BR112018013496A2 - aeronave - Google Patents

aeronave

Info

Publication number
BR112018013496A2
BR112018013496A2 BR112018013496-1A BR112018013496A BR112018013496A2 BR 112018013496 A2 BR112018013496 A2 BR 112018013496A2 BR 112018013496 A BR112018013496 A BR 112018013496A BR 112018013496 A2 BR112018013496 A2 BR 112018013496A2
Authority
BR
Brazil
Prior art keywords
cyclogiro
rotors
aircraft fuselage
aircraft
torque compensation
Prior art date
Application number
BR112018013496-1A
Other languages
English (en)
Other versions
BR112018013496B1 (pt
Inventor
Schwaiger Meinhard
Original Assignee
Cyclotech 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 Cyclotech Gmbh filed Critical Cyclotech Gmbh
Publication of BR112018013496A2 publication Critical patent/BR112018013496A2/pt
Publication of BR112018013496B1 publication Critical patent/BR112018013496B1/pt

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C27/00Rotorcraft; Rotors peculiar thereto
    • B64C27/22Compound rotorcraft, i.e. aircraft using in flight the features of both aeroplane and rotorcraft
    • B64C27/26Compound rotorcraft, i.e. aircraft using in flight the features of both aeroplane and rotorcraft characterised by provision of fixed wings
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C39/00Aircraft not otherwise provided for
    • B64C39/003Aircraft not otherwise provided for with wings, paddle wheels, bladed wheels, moving or rotating in relation to the fuselage
    • B64C39/005Aircraft not otherwise provided for with wings, paddle wheels, bladed wheels, moving or rotating in relation to the fuselage about a horizontal transversal axis
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C11/00Propellers, e.g. of ducted type; Features common to propellers and rotors for rotorcraft
    • B64C11/006Paddle wheels
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C27/00Rotorcraft; Rotors peculiar thereto
    • B64C27/22Compound rotorcraft, i.e. aircraft using in flight the features of both aeroplane and rotorcraft
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C29/00Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C27/00Rotorcraft; Rotors peculiar thereto
    • B64C27/82Rotorcraft; Rotors peculiar thereto characterised by the provision of an auxiliary rotor or fluid-jet device for counter-balancing lifting rotor torque or changing direction of rotorcraft
    • B64C2027/8236Rotorcraft; Rotors peculiar thereto characterised by the provision of an auxiliary rotor or fluid-jet device for counter-balancing lifting rotor torque or changing direction of rotorcraft including pusher propellers
    • 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
    • F03D7/00Controlling wind motors 
    • F03D7/06Controlling wind motors  the wind motors having rotation axis substantially perpendicular to the air flow entering the rotor

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Toys (AREA)
  • Transmission Devices (AREA)
  • Tires In General (AREA)

Abstract

a invenção refere-se a uma aeronave projetada como um helicóptero composto com uma fuselagem da aeronave (1), um rotor principal (2) disposto na fuselagem da aeronave (1) e rotores ciclogiro (3, 3') que se projetam lateralmente a partir da fuselagem da aeronave (1) e que incluem uma superfície de extremidade externa. uma compensação de torque melhorada é alcançada em que os rotores ciclogiro (3, 3') são conectados à fuselagem da aeronave (1) por meio de um dispositivo de suspensão (4, 4') que segura os rotores ciclogiro (3, 3') na borda externa dos rotores, e cada rotor ciclogiro (3, 3') pode ser controlado individualmente e independentemente do outro. uma função de compensação de torque do rotor principal (2) pode ser executada pelos rotores ciclogiro (3, 3').
BR112018013496-1A 2015-12-30 2016-12-30 Aeronave BR112018013496B1 (pt)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
ATA51113/2015 2015-12-30
ATA51113/2015A AT518116B1 (de) 2015-12-30 2015-12-30 Fluggerät
PCT/AT2016/060137 WO2017112973A1 (de) 2015-12-30 2016-12-30 Fluggerät

Publications (2)

Publication Number Publication Date
BR112018013496A2 true BR112018013496A2 (pt) 2018-12-04
BR112018013496B1 BR112018013496B1 (pt) 2022-02-08

