ES2611316B1 - Aerodino con capacidad de despegue y aterrizaje vertical - Google Patents
Aerodino con capacidad de despegue y aterrizaje vertical Download PDFInfo
- Publication number
- ES2611316B1 ES2611316B1 ES201531579A ES201531579A ES2611316B1 ES 2611316 B1 ES2611316 B1 ES 2611316B1 ES 201531579 A ES201531579 A ES 201531579A ES 201531579 A ES201531579 A ES 201531579A ES 2611316 B1 ES2611316 B1 ES 2611316B1
- Authority
- ES
- Spain
- Prior art keywords
- take
- lift
- rotors
- aerodyne
- wing
- Prior art date
- Legal status (The legal status 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 status listed.)
- Active
Links
Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/22—Compound rotorcraft, i.e. aircraft using in flight the features of both aeroplane and rotorcraft
- B64C27/28—Compound rotorcraft, i.e. aircraft using in flight the features of both aeroplane and rotorcraft with forward-propulsion propellers pivotable to act as lifting rotors
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/22—Compound rotorcraft, i.e. aircraft using in flight the features of both aeroplane and rotorcraft
- B64C27/26—Compound rotorcraft, i.e. aircraft using in flight the features of both aeroplane and rotorcraft characterised by provision of fixed wings
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/32—Rotors
- B64C27/37—Rotors having articulated joints
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C29/00—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft
- B64C29/0008—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded
- B64C29/0016—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded the lift during taking-off being created by free or ducted propellers or by blowers
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C29/00—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft
- B64C29/0008—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded
- B64C29/0016—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded the lift during taking-off being created by free or ducted propellers or by blowers
- B64C29/0033—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded the lift during taking-off being created by free or ducted propellers or by blowers the propellers being tiltable relative to the fuselage
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Toys (AREA)
- Jib Cranes (AREA)
Abstract
Aerodino con capacidad de despegue y aterrizaje vertical.#El aerodino propuesto con capacidad de despegue y aterrizaje vertical y con capacidad de generar sustentación tanto mediante rotores como mediante alas fijas incluye: un fuselaje (1); dos alas (2) fijas; dos rotores delanteros (11) y dos traseros (12) dispuestos simétricamente y accionados mediante motores (13); estando cada rotor (10) unido a una porción central de un ala (2) fija mediante un soporte (14); y articulado alrededor de un eje de articulación (E2), permitiendo modificar la inclinación de cada rotor (10) desde una posición de avance longitudinal, en la que impulsan el aerodino horizontalmente, hasta una posición de sustentación en la que proporciona sustentación vertical; quedando dichos rotores traseros en posición de sustentación parcialmente superpuestos con una porción del ala que incluye una aleta (20) libremente articulada al resto del ala determinándose su posición por efecto del empuje aerodinámico entre una posición de sustentación y una posición de avance longitudinal.
Description
Claims (1)
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imagen1 imagen2 imagen3 imagen4
Priority Applications (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
ES201531579A ES2611316B1 (es) | 2015-11-04 | 2015-11-04 | Aerodino con capacidad de despegue y aterrizaje vertical |
US15/773,785 US11053000B2 (en) | 2015-11-04 | 2016-10-14 | Aerodyne with vertical-takeoff-and-landing ability |
PCT/ES2016/000112 WO2017077144A1 (es) | 2015-11-04 | 2016-10-14 | Aerodino con capacidad de despegue y aterrizaje vertical |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
ES201531579A ES2611316B1 (es) | 2015-11-04 | 2015-11-04 | Aerodino con capacidad de despegue y aterrizaje vertical |
Publications (2)
