BR112015020484A2 - aeronave - Google Patents

aeronave

Info

Publication number
BR112015020484A2
BR112015020484A2 BR112015020484A BR112015020484A BR112015020484A2 BR 112015020484 A2 BR112015020484 A2 BR 112015020484A2 BR 112015020484 A BR112015020484 A BR 112015020484A BR 112015020484 A BR112015020484 A BR 112015020484A BR 112015020484 A2 BR112015020484 A2 BR 112015020484A2
Authority
BR
Brazil
Prior art keywords
fuselage
canard
main wing
aircraft
coupled
Prior art date
Application number
BR112015020484A
Other languages
English (en)
Other versions
BR112015020484B1 (pt
Inventor
S Sommer Geoffrey
A Cote Kenneth
Original Assignee
Northrop Grumman Systems Corp
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 Northrop Grumman Systems Corp filed Critical Northrop Grumman Systems Corp
Publication of BR112015020484A2 publication Critical patent/BR112015020484A2/pt
Publication of BR112015020484B1 publication Critical patent/BR112015020484B1/pt

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C39/00—Aircraft not otherwise provided for
    • B64C39/12—Canard-type aircraft
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C3/00—Wings
    • B64C3/38—Adjustment of complete wings or parts thereof
    • B64C3/40—Varying angle of sweep
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C30/00—Supersonic type aircraft
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C5/00—Stabilising surfaces
    • B64C5/04—Noseplanes
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Toys (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Tires In General (AREA)

Abstract

1 / 1 resumo “ a e ro n a v e ” uma aeronave inclui uma fuselagem, uma asa principal articuladamente acoplada a uma porã§ã£o de rã© da fuselagem e um canard acoplado a uma porã§ã£o de vante da fuselagem, em que a asa principal e o canard sã£o configurados para serem conectados juntos para voo supersã´nico e desconectados uns dos outros para voo subsã´nico.
BR112015020484-8A 2013-02-27 2014-02-25 Aeronave BR112015020484B1 (pt)

Applications Claiming Priority (5)

Application Number Priority Date Filing Date Title
US201361770056P 2013-02-27 2013-02-27
US61/770,056 2013-02-27
US14/185,465 2014-02-20
US14/185,465 US9079663B2 (en) 2013-02-27 2014-02-20 Canard-locked oblique wing aircraft
PCT/US2014/018441 WO2014134072A1 (en) 2013-02-27 2014-02-25 Canard-locked oblique wing aircraft

Publications (2)

Publication Number Publication Date
BR112015020484A2 true BR112015020484A2 (pt) 2017-07-18
BR112015020484B1 BR112015020484B1 (pt) 2022-02-08

Family

ID=51387161

Family Applications (1)

Application Number Title Priority Date Filing Date
BR112015020484-8A BR112015020484B1 (pt) 2013-02-27 2014-02-25 Aeronave

Country Status (5)

Country Link
US (1) US9079663B2 (pt)
EP (1) EP2961652B1 (pt)
BR (1) BR112015020484B1 (pt)
CA (1) CA2901678C (pt)
WO (1) WO2014134072A1 (pt)

Families Citing this family (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2010111752A (ru) * 2007-08-29 2011-10-10 ЭДВАНСТ ПРОДАКТ ДИВЕЛОПМЕНТ, ЭлЭлСи (US) Летательный аппарат с корпусом в виде скользящего крыла смешанного типа
US9522727B2 (en) * 2012-11-28 2016-12-20 The Boeing Company Bilaterally asymmetric design for minimizing wave drag
US9387929B2 (en) * 2013-03-15 2016-07-12 Ian Todd Gaillimore Vertical takeoff and landing (“VTOL”) aircraft
US10464668B2 (en) 2015-09-02 2019-11-05 Jetoptera, Inc. Configuration for vertical take-off and landing system for aerial vehicles
US11001378B2 (en) 2016-08-08 2021-05-11 Jetoptera, Inc. Configuration for vertical take-off and landing system for aerial vehicles
IL257811B (en) 2015-09-02 2022-08-01 Jetoptera Inc Pleoidal propulsion system
EP3321186A1 (en) * 2016-11-14 2018-05-16 Airbus Operations GmbH Aircraft
EP3645854A4 (en) 2017-06-27 2021-03-24 Jetoptera, Inc. VERTICAL TAKE-OFF AND LANDING SYSTEM CONFIGURATION FOR AIR VEHICLES
US11685510B2 (en) * 2018-11-01 2023-06-27 Viettel Group Wing deployment mechanism and design method using pneumatic technique
CN109677587B (zh) * 2019-01-20 2022-01-25 成都飞机工业（集团）有限责任公司 一种可兼顾高低速飞行的斜置翼飞机的控制方法
CN115636079A (zh) * 2022-12-21 2023-01-24 中国航空工业集团公司沈阳空气动力研究所 一种超高升阻比的高空长航时无人机布局

