ES2113676T3 - Aeronave hibrida. - Google Patents

Aeronave hibrida.

Info

Publication number
ES2113676T3
ES2113676T3 ES94927134T ES94927134T ES2113676T3 ES 2113676 T3 ES2113676 T3 ES 2113676T3 ES 94927134 T ES94927134 T ES 94927134T ES 94927134 T ES94927134 T ES 94927134T ES 2113676 T3 ES2113676 T3 ES 2113676T3
Authority
ES
Spain
Prior art keywords
air
tunnel
helicopter
vehicle
landing
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.)
Expired - Lifetime
Application number
ES94927134T
Other languages
English (en)
Inventor
Viktor Mikhailovich Kapin
Valeriy Andreevich Ivchin
Nikolai Serathimovich Pavlenko
Evgeny Lvovich Pogrebinsky
Viktor Vladimirovich Subbotin
Oleg Nikolaevich Majorov
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.)
TOVARISCHESTVO S OGRANICHENNOI
Original Assignee
TOVARISCHESTVO S OGRANICHENNOI
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 TOVARISCHESTVO S OGRANICHENNOI filed Critical TOVARISCHESTVO S OGRANICHENNOI
Application granted granted Critical
Publication of ES2113676T3 publication Critical patent/ES2113676T3/es
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • 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
    • B64C29/0025—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 fixed relative to the fuselage
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B60—VEHICLES IN GENERAL
    • B60V—AIR-CUSHION VEHICLES
    • B60V3/00—Land vehicles, waterborne vessels, or aircraft, adapted or modified to travel on air cushions
    • B60V3/08—Aircraft, e.g. air-cushion alighting-gear therefor
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Transportation (AREA)
  • Toys (AREA)
  • Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Nitrogen And Oxygen Or Sulfur-Condensed Heterocyclic Ring Systems (AREA)

Abstract

EL VEHICULO AEREO DE COMBINACION POSEE UN FUSELAJE (1) EN FORMA DE UN ALA SUSTENTADORA ESPESADA EN EL CENTRO CON UN TUNEL (2) ABIERTO VERTICALMENTE, EN EL QUE SE RECIBE UN HELICOPTERO (4). EL VEHICULO AEREO SE ENCUENTRA A DISPOSICION TAMBIEN POR MEDIO DE ALAS SUSTENTADORAS LATERALES Y UNA DISPOSICION (8) DE TIMONES. EL VEHICULO AEREO ESTA EQUIPADO CON UN DISPOSITIVO (19) DE ATERRIZAJE DE COLCHON DE AIRE, QUE ABARCA SU APARICION A PARTIR DEL TUNEL. LA INSTALACION DEL MECANISMO DE IMPULSION DEL VEHICULO AEREO INCLUYE DOS BLOQUES (13) DE MOTORES, QUE ESTAN DISPUESTOS SOBRE DOS LADOS CON REFERENCIA AL TUNEL (2), UNIDOS CON EL HELICOPTERO (4) Y CON LOS PROPULSORES (12) AEREOS DE MARCHA. LA SUPERFICIE DE SECCION TRANSVERSAL DEL TUNEL EN EL PLANO DE ROTACION DEL HELICOPTERO CORRESPONDE A UNA RELACION DESDE 0,3 HASTA 0,8 CON RESPECTO AL CONTENIDO SUPERFICIAL DEL COLCHON DE AIRE DEL DISPOSITIVO DE ATERRIZAJE, QUE GARANTIZA UN ATERRIZAJE SEGURO SOBRE UN LUGAR TERRESTRE NO PREPARADO EN CASO DE FALLO DE UNO DE LOS BLOQUES DE MOTORES.
ES94927134T 1993-09-07 1994-09-02 Aeronave hibrida. Expired - Lifetime ES2113676T3 (es)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
RU9393043825A RU2012512C1 (ru) 1993-09-07 1993-09-07 Комбинированный летательный аппарат

Publications (1)

Publication Number Publication Date
ES2113676T3 true ES2113676T3 (es) 1998-05-01

Family

ID=20147191

Family Applications (1)

Application Number Title Priority Date Filing Date
ES94927134T Expired - Lifetime ES2113676T3 (es) 1993-09-07 1994-09-02 Aeronave hibrida.

Country Status (14)

Country Link
US (1) US5873545A (es)
EP (1) EP0667283B1 (es)
JP (1) JPH08503672A (es)
AU (1) AU679564B2 (es)
CA (1) CA2148797A1 (es)
CZ (1) CZ121395A3 (es)
DE (1) DE59405105D1 (es)
ES (1) ES2113676T3 (es)
FI (1) FI952208A (es)
NO (1) NO951788L (es)
NZ (1) NZ273413A (es)
PL (1) PL309029A1 (es)
RU (1) RU2012512C1 (es)
WO (1) WO1995007215A1 (es)

