo em um dentre um veículo elétrico híbrido (hev) e um veículo elétrico (ev) | |
BR112012030189A2 (pt) | dispositivo de transmissão de potência para veículo elétrico | |
BR112013002382A2 (pt) | unidade de transmissão de propulsão e movimento, em particular para uma aeronave de asa giratória | |
DE502007006549D1 (de) | Fluggerät | |
WO2012139123A3 (en) | Starter machine system and method | |
WO2012150242A3 (de) | Axiallager für einen elektrischen antrieb | |
PE20151571A1 (es) | Turbinas de gas en aplicaciones de accionamiento mecanico y metodo de funcionamiento | |
BRPI1100580A8 (pt) | Veículo de inspeção para inspecionar uma folga de ar entre o rotor e o estator de um gerador | |
MX359421B (es) | Dispositivo de movimiento giratorio con desplazamiento positivo gradual. | |
EP2367270A3 (en) | Electric rotary actuator | |
BR112014031321A2 (pt) | trator de poço | |
BR102016027344B8 (pt) | Atuador para acionar um corpo de bomba, e, bomba | |
BR112014004258A2 (pt) | dispositivo de motorização multieixo e instrumento de comando equipado com um tal dispositivo | |
WO2013087056A3 (de) | Elektrische maschine, insbesondere für luftfahrzeuge | |
WO2014087134A3 (en) | Electric Machine | |
BR112012032056A2 (pt) | fornecimento de energia elétrica para aparelhos sustentados pelo rotor de um motor de aeronave. | |
BRPI0924900A8 (pt) | Conjunto de mancal e motor elétrico | |
WO2013021250A3 (en) | Drive device for electric vehicle | |
GB2531212A (en) | Supercharger for a combustion engine | |
BR112015023575A8 (pt) | unidade de geração de potência e método para controlar motor gerador". | |
BRPI1014884A2 (pt) | máquina elétrica com um rotor e um estator e um dispositivo para controle do entreferro entre rotor e estator | |
BR102013031894A8 (pt) | trem de transmissão elétrico de um dispositivo e equipamento de compressão de gás | |
BR112014031921A2 (pt) | método para controle simultâneo de torque de motor de combustão e máquina elétrica em um veículo híbrido | |
BR112014016886A2 (pt) | unidade de retirada de energia (pto) com alternador integral |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
B06F | Objections, documents and/or translations needed after an examination request according [chapter 6.6 patent gazette] | ||
B08F | Application dismissed because of non-payment of annual fees [chapter 8.6 patent gazette] |
Free format text: REFERENTE A 8A ANUIDADE. |
|
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 2524 DE 21-05-2019 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. |