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US2461805A (en) 1944-10-06 1949-02-15 Barker Parrish Airplane wing arrangement
US3737121A (en) 1971-12-09 1973-06-05 Nasa Dual-fuselage aircraft having yawable wing and horizontal stabilizer
US3942747A (en) 1972-12-27 1976-03-09 Julian Wolkovitch Joined wing aircraft
US3971535A (en) 1973-01-05 1976-07-27 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Oblique-wing supersonic aircraft
US4132374A (en) 1976-12-30 1979-01-02 The Boeing Company Wing pivot location and structure for oblique wing airplane
US4365773A (en) 1979-04-11 1982-12-28 Julian Wolkovitch Joined wing aircraft
US4336913A (en) * 1979-10-02 1982-06-29 Hall Eric B Compound wing aircraft
US4444365A (en) * 1981-11-25 1984-04-24 Omac, Inc. Double cam mounting assembly for mounting an aircraft wing to a fuselage to provide an adjustable angle of attack
FR2523072A1 (fr) * 1982-03-09 1983-09-16 Cabrol Lucien Aeronef pourvu d'une structure de sustentation a ailes superposees multiples
US4856736A (en) 1987-06-26 1989-08-15 Skywardens Limited Aircraft with paired aerofoils
US4998689A (en) 1989-07-14 1991-03-12 Rockwell International Corporation 90 degree rotation aircraft wing
US5899410A (en) 1996-12-13 1999-05-04 Mcdonnell Douglas Corporation Aerodynamic body having coplanar joined wings
US5984231A (en) 1998-06-19 1999-11-16 Northrop Grumman Corporation Aircraft with variable forward-sweep wing
US6474604B1 (en) * 1999-04-12 2002-11-05 Jerry E. Carlow Mobius-like joining structure for fluid dynamic foils
US6729577B2 (en) 2000-12-08 2004-05-04 Lockheed Martin Corporation Tail-braced wing aircraft and configurations for achieving long supersonic range and low sonic boom
US6986481B2 (en) * 2002-10-31 2006-01-17 Kazak Composites, Incorporated Extendable joined wing system for a fluid-born body
US6923404B1 (en) 2003-01-10 2005-08-02 Zona Technology, Inc. Apparatus and methods for variable sweep body conformal wing with application to projectiles, missiles, and unmanned air vehicles
US20050211827A1 (en) * 2004-03-29 2005-09-29 The Boeing Company High speed missile wing and associated method
US7131611B2 (en) * 2004-07-30 2006-11-07 Saint Louis University Device and method of control of fixed and variable geometry rhomboid wings
US7611090B2 (en) * 2005-12-20 2009-11-03 The Boeing Company Reaction-drive rotorcraft having an adjustable blade jet
US7841559B1 (en) * 2006-02-16 2010-11-30 Mbda Incorporated Aerial vehicle with variable aspect ratio deployable wings
US9545993B2 (en) * 2007-01-12 2017-01-17 John William McGinnis Aircraft stability and efficient control through induced drag reduction
WO2010036419A2 (en) * 2008-06-06 2010-04-01 Frontline Aerospace, Inc. Vtol aerial vehicle
FR2941915B1 (fr) * 2009-02-12 2013-05-10 Airbus France Aeronef presentant deux paires d'ailes
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US8444082B1 (en) * 2009-08-19 2013-05-21 The United States Of America, As Represented By The Secretary Of The Navy High performance ‘X’-configuration airplane for storage and launch from a tubular container
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FR2989063B1 (fr) * 2012-04-05 2015-01-02 Airbus Operations Sas Procede de couplage dissociable entre un module de propulsion et un module de transport d’un avion et avion modulaire de mise en oeuvre
WO2014074146A1 (en) * 2012-11-12 2014-05-15 United Technologies Corporation Box wing with angled gas turbine engine cores
USD724001S1 (en) * 2013-12-27 2015-03-10 Elytron Aircraft LLC Joined-wing tilt-wing aircraft

Also Published As

Publication number Publication date
US20140239117A1 (en) 2014-08-28
EP2961652B1 (en) 2017-01-04
WO2014134072A1 (en) 2014-09-04
CA2901678A1 (en) 2014-09-04
US9079663B2 (en) 2015-07-14
BR112015020484B1 (pt) 2022-02-08
CA2901678C (en) 2016-08-23
EP2961652A1 (en) 2016-01-06

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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]
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 25/02/2014, OBSERVADAS AS CONDICOES LEGAIS.