AR113936A1 - Unidad de propulsión para una aeronave - Google Patents

Unidad de propulsión para una aeronave

Info

Publication number
AR113936A1
AR113936A1 ARP180103647A ARP180103647A AR113936A1 AR 113936 A1 AR113936 A1 AR 113936A1 AR P180103647 A ARP180103647 A AR P180103647A AR P180103647 A ARP180103647 A AR P180103647A AR 113936 A1 AR113936 A1 AR 113936A1
Authority
AR
Argentina
Prior art keywords
wing
axis
bearing
rotation
propulsion unit
Prior art date
Application number
ARP180103647A
Other languages
English (en)
Inventor
Stephan Lanser
Michael Winderl
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 AR113936A1 publication Critical patent/AR113936A1/es

Links

Classifications

    • 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
    • B64C39/00Aircraft not otherwise provided for
    • B64C39/10All-wing aircraft
    • 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
    • B64C39/00Aircraft not otherwise provided for
    • B64C39/10All-wing aircraft
    • B64C2039/105All-wing aircraft of blended wing body type
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64UUNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U10/00Type of UAV
    • B64U10/25Fixed-wing aircraft
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64UUNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U10/00Type of UAV
    • B64U10/80UAVs characterised by their small size, e.g. micro air vehicles [MAV]
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64UUNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U30/00Means for producing lift; Empennages; Arrangements thereof
    • B64U30/20Rotors; Rotor supports

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Transmission Devices (AREA)
  • Wind Motors (AREA)
  • Pivots And Pivotal Connections (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Toys (AREA)

Abstract

La presente se refiere a una unidad de propulsión para una aeronave que comprende un ala (2) giratoria a lo largo de una órbita (52) alrededor de un eje de rotación (51) de la unidad de propulsión, y que está montada de forma pivotable alrededor de un eje de cojinete de ala de forma paralela al eje de rotación; un mecanismo de inclinación (3) con un dispositivo de acoplamiento (31) y un dispositivo de cojinete (33); y un dispositivo de compensación (4), en el que el ala se acopla, en donde el dispositivo de compensación define un eje de cojinete excéntrico (41) que se monta a una distancia de compensación ajustable (43). El dispositivo de acoplamiento está acoplado al ala en un punto de acoplamiento (32), que está posicionado de tal manera que el plano que comprende el eje de cojinete del ala y el punto de acoplamiento, y el plano tangencial en la órbita a través del eje de cojinete del ala incluyen un ángulo determinado, que no desaparece (wₐ) cuando la distancia de compensación se establece en cero. Según un segundo aspecto de la presente, el eje de cojinete del ala con respecto al plano que pasa a través del centro de gravedad del ala y de forma paralela tanto al eje de rotación como también al ancho de la cuerda del perfil del ala, se desplaza hacia el eje de rotación a una cierta distancia.
ARP180103647A 2017-12-14 2018-12-13 Unidad de propulsión para una aeronave AR113936A1 (es)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE102017011890.6A DE102017011890B4 (de) 2017-12-14 2017-12-14 Antriebsvorrichtung für ein Fluggerät

Publications (1)

Publication Number Publication Date
AR113936A1 true AR113936A1 (es) 2020-07-01

Family

ID=64870428

Family Applications (2)

Application Number Title Priority Date Filing Date
ARP180103647A AR113936A1 (es) 2017-12-14 2018-12-13 Unidad de propulsión para una aeronave
ARP210102547A AR123508A2 (es) 2017-12-14 2021-09-14 Dispositivo de propulsión para una aeronave

Family Applications After (1)

Application Number Title Priority Date Filing Date
ARP210102547A AR123508A2 (es) 2017-12-14 2021-09-14 Dispositivo de propulsión para una aeronave

Country Status (8)

Country Link
US (1) US11479356B2 (es)
EP (2) EP3548378B1 (es)
JP (1) JP7157157B2 (es)
CN (1) CN111479750B (es)
AR (2) AR113936A1 (es)
BR (1) BR112020011814B1 (es)
DE (1) DE102017011890B4 (es)
WO (1) WO2019115532A1 (es)

