BR112017006721A2 - painel central de asa para um veículo aéreo e método de seu controle - Google Patents
painel central de asa para um veículo aéreo e método de seu controleInfo
- Publication number
- BR112017006721A2 BR112017006721A2 BR112017006721A BR112017006721A BR112017006721A2 BR 112017006721 A2 BR112017006721 A2 BR 112017006721A2 BR 112017006721 A BR112017006721 A BR 112017006721A BR 112017006721 A BR112017006721 A BR 112017006721A BR 112017006721 A2 BR112017006721 A2 BR 112017006721A2
- Authority
- BR
- Brazil
- Prior art keywords
- wing
- frame section
- geometry axis
- panel
- horizontal
- Prior art date
Links
- 230000008878 coupling Effects 0.000 abstract 1
- 238000010168 coupling process Methods 0.000 abstract 1
- 238000005859 coupling reaction Methods 0.000 abstract 1
- 230000007704 transition Effects 0.000 abstract 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C3/00—Wings
- B64C3/38—Adjustment of complete wings or parts thereof
- B64C3/56—Folding or collapsing to reduce overall dimensions of aircraft
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60F—VEHICLES FOR USE BOTH ON RAIL AND ON ROAD; AMPHIBIOUS OR LIKE VEHICLES; CONVERTIBLE VEHICLES
- B60F5/00—Other convertible vehicles, i.e. vehicles capable of travelling in or on different media
- B60F5/02—Other convertible vehicles, i.e. vehicles capable of travelling in or on different media convertible into aircraft
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C37/00—Convertible aircraft
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60Y—INDEXING SCHEME RELATING TO ASPECTS CROSS-CUTTING VEHICLE TECHNOLOGY
- B60Y2200/00—Type of vehicle
- B60Y2200/50—Aeroplanes, Helicopters
- B60Y2200/51—Aeroplanes
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/10—Drag reduction
Abstract
um painel central de asa para um veículo de transporte híbrido para transporte terrestre e aéreo. o painel central de assa possui uma seção de estrutura dianteira e uma seção de estrutura traseira conectadas por um ou mais elementos cruzados. o painel central de asa também pode ter um primeiro eixo geométrico vertical e um segundo eixo geométrico vertical, posicionados perto de extremidades opostas da seção de estrutura dianteira, onde uma primeira asa é configurada para girar em torno do primeiro eixo geométrico vertical e uma segunda asa é configurada para girar em torno do segundo eixo geométrico vertical para transitar entre um modo aéreo e um modo terrestre. o painel central de asa pode possuir adicionalmente um primeiro eixo geométrico horizontal estendendo-se substancialmente em paralelo ao longo de uma parte inferior da seção de estrutura dianteira, onde o painel central de asa é configurado para girar em torno do primeiro eixo geométrico horizontal permitindo o ajuste de um ângulo de ataque do veículo. o painel central de asa também pode ter um segundo eixo geométrico horizontal se estendendo ao longo de uma parte inferior da seção de estrutura traseira, onde a seção de estrutura traseira é configurada para girar em torno do segundo eixo geométrico horizontal para permitir o acoplamento e desacoplamento da seção de estrutura traseira da primeira asa e da segunda asa para transitar entre o modo aéreo e o modo terrestre.
