BR112013002735A2 - articulação e armação de asa retrátil de veículo de voo - Google Patents

articulação e armação de asa retrátil de veículo de voo

Info

Publication number
BR112013002735A2
BR112013002735A2 BR112013002735A BR112013002735A BR112013002735A2 BR 112013002735 A2 BR112013002735 A2 BR 112013002735A2 BR 112013002735 A BR112013002735 A BR 112013002735A BR 112013002735 A BR112013002735 A BR 112013002735A BR 112013002735 A2 BR112013002735 A2 BR 112013002735A2
Authority
BR
Brazil
Prior art keywords
frame
wing
wings
flight vehicle
holders
Prior art date
Application number
BR112013002735A
Other languages
English (en)
Other versions
BR112013002735B1 (pt
Inventor
A Brown Matthew
N Roberts Robert
Hall Bousfield Samuel
A J Anemaat Willem
Original Assignee
Samson Aip Inc
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 Samson Aip Inc filed Critical Samson Aip Inc
Publication of BR112013002735A2 publication Critical patent/BR112013002735A2/pt
Publication of BR112013002735B1 publication Critical patent/BR112013002735B1/pt

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C37/00—Convertible aircraft
    • 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
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C5/00—Stabilising surfaces
    • B64C5/10—Stabilising surfaces adjustable
    • B64C5/12—Stabilising surfaces adjustable for retraction against or within fuselage or nacelle

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Bridges Or Land Bridges (AREA)
  • Vehicle Step Arrangements And Article Storage (AREA)
  • Body Structure For Vehicles (AREA)

Abstract

articulação e armação de asa retrátil de veículo de voo. a presente invenção refere-se a uma armação para um veículo de voo que suporta um par de asas em uma maneira que facilita a articulação das asas entre uma configuração desdobrada e uma configuração retraída. a armação inclui placas de topo e de fundo paralelas com a folga entre elas. as asas têm suportes de asa fixados a mesma com os suportes de asa articulavelmente suportados pelos conjntos de articulação á placa superior e á placa de fundo de armação. os conjuntos de travas poem ser seletivamente acionados para segurarem os suportes de asa e asas associadas á armação em, ou na configuração desdobrada, ou na configuração retraída, de modo que cargas entre as asas e a armação sejam principalmente transportadas através dos conjuntos de travas preferivelmente do que através dos conjuntos de articulações. uma posição de articulação na armação e nos suportes de asa é selecionada para maximizar o comprimento da asa ponta a ponta, enquanto minimiza um contorno requerido para o veículo quando as asas estão totalmente retraídas.
BR112013002735-5A 2010-08-03 2011-08-02 veículo de voo com asas retráteis, conjunto de asa e de armação para um veículo de voo que define asas retráteis e veículo de voo com uma asa oscilante BR112013002735B1 (pt)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US40089610P 2010-08-03 2010-08-03
US61/400,896 2010-08-03
PCT/US2011/001355 WO2012018382A2 (en) 2010-08-03 2011-08-02 Flying vehicle retractable wing hinge and truss

Publications (2)

Publication Number Publication Date
BR112013002735A2 true BR112013002735A2 (pt) 2017-06-27
BR112013002735B1 BR112013002735B1 (pt) 2021-02-02

Family

ID=45555410

Family Applications (1)

Application Number Title Priority Date Filing Date
BR112013002735-5A BR112013002735B1 (pt) 2010-08-03 2011-08-02 veículo de voo com asas retráteis, conjunto de asa e de armação para um veículo de voo que define asas retráteis e veículo de voo com uma asa oscilante

Country Status (5)

Country Link
US (2) US10293935B2 (pt)
JP (1) JP5960139B2 (pt)
BR (1) BR112013002735B1 (pt)
WO (1) WO2012018382A2 (pt)
ZA (1) ZA201301527B (pt)