Families Citing this family (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CA3134326A1 (en) * 2019-06-25 2020-12-30 Mehdi HABIBNIA RAMI Flight propulsion system based on rotary and stationary devices
EP4091939A1 (de) 2021-05-21 2022-11-23 CycloTech GmbH Fluggerät
US20220380059A1 (en) * 2021-05-31 2022-12-01 George Pul Piston Wings
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

Family Cites Families (19)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR640890A (fr) 1927-02-25 1928-07-24 Moteur sustentateur et propulseur dans un fiuide
US2413460A (en) * 1944-05-16 1946-12-31 David W Main Airplane
US2950765A (en) * 1956-12-27 1960-08-30 Pacific Car & Foundry Co Balanced lift vertical axis propellers
US4194707A (en) 1977-12-16 1980-03-25 Sharpe Thomas H Lift augmenting device for aircraft
US4196707A (en) 1978-07-31 1980-04-08 General Motors Corporation Exhaust gas recirculation control
US5265827A (en) * 1991-06-17 1993-11-30 Northrop Corporation Paddle wheel rotorcraft
DE19637833C1 (de) 1996-09-17 1998-02-05 Voith Hydro Gmbh Schiffstechni Zykloidalpropeller
US7219854B2 (en) 2005-03-04 2007-05-22 Information Systems Laboratories, Inc. Cycloidal hybrid advanced surface effects vehicle
US20070200029A1 (en) * 2006-02-27 2007-08-30 Sullivan Callum R Hydraulic cycloidal control system
US20080011900A1 (en) * 2006-07-15 2008-01-17 Javier Quintana Apparatus and method to control the flight dynamics in a lighter-than-air airship
DE102007009951B3 (de) * 2007-03-01 2008-07-31 Bauhaus Luftfahrt E.V. Fluggerät mit rotierenden Zylindern zur Erzeugung von Auftrieb und/oder Vortrieb
JP2009051381A (ja) 2007-08-28 2009-03-12 Mitsubishi Heavy Ind Ltd サイクロイダル・ブレード
US20100322769A1 (en) * 2008-02-25 2010-12-23 Thomas Glenn Stephens Fluid turbine optimized for power generation
JP5995200B2 (ja) 2012-03-09 2016-09-21 国立研究開発法人宇宙航空研究開発機構 可変ピッチプロペラ
US9346535B1 (en) * 2012-04-05 2016-05-24 The United States Of America As Represented By The Secretary Of The Air Force Ring cam and ring cam assembly for dynamically controlling pitch of cycloidal rotor blades
AT518116B1 (de) * 2015-12-30 2019-05-15 Cyclotech Gmbh Fluggerät
US10279900B2 (en) 2016-08-10 2019-05-07 Bell Helicopter Textron Inc. Rotorcraft variable thrust cross-flow fan systems
US10384776B2 (en) * 2017-02-22 2019-08-20 Bell Helicopter Textron Inc. Tiltrotor aircraft having vertical lift and hover augmentation
US10814967B2 (en) * 2017-08-28 2020-10-27 Textron Innovations Inc. Cargo transportation system having perimeter propulsion

Also Published As

Publication number Publication date
DE102017011890A1 (de) 2019-06-19
CN111479750A (zh) 2020-07-31
EP3548378A1 (de) 2019-10-09
EP3715249B1 (de) 2021-06-23
US11479356B2 (en) 2022-10-25
BR112020011814A2 (pt) 2020-11-17
JP2021506650A (ja) 2021-02-22
DE102017011890B4 (de) 2023-02-09
CN111479750B (zh) 2023-04-25
AR123508A2 (es) 2022-12-07
JP7157157B2 (ja) 2022-10-19
BR112020011814B1 (pt) 2024-04-30
WO2019115532A1 (de) 2019-06-20
US20210229803A1 (en) 2021-07-29
EP3715249A1 (de) 2020-09-30
EP3548378B1 (de) 2021-06-23

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