BR112014011295A2 - veículo - Google Patents

veículo

Info

Publication number
BR112014011295A2
BR112014011295A2 BR112014011295A BR112014011295A BR112014011295A2 BR 112014011295 A2 BR112014011295 A2 BR 112014011295A2 BR 112014011295 A BR112014011295 A BR 112014011295A BR 112014011295 A BR112014011295 A BR 112014011295A BR 112014011295 A2 BR112014011295 A2 BR 112014011295A2
Authority
BR
Brazil
Prior art keywords
tail segment
tail
segment
vehicle
tubular
Prior art date
Application number
BR112014011295A
Other languages
English (en)
Other versions
BR112014011295B1 (pt
Inventor
Cornelis Klok Christiaan
Petrus Valentijn Marie Van Rijn Louis
Alwin William Stekelenburg Michael
Christiaan Wegerif Robert
Adriaan Soethoudt Wouter
Original Assignee
Pal-V Europe N V
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 Pal-V Europe N V filed Critical Pal-V Europe N V
Publication of BR112014011295A2 publication Critical patent/BR112014011295A2/pt
Publication of BR112014011295B1 publication Critical patent/BR112014011295B1/pt

Links

Classifications

    • 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
    • B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C1/06—Frames; Stringers; Longerons ; Fuselage sections
    • B64C1/061—Frames
    • B64C1/063—Folding or collapsing to reduce overall dimensions, e.g. foldable tail booms
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C1/26—Attaching the wing or tail units or stabilising surfaces
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C1/30—Parts of fuselage relatively movable to reduce overall dimensions of aircraft
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C27/00—Rotorcraft; Rotors peculiar thereto
    • B64C27/02—Gyroplanes
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C27/00—Rotorcraft; Rotors peculiar thereto
    • B64C27/04—Helicopters
    • B64C27/06—Helicopters with single rotor
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C27/00—Rotorcraft; Rotors peculiar thereto
    • B64C27/32—Rotors
    • B64C27/46—Blades
    • B64C27/473—Constructional features
    • B64C27/50—Blades foldable to facilitate stowage of aircraft
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C27/00—Rotorcraft; Rotors peculiar thereto
    • B64C27/52—Tilting of rotor bodily relative to fuselage
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C37/00—Convertible aircraft

Abstract

abstract the present invention discloses a vehicle (1) capable of being converted between a flying condition and an automotive riding condition. the vehicle has a telescopically extendable tail (10) comprising a first tubular tail segment (11) and a second tail segment (12) disposed axially slideable within the first tubular tail segment. the tail is provided with at least two form-closing coupling members (21, 35; 31, 36) located at an axial distance (li) from each other for providing a force- transferring coupling between the second tail segment (12) and the first tubular tail segment (11) in the extended state of the second tail segment (12), each of said form-closing coupling members (21, 35; 31, 36) capable of transferring torque and transverse forces, and each of said form-closing coupling members (21, 35; 31, 36) coming into engagement by axial displacement of the second tail segment (12) in the outward direction. tradução resumo resumo patente de invenção: "veículo". trata-se de um veículo (1) capaz de ser convertido entre uma condição de voo e uma condição de direção automotiva. o veículo possui uma cauda telescopicamente extensível (10) que compreende um primeiro segmento de cauda tubular (11) e um segundo segmento de cauda (12) disposto axialmente deslizável dentro do primeiro segmento de cauda tubular. a cauda é fornecida com pelo menos dois elementos de acoplamento de fechamento de forma (21, 35; 31, 36) localizados em uma distância axial (li) um do outro para fornecer um acoplamento de transferência de força entre o segundo segmento de cauda (12) e o primeiro segmento de cauda tubular (11) no estado estendido do segundo segmento de cauda (12), sendo que cada um dos ditos elementos de acoplamento de fechamento de forma (21, 35; 31, 36) é capaz de transferir torque e forças transversais, e cada um dos ditos elementos de acoplamento de fechamento de forma (21, 35; 31, 36) entra em engate por deslocamento axial do segundo segmento de cauda (12) na direção para fora.
BR112014011295-9A 2011-11-11 2012-11-09 Cauda telescopicamente extensível de um veículo voador, veículo voador, veículo que é conversível entre uma condição de direção automotiva para dirigir em uma estrada e uma condição de voo para voar no ar, veículo voador que possui uma condição de voo para voar no ar, e veículo que é conversível entre uma condição de direção para dirigir em uma estrada e uma condição de voo para voar no ar BR112014011295B1 (pt)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
NL1039163A NL1039163C2 (en) 2011-11-11 2011-11-11 Vehicle.
NL1039163 2011-11-11
PCT/NL2012/000070 WO2013070061A1 (en) 2011-11-11 2012-11-09 Vehicle