Families Citing this family (23)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB201018185D0 (en) * 2010-10-28 2010-12-08 Airbus Operations Ltd Wing tip device attachment apparatus and method
US9290260B2 (en) 2011-10-01 2016-03-22 The Boeing Company Wing fold controller
US9211946B2 (en) 2011-10-01 2015-12-15 The Boeing Company Wing fold system with latch pins through multiple mating lugs
US9296469B2 (en) 2011-10-01 2016-03-29 The Boeing Company Horizontal folding wingtip
US9499252B2 (en) 2011-10-01 2016-11-22 The Boeing Company Wing fold controller
US9469392B2 (en) 2012-10-30 2016-10-18 The Boeing Company Wing fold system rotating latch
US9415857B2 (en) 2012-10-30 2016-08-16 The Boeing Company Wing fold system
US9296471B2 (en) * 2013-10-06 2016-03-29 The Boeing Company Swing wing tip system, assembly and method with dual load path structure
CN103692873B (zh) * 2013-12-20 2015-11-18 胡新如 一种水陆飞行汽车
AU2015200677B2 (en) * 2014-04-25 2019-01-17 The Boeing Company System for latching and locking a foldable airfoil
GB2530578A (en) 2014-09-29 2016-03-30 Airbus Operations Ltd Interface for control of a foldable wing on an aircraft
BR112017006721A2 (pt) * 2014-10-08 2017-12-19 Aeromobil Sro painel central de asa para um veículo aéreo e método de seu controle
US11027584B1 (en) * 2015-07-22 2021-06-08 Taras Kiceniuk, Jr. Flying car with fore and aft lifting surfaces
CN105857573B (zh) * 2016-04-23 2017-12-26 广州市绿化公司 一种市政园林绿化用智能无人机
SK500352017A3 (sk) * 2017-05-11 2018-12-03 Štefan Klein Spôsob transformácie motorového dopravného prostriedku na transport na zemskom povrchu a vo vzduchu a motorový dopravný prostriedok
WO2019021521A1 (ja) * 2017-07-27 2019-01-31 株式会社辰巳菱機 浮遊型移動装置
GB2573120A (en) * 2018-04-24 2019-10-30 Airbus Operations Ltd Improved secondary locking mechanism
US11370526B2 (en) * 2018-05-31 2022-06-28 Airbus Operations Gmbh Latching device for a wing arrangement for an aircraft
US11319054B2 (en) * 2018-05-31 2022-05-03 Airbus Operations Gmbh Wing arrangement for an aircraft
CN110550187A (zh) * 2018-06-01 2019-12-10 空中客车德国运营有限责任公司 用于飞行器的机翼装置和飞行器
EP3587252A1 (en) * 2018-06-28 2020-01-01 Airbus Operations GmbH Arresting system for arresting a first aircraft component relative to a second aircraft component
US11046416B2 (en) * 2018-08-03 2021-06-29 Aurora Flight Sciences Corporation Combination flight and ground apparatus for a vehicle
US11524780B2 (en) 2021-01-07 2022-12-13 Faruk Hossain Fan powered folding wing bicycle apparatus

Family Cites Families (23)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1998148A (en) * 1934-04-18 1935-04-16 Vieriu Daniel Auto-aeroplane
US2573271A (en) * 1947-06-30 1951-10-30 Adolph R Perl Roadable aircraft
US3285540A (en) * 1964-06-15 1966-11-15 Lee Shao-Tang Shiftable variable area wing construction
GB1135946A (en) * 1965-04-01 1968-12-11 British Aircraft Corp Ltd Improvements in aircraft
US3489375A (en) * 1967-11-21 1970-01-13 Richard R Tracy Variable lifting surface craft
FR1601027A (pt) * 1968-12-30 1970-08-03
US3606978A (en) * 1969-10-16 1971-09-21 Boeing Co Wing sweep pivot-bearing arrangement
IL39260A (en) * 1972-04-21 1975-06-25 Bouchnik J Detachable cabin aircraft
US4212441A (en) * 1978-05-11 1980-07-15 The United States Of America As Represented By The Secretary Of The Air Force Wing pivot assembly for variable sweep wing aircraft
US4703905A (en) * 1985-09-05 1987-11-03 Grumman Aerospace Corporation Manned entry vehicle system
JPS6449899A (en) * 1987-08-20 1989-02-27 Mitsubishi Electric Corp Guided missile
US4915664A (en) * 1988-12-22 1990-04-10 Erik Bakker Toy glider with wing converging mechanism
US5050817A (en) * 1989-10-16 1991-09-24 Miller Harvey R Combined road and aircraft vehicle
US5192037A (en) * 1991-08-23 1993-03-09 Mcdonnell Douglas Corporation Double-pivoting deployment system for aerosurfaces
US5899410A (en) * 1996-12-13 1999-05-04 Mcdonnell Douglas Corporation Aerodynamic body having coplanar joined wings
DE19827277B4 (de) * 1998-06-19 2006-08-10 Diehl Stiftung & Co.Kg Lageranordnung für die aufschwenkbaren Ruderblätter eines lenkbaren Flugkörpers
US5984231A (en) * 1998-06-19 1999-11-16 Northrop Grumman Corporation Aircraft with variable forward-sweep wing
US6073882A (en) * 1998-09-21 2000-06-13 Zieger; N. Henning Flying vehicle with retractable wing assembly
US6089503A (en) * 1999-01-15 2000-07-18 Northrop Grumman Corp Selectively rotatable and torsionally flexible aerodynamic control apparatus
FR2836889B1 (fr) * 2002-03-11 2004-05-28 Eurocopter France Procede et dispositif de repliage-depliage des pales d'un rotor de giravion
JP4171913B2 (ja) * 2004-04-13 2008-10-29 独立行政法人 宇宙航空研究開発機構 低ブーム特性と低抵抗特性を両立する可変前進翼超音速航空機
US7559505B2 (en) * 2005-12-01 2009-07-14 Lockheed Martin Corporation Apparatus and method for restraining and deploying an airfoil
US7946527B2 (en) * 2007-09-10 2011-05-24 Alan Glen Holmes Aircraft with fixed, swinging and folding wings

