ES2604711A1 - Aeronave - Google Patents

Aeronave Download PDF

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Publication number
ES2604711A1
ES2604711A1 ES201730123A ES201730123A ES2604711A1 ES 2604711 A1 ES2604711 A1 ES 2604711A1 ES 201730123 A ES201730123 A ES 201730123A ES 201730123 A ES201730123 A ES 201730123A ES 2604711 A1 ES2604711 A1 ES 2604711A1
Authority
ES
Spain
Prior art keywords
aircraft
translation
machine
legally binding
google translate
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.)
Granted
Application number
ES201730123A
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English (en)
Other versions
ES2604711B1 (es
Inventor
Alberto ADARVE LOZANO
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.)
Defensya Ingenieria Internacional SL
Original Assignee
Defensya Ingenieria Internacional 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 Defensya Ingenieria Internacional SL filed Critical Defensya Ingenieria Internacional SL
Priority to ES201730123A priority Critical patent/ES2604711B1/es
Publication of ES2604711A1 publication Critical patent/ES2604711A1/es
Application granted granted Critical
Publication of ES2604711B1 publication Critical patent/ES2604711B1/es
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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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
    • B64C27/26—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
    • B64C27/22—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
    • 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
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C3/00—Wings
    • B64C3/38—Adjustment of complete wings or parts thereof
    • B64C3/54—Varying in area
    • B64C3/546—Varying in area by foldable elements

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Transmission Devices (AREA)
  • Catching Or Destruction (AREA)

Abstract

Aeronave que comprende un cuerpo (1) de la aeronave, una hélice superior (2) montada encima del cuerpo (1) de la aeronave y tres rotores; un rotor de cola o principal (5) y dos rotores laterales (4) montados en los extremos de unos soportes (6) donde los rotores laterales (4) y el rotor de cola (5) giran respecto de un eje horizontal, hasta incluso llegar a ponerse en posición vertical. Las alas (3) pueden ser retráctiles o plegables, que se plegarán o recogerán según las condiciones de vuelo o similares, la hélice superior (2) puede contar con un sistema de inclinación de la misma con objeto de evitar un giro excesivo y la propulsión de la aeronave puede ser mediante un motor de combustión o mediante un motor híbrido provisto de un embrague. Siendo los motores eléctricos alimentados por baterías o similares recargables por el giro de las hélices o por otros medios.

Description

imagen1
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lograr el par de arranque de la hélice superior. Los rotores pueden ser accionados bien mediante motores de combustión o eléctricos. Los motores eléctricos son energizados desde unas baterías, recargables por el giro de las hélices u otros medios como puede ser un cargador en tierra.
5
Una aeronave como la descrita puede contar con un sistema de navegación GPS, un sistema de control centralizado, un sistema de reducción de ruido, servocontrol de dirección en tierra, posibilidad de 3 y hasta seis pasajeros, mecanismo de aterrizaje retráctil, puede llegar a tener una máxima carga de
10 600 Kg, alcanzar una velocidad por encima de 250 Km/h y una autonomía de al menos 500 km.
Descrita suficientemente la naturaleza de la presente invención, así como la manera de ponerla en práctica, se hace constar que, dentro de su esencialidad,
15 podrá ser llevada a la práctica en otras formas de realización que difieran en detalle de la indicada a título de ejemplo, y a las cuales alcanzará igualmente la protección que se recaba, siempre que no altere, cambie o modifique su principio fundamental.
8

Claims (1)

  1. imagen1
ES201730123A 2017-02-02 2017-02-02 Aeronave Expired - Fee Related ES2604711B1 (es)

Priority Applications (1)

Application Number Priority Date Filing Date Title
ES201730123A ES2604711B1 (es) 2017-02-02 2017-02-02 Aeronave

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
ES201730123A ES2604711B1 (es) 2017-02-02 2017-02-02 Aeronave

Publications (2)

Publication Number Publication Date
ES2604711A1 true ES2604711A1 (es) 2017-03-08
ES2604711B1 ES2604711B1 (es) 2017-12-18

Family

ID=58191740

Family Applications (1)

Application Number Title Priority Date Filing Date
ES201730123A Expired - Fee Related ES2604711B1 (es) 2017-02-02 2017-02-02 Aeronave

Country Status (1)

Country Link
ES (1) ES2604711B1 (es)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN108516083A (zh) * 2018-03-27 2018-09-11 西北工业大学 双离合式可停转旋翼飞行器驱动系统及改变工作模式方法
EP3656668A3 (en) * 2018-11-26 2020-07-29 Bell Textron Inc. Tilting duct compound helicopter

Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3241791A (en) * 1964-04-03 1966-03-22 Frank N Piasecki Compound helicopter with shrouded tail propeller
US20050045762A1 (en) * 2003-01-09 2005-03-03 Pham Roger N. High performance VTOL convertiplanes
US20050133662A1 (en) * 2003-12-23 2005-06-23 Eric Magre Convertible aircraft provided with two tilt fans on either side of the fuselage and with a third tilt fan arranged on the tail of the aircraft
WO2007014531A1 (fr) * 2005-08-02 2007-02-08 Peizhou Han Aeronef a decollage et atterrissage verticaux a rotors avant basculants
US20080184906A1 (en) * 2007-02-07 2008-08-07 Kejha Joseph B Long range hybrid electric airplane
WO2013105094A1 (en) * 2012-01-12 2013-07-18 Israel Aerospace Industries Ltd. System, method and computer program product for maneuvering of an air vehicle with tiltable propulsion unit
EP2690012A1 (en) * 2012-07-27 2014-01-29 Eurocopter Deutschland GmbH Semi-convertible rotorcraft
WO2014206058A1 (zh) * 2013-06-28 2014-12-31 Li Hongsheng 主螺旋桨前倾式直升机

Patent Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3241791A (en) * 1964-04-03 1966-03-22 Frank N Piasecki Compound helicopter with shrouded tail propeller
US20050045762A1 (en) * 2003-01-09 2005-03-03 Pham Roger N. High performance VTOL convertiplanes
US20050133662A1 (en) * 2003-12-23 2005-06-23 Eric Magre Convertible aircraft provided with two tilt fans on either side of the fuselage and with a third tilt fan arranged on the tail of the aircraft
WO2007014531A1 (fr) * 2005-08-02 2007-02-08 Peizhou Han Aeronef a decollage et atterrissage verticaux a rotors avant basculants
US20080184906A1 (en) * 2007-02-07 2008-08-07 Kejha Joseph B Long range hybrid electric airplane
WO2013105094A1 (en) * 2012-01-12 2013-07-18 Israel Aerospace Industries Ltd. System, method and computer program product for maneuvering of an air vehicle with tiltable propulsion unit
EP2690012A1 (en) * 2012-07-27 2014-01-29 Eurocopter Deutschland GmbH Semi-convertible rotorcraft
WO2014206058A1 (zh) * 2013-06-28 2014-12-31 Li Hongsheng 主螺旋桨前倾式直升机

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN108516083A (zh) * 2018-03-27 2018-09-11 西北工业大学 双离合式可停转旋翼飞行器驱动系统及改变工作模式方法
CN108516083B (zh) * 2018-03-27 2021-05-14 西北工业大学 双离合式可停转旋翼飞行器驱动系统及改变工作模式方法
EP3656668A3 (en) * 2018-11-26 2020-07-29 Bell Textron Inc. Tilting duct compound helicopter
US11148799B2 (en) 2018-11-26 2021-10-19 Textron Innovations Inc. Tilting duct compound helicopter

Also Published As

Publication number Publication date
ES2604711B1 (es) 2017-12-18

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