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
SK50058-2014A SK288638B6 (sk) | 2014-10-08 | 2014-10-08 | Centroplán lietajúceho vozidla/hybridného dopravného prostriedku pre vzduch a súš a spôsob jeho ovládania centroplánom |
SK50123-2014U SK7493Y1 (sk) | 2014-10-08 | 2014-10-08 | Centroplán lietajúceho vozidla a spôsob jeho ovládania |
PCT/SK2015/000004 WO2016057004A1 (en) | 2014-10-08 | 2015-10-08 | Central wing panel for a flying vehicle and method of its control |
Publications (1)
Publication Number | Publication Date |
---|---|
BR112017006721A2 true BR112017006721A2 (pt) | 2017-12-19 |
Family
ID=60084164
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
BR112017006721A BR112017006721A2 (pt) | 2014-10-08 | 2015-10-08 | painel central de asa para um veículo aéreo e método de seu controle |
Country Status (8)
Country | Link |
---|---|
US (1) | US10611459B2 (pt) |
EP (1) | EP3204246B1 (pt) |
JP (1) | JP2017534515A (pt) |
KR (1) | KR20170066563A (pt) |
CN (1) | CN107107690B (pt) |
BR (1) | BR112017006721A2 (pt) |
RU (1) | RU2687543C2 (pt) |
WO (1) | WO2016057004A1 (pt) |
Families Citing this family (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE102016006696A1 (de) | 2016-05-27 | 2017-11-30 | Christoph Jaeger | Flugautosystem |
US20180079488A1 (en) * | 2016-09-21 | 2018-03-22 | Bell Helicopter Textron Inc. | Foldable aircraft with anhedral stabilizing wings |
EP3335916A1 (en) | 2016-12-13 | 2018-06-20 | AeroMobil R&D, s. r. o. | Acceleration control for a convertible air - road vehicle |
EP3335915B1 (en) | 2016-12-13 | 2019-12-04 | AeroMobil R&D, s. r. o. | Stability control for operation of a convertible air - road vehicle |
EP3335914B1 (en) | 2016-12-13 | 2019-11-13 | AeroMobil R&D, s. r. o. | Vehicle including control pedal arrangement |
EP3366570A1 (en) | 2017-02-22 | 2018-08-29 | AeroMobil R&D, s. r. o. | Wing folding |
EP3412560B1 (en) | 2017-06-05 | 2020-02-12 | AeroMobil R&D, s. r. o. | Wing folding |
EP3418184A1 (en) | 2017-06-20 | 2018-12-26 | AeroMobil R&D, s. r. o. | Wing flap system for flying car |
JP7265260B2 (ja) * | 2019-09-17 | 2023-04-26 | 国立研究開発法人宇宙航空研究開発機構 | 航空機 |
Family Cites Families (18)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB556478A (en) | 1942-04-04 | 1943-10-06 | Osmond Ernst Fletcher | Improvements in or relating to aircraft wings |
US2692095A (en) * | 1952-08-01 | 1954-10-19 | Fred A Carpenter | Convertible airplane and highway vehicle |
US2940688A (en) * | 1956-08-27 | 1960-06-14 | Edward F Bland | Roadable aircraft and sailboat |
FR2577198A1 (fr) * | 1985-02-13 | 1986-08-14 | Bazin Claudine | Avion convertible |
US4881700A (en) * | 1988-01-05 | 1989-11-21 | Branko Sarh | Convertible fixed wing aircraft |
RU2058911C1 (ru) * | 1988-06-15 | 1996-04-27 | Казанский государственный технический университет им.А.Н.Туполева | Устройство поворотного узла складывания крыла при базировании |
JPH0338499A (ja) * | 1989-07-03 | 1991-02-19 | Mitsubishi Heavy Ind Ltd | 可変主翼をもつ航空機 |
JPH04297798A (ja) * | 1991-03-04 | 1992-10-21 | Mitsubishi Electric Corp | 誘導飛しょう体 |
DE4119613C2 (de) * | 1991-06-14 | 1997-03-27 | Diehl Gmbh & Co | Flugkörper mit ausklappbaren Leiteinrichtungen |
US7946527B2 (en) * | 2007-09-10 | 2011-05-24 | Alan Glen Holmes | Aircraft with fixed, swinging and folding wings |
US8157206B2 (en) * | 2008-06-11 | 2012-04-17 | Icon Aircraft, Inc. | Two-motion wing-fold mechanism with independent load path |
WO2010012285A2 (en) * | 2008-07-28 | 2010-02-04 | Fleck Fitness Concepts Gmbh | Combined air, water and road vehicle |
US8464979B2 (en) * | 2009-06-02 | 2013-06-18 | Sunstar IM | Foldable swan-wings aircraft |
RU2403177C1 (ru) * | 2009-07-31 | 2010-11-10 | Общество С Ограниченной Ответственностью "Научно-Производственная Фирма "Сигма-Тс" | Самолет со складываемым крылом и устройство складывания крыла самолета |
US8162253B2 (en) * | 2009-08-19 | 2012-04-24 | Seiford Sr Donald S | Convertible vehicle for road, air, and water usage |
US10293935B2 (en) * | 2010-08-03 | 2019-05-21 | Tudor Crossfelt, Lp | Flying vehicle retractable wing hinge and truss |