Also Published As

Publication number Publication date
US10293935B2 (en) 2019-05-21
BR112013002735B1 (pt) 2021-02-02
US20120032023A1 (en) 2012-02-09
ZA201301527B (en) 2013-11-27
WO2012018382A3 (en) 2012-06-14
US20190300170A1 (en) 2019-10-03
JP2014503400A (ja) 2014-02-13
WO2012018382A2 (en) 2012-02-09
JP5960139B2 (ja) 2016-08-02
US11142312B2 (en) 2021-10-12

Similar Documents

Publication Publication Date Title
BR112013002735A2 (pt) articulação e armação de asa retrátil de veículo de voo
JP2014503400A5 (pt)
BR112015017337A2 (pt) compartimento de bagagem superior para aeronave
BRPI1101187A8 (pt) assento de veículo com elemento deslizante
BR112015013009A2 (pt) aeronave conversível dotada de dois rotores carenados na extremidade da asa e de uma ventoinha horizontal na fuselagem
BR112013030012A2 (pt) dispositivo para folhas de portas de correr com fechamento coplanar, particularmente para mobiliário e semelhante
BR112013031257A2 (pt) fecho de peça única para equipar um recipiente
BR112014031099A2 (pt) estrutura de parte posterior de corpo de veículo
BRPI0821427A2 (pt) Componente estrutural de fuselagem da asa para a ligação duas asas de sustentação e uma seção de fuselagem em um avião.
WO2016187310A3 (en) Helicopter blade folding apparatus
BR112013025160A2 (pt) dispositivo de alta elevação de uma aeronave
IN2014MU02903A (pt)
BR112015005805A2 (pt) cabine de ponte de embarque e desembarque e ponte de embarque e desembarque com o mesmo método de interface
BR112012024769A2 (pt) dispositivo de estrutura de elevação
NZ708639A (en) Pinch valve having pivotably mounted upper and lower casings
BR112014029201A2 (pt) embalagem cartonada e matriz de embalagem cartonada
BR112015017932A2 (pt) aparelho de fixação
BR112012022077A2 (pt) chassi de um caminhão de controle avançado com uma cabine inclinável
BR112014030055A2 (pt) grade lateral da cama
CN203957690U (zh) 画板装置
CN205541764U (zh) 一种能够自动打开的汽车三角警示牌
BRPI0706140A2 (pt) biplano tandem com fuselagem de piso múltiplo
CN204048689U (zh) 一种穿衣柜
CN206458126U (zh) 用于听力体检的移动隔音板房
CN204826968U (zh) 快拆式铰链

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]
B06A Patent application procedure suspended [chapter 6.1 patent gazette]
B09A Decision: intention to grant [chapter 9.1 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 02/08/2011, OBSERVADAS AS CONDICOES LEGAIS.