Publications (2)

Publication Number Publication Date
BR112014011295A2 true BR112014011295A2 (pt) 2017-04-25
BR112014011295B1 BR112014011295B1 (pt) 2021-08-10

Family

ID=47263519

Family Applications (1)

Application Number Title Priority Date Filing Date
BR112014011295-9A BR112014011295B1 (pt) 2011-11-11 2012-11-09 Cauda telescopicamente extensível de um veículo voador, veículo voador, veículo que é conversível entre uma condição de direção automotiva para dirigir em uma estrada e uma condição de voo para voar no ar, veículo voador que possui uma condição de voo para voar no ar, e veículo que é conversível entre uma condição de direção para dirigir em uma estrada e uma condição de voo para voar no ar

Country Status (11)

Country Link
US (2) US9340081B2 (pt)
EP (2) EP2776259B1 (pt)
KR (1) KR102048104B1 (pt)
CN (2) CN104093580B (pt)
BR (1) BR112014011295B1 (pt)
ES (1) ES2748122T3 (pt)
HU (1) HUE046247T2 (pt)
MX (1) MX350275B (pt)
NL (1) NL1039163C2 (pt)
RU (1) RU2620454C2 (pt)
WO (1) WO2013070061A1 (pt)

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EP2933187B1 (en) * 2014-04-15 2017-01-11 AIRBUS HELICOPTERS DEUTSCHLAND GmbH Rotary wing aircraft with a multiple beam tail boom
CA3015471A1 (en) 2016-01-29 2017-08-03 JG Entrepreneurial Enterprises LLC Aeronautical car and associated features
DE102016006696A1 (de) 2016-05-27 2017-11-30 Christoph Jaeger Flugautosystem
IL249888B (en) 2017-01-01 2021-04-29 Levy Moshe Universal flying ground vehicle
NL1042265B1 (en) 2017-02-13 2018-09-04 Pal V Ip B V Fly/drive vehicle that is convertible between a road riding condition and a flying condition
CN107054623B (zh) * 2017-03-13 2023-09-05 普宙科技有限公司 无人机滑动式机臂装置及无人机
CN107719659A (zh) * 2017-08-28 2018-02-23 南京达索航空科技有限公司 一种垂直起降固定翼式飞行器
RU2699593C2 (ru) * 2017-12-15 2019-09-06 Харис Нуриахметович Мухаметшин Автоконвертоплан
CN208325617U (zh) * 2018-04-28 2019-01-04 上海飞来信息科技有限公司 轴距可变的多旋翼飞行器
RU2708497C1 (ru) * 2019-02-19 2019-12-09 Общество с ограниченной ответственностью Научно-производственное предприятие "Резонанс" (ООО НПП "Резонанс") Плавающая транспортная платформа
NL1043196B1 (en) * 2019-03-18 2020-09-25 Pal V Ip B V Rotor blades of a lift rotor
CN111824390A (zh) * 2020-07-24 2020-10-27 浙江点辰航空科技有限公司 一种具有可伸缩机翼的无人机
CN113459741A (zh) * 2021-07-21 2021-10-01 广东汇天航空航天科技有限公司 螺旋桨连接臂和汽车
US11673662B1 (en) * 2022-01-05 2023-06-13 Textron Innovations Inc. Telescoping tail assemblies for use on aircraft

