AR123508A2 - Dispositivo de propulsión para una aeronave - Google Patents
Dispositivo de propulsión para una aeronaveInfo
- Publication number
- AR123508A2 AR123508A2 ARP210102547A ARP210102547A AR123508A2 AR 123508 A2 AR123508 A2 AR 123508A2 AR P210102547 A ARP210102547 A AR P210102547A AR P210102547 A ARP210102547 A AR P210102547A AR 123508 A2 AR123508 A2 AR 123508A2
- Authority
- AR
- Argentina
- Prior art keywords
- wing
- axis
- rotation
- bearing
- offset
- Prior art date
Links
- 230000008878 coupling Effects 0.000 abstract 4
- 238000010168 coupling process Methods 0.000 abstract 4
- 238000005859 coupling reaction Methods 0.000 abstract 4
- 230000005484 gravity Effects 0.000 abstract 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C39/00—Aircraft not otherwise provided for
- B64C39/003—Aircraft not otherwise provided for with wings, paddle wheels, bladed wheels, moving or rotating in relation to the fuselage
- B64C39/005—Aircraft not otherwise provided for with wings, paddle wheels, bladed wheels, moving or rotating in relation to the fuselage about a horizontal transversal axis
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C39/00—Aircraft not otherwise provided for
- B64C39/10—All-wing aircraft
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C11/00—Propellers, e.g. of ducted type; Features common to propellers and rotors for rotorcraft
- B64C11/006—Paddle wheels
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C39/00—Aircraft not otherwise provided for
- B64C39/10—All-wing aircraft
- B64C2039/105—All-wing aircraft of blended wing body type
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
- B64U10/25—Fixed-wing aircraft
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
- B64U10/80—UAVs characterised by their small size, e.g. micro air vehicles [MAV]
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U30/00—Means for producing lift; Empennages; Arrangements thereof
- B64U30/20—Rotors; Rotor supports
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Transmission Devices (AREA)
- Wind Motors (AREA)
- Toys (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Pivots And Pivotal Connections (AREA)
Abstract
La presente invención 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 esta 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 invención, 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.
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 |
|---|---|
| AR123508A2 true AR123508A2 (es) | 2022-12-07 |
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 Before (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| ARP180103647A AR113936A1 (es) | 2017-12-14 | 2018-12-13 | Unidad de propulsión para una aeronave |
Country Status (8)
| Country | Link |
|---|---|
| US (1) | US11479356B2 (es) |
| EP (2) | EP3715249B1 (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)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2020261149A1 (en) * | 2019-06-25 | 2020-12-30 | Universidade Da Beira Interior | 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)
| 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 |
-
2017
- 2017-12-14 DE DE102017011890.6A patent/DE102017011890B4/de active Active
-
2018
- 2018-12-11 US US16/771,868 patent/US11479356B2/en active Active
- 2018-12-11 JP JP2020531692A patent/JP7157157B2/ja active Active
- 2018-12-11 CN CN201880080368.XA patent/CN111479750B/zh active Active
- 2018-12-11 WO PCT/EP2018/084371 patent/WO2019115532A1/de unknown
- 2018-12-11 EP EP20168135.0A patent/EP3715249B1/de active Active
- 2018-12-11 BR BR112020011814-1A patent/BR112020011814B1/pt active IP Right Grant
- 2018-12-11 EP EP18825918.8A patent/EP3548378B1/de active Active
- 2018-12-13 AR ARP180103647A patent/AR113936A1/es active IP Right Grant
-
2021
- 2021-09-14 AR ARP210102547A patent/AR123508A2/es unknown
Also Published As
| Publication number | Publication date |
|---|---|
| DE102017011890B4 (de) | 2023-02-09 |
| CN111479750A (zh) | 2020-07-31 |
| US11479356B2 (en) | 2022-10-25 |
| WO2019115532A1 (de) | 2019-06-20 |
| BR112020011814A2 (pt) | 2020-11-17 |
| JP7157157B2 (ja) | 2022-10-19 |
| BR112020011814B1 (pt) | 2024-04-30 |
| EP3715249A1 (de) | 2020-09-30 |
| AR113936A1 (es) | 2020-07-01 |
| EP3715249B1 (de) | 2021-06-23 |
| DE102017011890A1 (de) | 2019-06-19 |
| CN111479750B (zh) | 2023-04-25 |
| JP2021506650A (ja) | 2021-02-22 |
| EP3548378B1 (de) | 2021-06-23 |
| US20210229803A1 (en) | 2021-07-29 |
| EP3548378A1 (de) | 2019-10-09 |
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