Publication Number | Publication Date |
---|---|
ES2611316A1 ES2611316A1 (es) | 2017-05-08 |
ES2611316B1 true ES2611316B1 (es) | 2018-01-22 |
Family
ID=58643397
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
ES201531579A Active ES2611316B1 (es) | 2015-11-04 | 2015-11-04 | Aerodino con capacidad de despegue y aterrizaje vertical |
Country Status (3)
Country | Link |
---|---|
US (1) | US11053000B2 (es) |
ES (1) | ES2611316B1 (es) |
WO (1) | WO2017077144A1 (es) |
Families Citing this family (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR3050385B1 (fr) * | 2016-04-26 | 2018-04-06 | Airbus Helicopters | Drone comportant au moins trois rotors de sustentation et de propulsion |
DE102017112452A1 (de) * | 2017-06-06 | 2018-12-06 | Jonathan Hesselbarth | Steuerungsverfahren zur Steuerung eines Gier- und eines Rollwinkels eines senkrecht startenden Flugzeugs |
CN109305356A (zh) * | 2017-08-29 | 2019-02-05 | 陕西安康领航智能股份有限公司 | 一种倾转式垂直起降无人机 |
DE102017122359A1 (de) * | 2017-09-26 | 2019-03-28 | Paul Schreiber | Luftfahrzeug in Drachenkonfiguration |
DE102019102189B4 (de) | 2018-01-29 | 2022-11-03 | xFlight GmbH | Fluggerät |
WO2019204688A1 (en) * | 2018-04-19 | 2019-10-24 | Hi-Lite Aircraft | Vertical take off and landing fixed wing aircraft |
ES2880758T3 (es) * | 2018-08-03 | 2021-11-25 | Fuvex Civil Sl | Vehículo aéreo no tripulado con diferentes modos de vuelo |
US11279478B2 (en) * | 2019-06-18 | 2022-03-22 | Textron Innovations Inc. | Tilting closed-wing aircraft |
JP2022552431A (ja) * | 2019-08-16 | 2022-12-15 | テクストロン システムズ コーポレーション | 多関節ローターを持つ分離型揚力推力vtol航空機 |
DE102020105899A1 (de) * | 2020-03-05 | 2021-09-09 | Innotec Lightweight Engineering & Polymer Technology Gmbh | Fluggerät mit mehreren Flugmodi und Verfahren zu dessen Betreiben |
RU2746770C1 (ru) * | 2020-07-29 | 2021-04-20 | Александр Игоревич Никитин | Летательный аппарат вертикального взлета и посадки и способ управления его полетом |
CN112061387A (zh) * | 2020-09-10 | 2020-12-11 | 西安爱生技术集团公司 | 一种基于无人机机翼的旋翼安装结构 |
Family Cites Families (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3231221A (en) | 1964-03-10 | 1966-01-25 | Haviland H Platt | Vertical take-off airplanes |
US3934843A (en) * | 1974-08-05 | 1976-01-27 | Black John O | Free wing for convertible aircraft structure |
DE3929886A1 (de) * | 1989-09-08 | 1991-03-28 | Dornier Conrado | Flugzeug mit um eine querachse kippbaren triebwerksgondeln |
US6655631B2 (en) * | 2000-07-28 | 2003-12-02 | John Frederick Austen-Brown | Personal hoverplane with four tiltmotors |
US7054855B2 (en) | 2001-07-03 | 2006-05-30 | International Business Machines Corporation | Method and system for performing a pattern match search for text strings |
WO2010026517A2 (en) * | 2008-09-02 | 2010-03-11 | Urban Aeronautics Ltd. | Vtol vehicle with coaxially tilted or tiltable rotors |
US9187174B2 (en) * | 2010-10-06 | 2015-11-17 | Donald Orval Shaw | Aircraft with wings and movable propellers |
CN102363445B (zh) * | 2011-06-21 | 2014-07-30 | 杨朝习 | 倾转动力式垂直起降陆空两用飞行器 |
US20150013689A1 (en) | 2011-12-19 | 2015-01-15 | Howard L. Shackelford | Anatomical orientation system |
DE102012104783B4 (de) * | 2012-06-01 | 2019-12-24 | Quantum-Systems Gmbh | Fluggerät, bevorzugt UAV, Drohne und/oder UAS |
DE202012013513U1 (de) * | 2012-07-27 | 2017-05-12 | Jonathan Hesselbarth | Senkrecht startendes Flugzeug |
-
2015
- 2015-11-04 ES ES201531579A patent/ES2611316B1/es active Active
-
2016
- 2016-10-14 US US15/773,785 patent/US11053000B2/en active Active
- 2016-10-14 WO PCT/ES2016/000112 patent/WO2017077144A1/es active Application Filing
Also Published As
Publication number | Publication date |
---|---|
WO2017077144A1 (es) | 2017-05-11 |
US11053000B2 (en) | 2021-07-06 |
ES2611316A1 (es) | 2017-05-08 |
US20190152593A1 (en) | 2019-05-23 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
FG2A | Definitive protection |
Ref document number: 2611316 Country of ref document: ES Kind code of ref document: B1 Effective date: 20180122 |
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PC2A | Transfer of patent |
Effective date: 20180521 Owner name: UNIVERSIDAD PUBLICA DE NAVARRA Effective date: 20180521 |