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US2940688A (en) * 1956-08-27 1960-06-14 Edward F Bland Roadable aircraft and sailboat
US3116896A (en) * 1961-04-05 1964-01-07 Eltra Corp Combination helicopter-automobile
GB1091401A (en) * 1963-05-03 1967-11-15 Handley Page Ltd Improvements in relation to rotorcraft
US3321021A (en) * 1966-07-19 1967-05-23 Ryan Aeronautical Co Lightweight folding rotor
US4601639A (en) * 1984-03-19 1986-07-22 Bell Helicopter Textron Inc. Nodalized rotor
US4627585A (en) * 1984-06-25 1986-12-09 Harry Einstein Pusher type auto-plane
US4706907A (en) * 1985-01-29 1987-11-17 Eduard Kopylov Aircraft
CA1324366C (en) * 1989-06-28 1993-11-16 Peter Haseloh Gyroplane
US5050817A (en) * 1989-10-16 1991-09-24 Miller Harvey R Combined road and aircraft vehicle
IT1240175B (it) * 1990-04-06 1993-11-27 Agusta Spa Pala per elicottero
US5203520A (en) * 1991-10-28 1993-04-20 Jozef Przygodzki Helicar
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AUPP105297A0 (en) * 1997-12-22 1998-01-15 Kusic, Tom Tandem rotor vertical take-off variable body aircraft
US6978969B1 (en) * 2003-03-05 2005-12-27 Neal Larry R Fly-drive vehicle
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EA011979B1 (ru) * 2007-06-08 2009-06-30 Борис Иосифович Синельников Автоверт
US9259984B2 (en) * 2008-07-28 2016-02-16 Fleck Future Concepts Gmbh Combined air, water and road vehicle
CN201385556Y (zh) * 2009-04-08 2010-01-20 冯云龙 水路空多用变形汽车
US20100308174A1 (en) * 2009-06-03 2010-12-09 Grant Calverley Rotocraft power-generation, control apparatus and method
US8371520B2 (en) * 2009-07-31 2013-02-12 William Craig Easter Rapidly convertible hybrid aircraft and manufacturing method

Also Published As

Publication number Publication date
EP3604000B1 (en) 2023-10-25
CN107089107B (zh) 2019-10-22
ES2748122T3 (es) 2020-03-13
US20140291440A1 (en) 2014-10-02
EP3604000C0 (en) 2023-10-25
WO2013070061A1 (en) 2013-05-16
RU2014123713A (ru) 2015-12-20
EP2776259A1 (en) 2014-09-17
US9566839B2 (en) 2017-02-14
US20160229245A1 (en) 2016-08-11
RU2620454C2 (ru) 2017-05-25
BR112014011295B1 (pt) 2021-08-10
KR20140091715A (ko) 2014-07-22
MX2014005716A (es) 2015-03-09
MX350275B (es) 2017-08-31
US9340081B2 (en) 2016-05-17
CN104093580A (zh) 2014-10-08
NL1039163C2 (en) 2013-05-14
CN104093580B (zh) 2016-12-14
KR102048104B1 (ko) 2019-12-02
CN107089107A (zh) 2017-08-25
EP2776259B1 (en) 2019-07-10
EP3604000A1 (en) 2020-02-05
HUE046247T2 (hu) 2020-02-28

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Legal Events

Date Code Title Description
B06F Objections, documents and/or translations needed after an examination request according [chapter 6.6 patent gazette]
B06U Preliminary requirement: requests with searches performed by other patent offices: procedure suspended [chapter 6.21 patent gazette]
B09A Decision: intention to grant [chapter 9.1 patent gazette]
B350 Update of information on the portal [chapter 15.35 patent gazette]
B16A Patent or certificate of addition of invention granted [chapter 16.1 patent gazette]

Free format text: PRAZO DE VALIDADE: 20 (VINTE) ANOS CONTADOS A PARTIR DE 09/11/2012, OBSERVADAS AS CONDICOES LEGAIS.