SK6347Y1 (en) * | 2011-08-30 | 2013-01-02 | Aeromobil Sro | Method of transformation of hybrid vehicles for land and air and hybrid vehicle |
CN102616096A (zh) * | 2012-04-24 | 2012-08-01 | 赵辉 | 一种折叠机翼太阳能飞行汽车 |
-
2015
- 2015-10-08 KR KR1020177012129A patent/KR20170066563A/ko unknown
- 2015-10-08 RU RU2017115995A patent/RU2687543C2/ru not_active IP Right Cessation
- 2015-10-08 US US15/517,545 patent/US10611459B2/en active Active
- 2015-10-08 EP EP15801514.9A patent/EP3204246B1/en not_active Not-in-force
- 2015-10-08 CN CN201580054659.8A patent/CN107107690B/zh not_active Expired - Fee Related
- 2015-10-08 WO PCT/SK2015/000004 patent/WO2016057004A1/en active Application Filing
- 2015-10-08 BR BR112017006721A patent/BR112017006721A2/pt not_active Application Discontinuation
- 2015-10-08 JP JP2017518523A patent/JP2017534515A/ja not_active Ceased
Also Published As
Publication number | Publication date |
---|---|
KR20170066563A (ko) | 2017-06-14 |
RU2017115995A (ru) | 2018-11-13 |
WO2016057004A8 (en) | 2017-04-20 |
RU2017115995A3 (pt) | 2019-03-04 |
WO2016057004A1 (en) | 2016-04-14 |
US10611459B2 (en) | 2020-04-07 |
JP2017534515A (ja) | 2017-11-24 |
CN107107690A (zh) | 2017-08-29 |
CN107107690B (zh) | 2019-10-08 |
EP3204246A1 (en) | 2017-08-16 |
EP3204246B1 (en) | 2019-06-05 |
RU2687543C2 (ru) | 2019-05-14 |
US20170305527A1 (en) | 2017-10-26 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
BR112017006721A2 (pt) | painel central de asa para um veículo aéreo e método de seu controle | |
EP3630601A4 (en) | AUXILIARY POWER SYSTEM FOR GIRAVIONS WITH FOLDING PROPELLER ARMS AND DEFORMABLE ZONE LANDING GEAR | |
SG11201910744WA (en) | Vertical take-off and landing unmanned aerial vehicle having foldable fixed wing and based on twin-ducted fan power system | |
GB2534435B (en) | An unmanned aerial vehicle with folding wing arrangement | |
EP3465660A4 (en) | RADAR SYSTEM FOR TRACKING PILOTLESS AIR VEHICLES AND LOW-ALTITUDE FLYING OBJECTS | |
EP4292923A3 (en) | Aerial vehicle with deployable components | |
EP3303123A4 (en) | DEVICES AND METHODS FOR HYBRID VTOL / FIXED AIRPLANE STRUCTURES WITH TRANSFER IN FLIGHT AND FLIGHT MODES | |
GB2537559A (en) | Tilt wing aerial vehicle | |
EP3280638A4 (en) | Ground movement system plugin for vertical take off and landing unmanned aerial vehicles | |
EP3386853A4 (en) | AERIAL MULTI-ROTOR VEHICLE WITH REDUNDANCY OF SINGLE ARM FAILURE | |
EP3240726A4 (en) | Rotary wing vtol with fixed wing forward flight mode | |
EP3489721A4 (en) | PILOTLESS AIR VEHICLE FLIGHT CONTROL SYSTEM BASED ON CORS NETWORK DIFFERENTIAL POSITIONING | |
EP3765366A4 (en) | CONTRA-ROTATING PROPELLERS FOR AIRCRAFT | |
UA117715C2 (uk) | Посилений бампер автомобіля | |
EP3089911A4 (en) | Methods and systems for transitioning an aerial vehicle between crosswind flight and hover flight | |
EP3321180A4 (en) | Propeller unit deployment-type unmanned aerial vehicle | |
WO2014172719A3 (en) | A transition arrangement for an aircraft | |
EP3604122A4 (en) | SUPER HIGH ASPECT RATIO AIRCRAFT BASED ON AUTOMATICALLY DEPLOYING FOLDABLE WING TECHNOLOGY | |
BR112018001909A2 (pt) | método e sistema de controle de veículo | |
EP3046836A4 (en) | Methods and systems for transitioning an aerial vehicle between crosswind flight and hover flight | |
BR112017013552A2 (pt) | sistema de controle de chapa despigadora para uma plataforma de uma colheitadeira agrícola | |
EP3684686A4 (en) | PILOTLESS AIR VEHICLE WITH COAXIAL REVERSIBLE ROTORS | |
SG11202003249UA (en) | Wing structure and attachment to frame for unmanned aerial vehicles | |
GB201805438D0 (en) | Aircraft comprising a propulsion assembly including a pair of propellers at the rear of the fuselage | |
EP3652068C0 (en) | PLANE WITH AT LEAST TWO WINGLETS |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
B06U | Preliminary requirement: requests with searches performed by other patent offices: procedure suspended [chapter 6.21 patent gazette] | ||
B11B | Dismissal acc. art. 36, par 1 of ipl - no reply within 90 days to fullfil the necessary requirements |