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HUP0300840A2 (hu) * 2000-07-28 2003-07-28 Henkel Kommanditgesellschaft Auf Aktien Új, Bacillus sp. A 7-7 (DSM 12368)-ból extrahált amilolitikus enzim, valamint használata mosó- és tisztítószerekben
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US6672538B2 (en) * 2002-05-23 2004-01-06 Sikorsky Aircraft Corporation Transmission for a coaxial counter rotating rotor system
US20060144994A1 (en) 2002-08-30 2006-07-06 Peter Spirov Homeostatic flying hovercraft
US6732972B2 (en) 2002-09-13 2004-05-11 Frank S. Malvestuto, Jr. High-lift, low-drag, stall-resistant airfoil
US6715574B1 (en) * 2002-10-18 2004-04-06 Aeromobile, Inc. Airstream control system for a hovercraft
US7059931B2 (en) * 2003-05-27 2006-06-13 Veratech Aero-Rpv Corporation Reduced visibility rotorcraft and method of controlling flight of reduced visibility rotorcraft
US20050230525A1 (en) * 2004-03-30 2005-10-20 Paterro Von F C Craft with magnetically curved space
US7946526B2 (en) * 2004-11-05 2011-05-24 Nachman Zimet Rotary-wing vehicle system
US7581696B2 (en) 2005-11-09 2009-09-01 Morgan Aircraft, Llc Aircraft attitude control configuration
FR2929243B1 (fr) * 2008-03-25 2010-04-23 Eurocopter France Helicoptere hybride rapide a grande distance franchissable
WO2010036419A2 (en) * 2008-06-06 2010-04-01 Frontline Aerospace, Inc. Vtol aerial vehicle
JP2010023820A (ja) * 2008-07-22 2010-02-04 Keiichi Aoyanagi 垂直離着陸する飛行機
US8240597B2 (en) * 2008-08-06 2012-08-14 Honeywell International Inc. UAV ducted fan lip shaping
RU2422309C1 (ru) * 2010-01-11 2011-06-27 Александр Иосифович Филимонов Комбинированный летательный аппарат
CN101837195B (zh) * 2010-01-21 2012-02-08 罗之洪 一种垂直起降的模型飞机
RU2010104373A (ru) * 2010-02-08 2011-08-20 Александр Иосифович Филимонов (RU) Самолет на воздушной подушке с аэростатической разгрузкой
US8579227B2 (en) * 2011-01-24 2013-11-12 J. Kellogg Burnham Vertical and horizontal flight aircraft “sky rover”
EP2690010B1 (en) * 2012-07-27 2014-09-03 AIRBUS HELICOPTERS DEUTSCHLAND GmbH Compound helicopter with tail booms
US9004973B2 (en) 2012-10-05 2015-04-14 Qfo Labs, Inc. Remote-control flying copter and method
EP2738091B1 (en) * 2012-11-30 2015-07-22 AIRBUS HELICOPTERS DEUTSCHLAND GmbH Vertical take-off and landing (VTOL) aerial vehicle and method of operating such a VTOL aerial vehicle
CN103231803A (zh) * 2013-04-27 2013-08-07 哈尔滨飞机工业集团有限责任公司 一种小型无人飞行器构型
CN103448910A (zh) * 2013-08-31 2013-12-18 西北工业大学 一种可垂直起降的高速飞行器
RU2546359C1 (ru) * 2014-02-18 2015-04-10 Александр Иосифович Филимонов Экранолет внеаэродромного базирования
GB2528489A (en) 2014-07-23 2016-01-27 Cassidian Ltd Improvements in and relating to unmanned aerial vehicles
CN105775121A (zh) * 2014-12-26 2016-07-20 深圳智航无人机有限公司 一种变翼式无人机及其方法
US9914528B2 (en) * 2015-02-25 2018-03-13 Embraer S.A. Airframe-integrated propeller-driven propulsion systems
CN105015770A (zh) * 2015-07-29 2015-11-04 张飞 翼身融合单涵道垂直起降飞行器
RU2603808C1 (ru) * 2015-10-22 2016-11-27 Российская Федерация в лице Министерства промышленности и торговли Российской Федерации (Минпромторг России) Самолет с шасси на воздушной подушке
US10258888B2 (en) 2015-11-23 2019-04-16 Qfo Labs, Inc. Method and system for integrated real and virtual game play for multiple remotely-controlled aircraft
GB2555439A (en) * 2016-10-27 2018-05-02 Mono Aerospace Ip Ltd Vertical take-off and landing aircraft and control method
USD808329S1 (en) * 2017-01-18 2018-01-23 Aurora Flight Sciences Corporation Lenticular aircraft
US11712637B1 (en) 2018-03-23 2023-08-01 Steven M. Hoffberg Steerable disk or ball
CN109335004B (zh) * 2018-11-30 2024-04-26 福建星图智控科技有限公司 一种配置混合动力的微型无人机
CN113353254B (zh) * 2021-07-14 2023-02-28 空中舞者(威海)航空动力技术有限公司 一种垂直起降旋翼机
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Also Published As

Publication number Publication date
NZ273413A (en) 1997-05-26
FI952208A (fi) 1995-07-05
CZ121395A3 (en) 1996-02-14
EP0667283A4 (de) 1996-01-03
EP0667283B1 (de) 1998-01-21
FI952208A0 (fi) 1995-05-08
AU7668294A (en) 1995-03-27
CA2148797A1 (en) 1995-03-16
US5873545A (en) 1999-02-23
PL309029A1 (en) 1995-09-18
RU2012512C1 (ru) 1994-05-15
WO1995007215A1 (fr) 1995-03-16
EP0667283A1 (de) 1995-08-16
DE59405105D1 (de) 1998-02-26
NO951788D0 (no) 1995-05-08
NO951788L (no) 1995-06-13
AU679564B2 (en) 1997-07-03
JPH08503672A (ja) 1996-04-23

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