ES2611316B1 - Aerodino con capacidad de despegue y aterrizaje vertical - Google Patents

Aerodino con capacidad de despegue y aterrizaje vertical Download PDF

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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
Application number
ES201531579A
Other languages
English (en)
Other versions
ES2611316A1 (es
Inventor
Jesús Carlos Castellano Aldave
Jesús VILLADANGOS ALONSO
José Javier ASTRAIN ESCOLA
Carlos MATILLA CODESAL
Mael TALEB
Tania JORAJURÍA GOMEZ
Ernö PETER COSMA
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Universidad Publica de Navarra
Original Assignee
Fuvex Sist Sl
Fuvex Sistemas Sl
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 Fuvex Sist Sl, Fuvex Sistemas Sl filed Critical Fuvex Sist Sl
Priority to ES201531579A priority Critical patent/ES2611316B1/es
Priority to US15/773,785 priority patent/US11053000B2/en
Priority to PCT/ES2016/000112 priority patent/WO2017077144A1/es
Publication of ES2611316A1 publication Critical patent/ES2611316A1/es
Application granted granted Critical
Publication of ES2611316B1 publication Critical patent/ES2611316B1/es
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • 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
    • 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
    • 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
    • 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

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Claims (1)

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ES201531579A 2015-11-04 2015-11-04 Aerodino con capacidad de despegue y aterrizaje vertical Active ES2611316B1 (es)

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)

* Cited by examiner, † Cited by third party
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)

* Cited by examiner, † Cited by third party
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

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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