Family

ID=57850811

Family Applications (1)

Application Number Title Priority Date Filing Date
BR112018013496-1A BR112018013496B1 (pt) 2015-12-30 2016-12-30 Aeronave

Country Status (9)

Country Link
US (1) US10822079B2 (pt)
EP (1) EP3397551B1 (pt)
JP (1) JP6618626B2 (pt)
CN (1) CN108473191B (pt)
AT (1) AT518116B1 (pt)
BR (1) BR112018013496B1 (pt)
ES (1) ES2750781T3 (pt)
RU (1) RU2682954C1 (pt)
WO (1) WO2017112973A1 (pt)

Families Citing this family (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2018140199A2 (en) * 2017-01-03 2018-08-02 The Texas A&M University System Cycloidal rotor micro-air vehicle
US10384776B2 (en) * 2017-02-22 2019-08-20 Bell Helicopter Textron Inc. Tiltrotor aircraft having vertical lift and hover augmentation
US10994840B1 (en) 2017-08-16 2021-05-04 United States Of America As Represented By The Secretary Of The Air Force Thrust vectoring control of a cyclorotor
DE102017011890B4 (de) * 2017-12-14 2023-02-09 Cyclotech Gmbh Antriebsvorrichtung für ein Fluggerät
WO2019139559A1 (ru) * 2018-01-15 2019-07-18 Александр Анатолиевич БАЛИЦКИЙ Циклоидальный ротор с эллиптической траекторией движения лопастей и способ управления воздушным судном с помощью циклоидального ротора
CN210027878U (zh) * 2018-11-06 2020-02-07 珠海隆华直升机科技有限公司 直升机垂平尾结构及直升机
RU2746025C2 (ru) * 2018-11-19 2021-04-06 Александр Александрович Горшков Безаэродромный летательный аппарат
DE102020109331B3 (de) * 2020-04-03 2021-07-08 Dr. Ing. H.C. F. Porsche Aktiengesellschaft Luftfahrzeug
DE102021003751B3 (de) 2021-07-20 2022-11-24 Friedrich B. Grimm Fahrzeug mit einer drehflügelkinematik
DE102021004136B4 (de) 2021-08-09 2023-03-09 Friedrich B. Grimm Vorrichtung für ein Drehflügelfahrzeug oder für eine Drehflügelturbine
DE102021005965B3 (de) 2021-12-01 2022-11-10 Friedrich Grimm Rotorblatt für eine wind - oder wasserturbine sowie für ein drehflügelfahrzeug und insbesondere für einen hubschrauber
DE102022114599B4 (de) 2022-06-09 2024-02-08 Louis Gagnon Fluggerät

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FR2736889B1 (fr) 1995-07-21 1997-09-12 Eurocopter France Aeronef a voilure tournante du type combine et element structurel arriere pour un tel aeronef
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US10384776B2 (en) * 2017-02-22 2019-08-20 Bell Helicopter Textron Inc. Tiltrotor aircraft having vertical lift and hover augmentation

Also Published As

Publication number Publication date
US20190023393A1 (en) 2019-01-24
JP6618626B2 (ja) 2019-12-11
WO2017112973A1 (de) 2017-07-06
CN108473191B (zh) 2021-12-07
CN108473191A (zh) 2018-08-31
RU2682954C1 (ru) 2019-03-22
AT518116A1 (de) 2017-07-15
AT518116B1 (de) 2019-05-15
JP2019500269A (ja) 2019-01-10
EP3397551A1 (de) 2018-11-07
US10822079B2 (en) 2020-11-03
BR112018013496B1 (pt) 2022-02-08
EP3397551B1 (de) 2019-07-10
ES2750781T3 (es) 2020-03-27

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Legal Events

Date Code Title Description
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]
B16A Patent or certificate of addition of invention granted [chapter 16.1 patent gazette]

Free format text: PRAZO DE VALIDADE: 20 (VINTE) ANOS CONTADOS A PARTIR DE 30/12/2016, OBSERVADAS AS CONDICOES LEGAIS.