BR112013002327A8 - dispositivo de acionamento elétrico para uma aeronave - Google Patents

dispositivo de acionamento elétrico para uma aeronave

Info

Publication number
BR112013002327A8
BR112013002327A8 BR112013002327A BR112013002327A BR112013002327A8 BR 112013002327 A8 BR112013002327 A8 BR 112013002327A8 BR 112013002327 A BR112013002327 A BR 112013002327A BR 112013002327 A BR112013002327 A BR 112013002327A BR 112013002327 A8 BR112013002327 A8 BR 112013002327A8
Authority
BR
Brazil
Prior art keywords
dynamoelectric machine
aircraft
rotor
electric drive
drive device
Prior art date
Application number
BR112013002327A
Other languages
English (en)
Other versions
BR112013002327A2 (pt
Inventor
Jens Hamann
Markus Klöpzig
Olaf Körner
Original Assignee
Siemens Ag
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 Siemens Ag filed Critical Siemens Ag
Publication of BR112013002327A2 publication Critical patent/BR112013002327A2/pt
Publication of BR112013002327A8 publication Critical patent/BR112013002327A8/pt

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D35/00—Transmitting power from power plant to propellers or rotors; Arrangements of transmissions
    • B64D35/02—Transmitting power from power plant to propellers or rotors; Arrangements of transmissions characterised by the type of power plant
    • 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; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D27/00—Arrangement or mounting of power plant in aircraft; Aircraft characterised thereby
    • B64D27/02—Aircraft characterised by the type or position of power plant
    • B64D27/24—Aircraft characterised by the type or position of power plant using steam, electricity, or spring force
    • 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

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).
BR112013002327A 2010-07-30 2011-07-22 dispositivo de acionamento elétrico para uma aeronave BR112013002327A8 (pt)

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 BR112013002327A2 (pt) 2016-05-24
BR112013002327A8 true 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)

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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
US9957040B2 (en) 2013-08-28 2018-05-01 Sikorsky Aircraft Corporation Propeller gearbox oil cooler for a rotary wing aircract
DE102013219724A1 (de) * 2013-09-30 2015-04-02 Siemens Aktiengesellschaft Elektrisch angetriebenes Flugzeug
JP6393916B2 (ja) * 2014-02-20 2018-09-26 北田回転機関合同会社 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
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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
CN109792198A (zh) * 2016-09-23 2019-05-21 卓胜镐 不间断电动机
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
GB201708289D0 (en) 2017-05-24 2017-07-05 Rolls Royce Plc Preventing electrical breakdown
GB201708297D0 (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
DE102022118426A1 (de) 2022-07-22 2024-01-25 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

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Also Published As

Publication number Publication date
EP2599195A2 (de) 2013-06-05
WO2012013594A3 (de) 2012-04-26
EP2413483A1 (de) 2012-02-01
BR112013002327A2 (pt) 2016-05-24
CN103026600B (zh) 2016-03-09
RU2547938C2 (ru) 2015-04-10
WO2012013594A2 (de) 2012-02-02
US20130126669A1 (en) 2013-05-23
CN103026600A (zh) 2013-04-03
RU2013108825A (ru) 2014-09-10

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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.