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BRPI0311741A2 - controle de uma aeronave como um pêndulo orientado por vetores de empuxo na vertical, na horizontal e em todos os seus modos transicionais de vôo - Google Patents

controle de uma aeronave como um pêndulo orientado por vetores de empuxo na vertical, na horizontal e em todos os seus modos transicionais de vôo

Info

Publication number
BRPI0311741A2
BRPI0311741A2 BRPI0311741A BR0311741A BRPI0311741A2 BR PI0311741 A2 BRPI0311741 A2 BR PI0311741A2 BR PI0311741 A BRPI0311741 A BR PI0311741A BR 0311741 A BR0311741 A BR 0311741A BR PI0311741 A2 BRPI0311741 A2 BR PI0311741A2
Authority
BR
Brazil
Prior art keywords
aircraft
horizontal
vertical
control
flight modes
Prior art date
Application number
BRPI0311741A
Other languages
English (en)
Inventor
Thomas Sash
Original Assignee
Thomas Sash
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 Thomas Sash filed Critical Thomas Sash
Publication of BRPI0311741A2 publication Critical patent/BRPI0311741A2/pt

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
    • B64C29/0033—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 tiltable relative to the fuselage
    • 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
    • B64C27/28—Compound rotorcraft, i.e. aircraft using in flight the features of both aeroplane and rotorcraft with forward-propulsion propellers pivotable to act as lifting rotors
    • 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
    • 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
    • B64C29/0041—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 jet motors
    • B64C29/0075—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 jet motors the motors being tiltable relative to the fuselage
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C3/00—Wings
    • B64C3/38—Adjustment of complete wings or parts thereof
    • B64C3/385—Variable incidence wings
    • 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)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Toys (AREA)
  • Vehicle Body Suspensions (AREA)
  • Body Structure For Vehicles (AREA)
BRPI0311741A 2002-06-12 2003-06-11 controle de uma aeronave como um pêndulo orientado por vetores de empuxo na vertical, na horizontal e em todos os seus modos transicionais de vôo BRPI0311741A2 (pt)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US38843502P 2002-06-12 2002-06-12
PCT/US2003/018288 WO2003106259A2 (en) 2002-06-12 2003-06-11 Control of an aircraft as a thrust-vectored pendulum in vertical, horizontal and all flight transitional modes thereof
US10/458,737 US6863241B2 (en) 2002-06-12 2003-06-11 Control of an aircraft as a thrust-vectored pendulum in vertical, horizontal and all flight transitional modes thereof

Publications (1)

Publication Number Publication Date
BRPI0311741A2 true BRPI0311741A2 (pt) 2016-06-28

Family

ID=29740025

Family Applications (1)

Application Number Title Priority Date Filing Date
BRPI0311741A BRPI0311741A2 (pt) 2002-06-12 2003-06-11 controle de uma aeronave como um pêndulo orientado por vetores de empuxo na vertical, na horizontal e em todos os seus modos transicionais de vôo

Country Status (7)

Country Link
US (1) US6863241B2 (pt)
EP (1) EP1511671A4 (pt)
AU (1) AU2003248659A1 (pt)
BR (1) BRPI0311741A2 (pt)
CA (1) CA2489591A1 (pt)
IL (1) IL165682A0 (pt)
WO (1) WO2003106259A2 (pt)

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GB2409845A (en) 2004-01-08 2005-07-13 Robert Graham Burrage Tilt-rotor aircraft changeable between vertical lift and forward flight modes
GB2418405B (en) * 2004-09-23 2010-03-10 Paul Vincenzi Rotorcraft
US7395988B2 (en) * 2005-11-02 2008-07-08 The Boeing Company Rotor wing aircraft having an adjustable tail nozzle
US8757537B2 (en) * 2005-11-02 2014-06-24 The Boeing Company Systems and methods for rotor/wing aircraft
US20070215750A1 (en) * 2005-11-18 2007-09-20 Michael Shantz Radio controlled helicopter
US20080230656A1 (en) * 2006-04-11 2008-09-25 Moshe Kretchmer Aircraft wings having hinged vanes and aircraft having said wings
US20080183341A1 (en) * 2006-08-22 2008-07-31 Neu Wayne L Method and apparatus for torque control for machinery using counter-rotating drives
JP4840930B2 (ja) * 2007-01-25 2011-12-21 株式会社リコー 粉体供給装置、画像形成装置、及び、粉体収容部の輸送方法
CN101618763A (zh) * 2008-07-02 2010-01-06 孙为红 微型高速直升自旋翼飞行器
US8366037B2 (en) * 2009-05-22 2013-02-05 Heliplane, Llc Towable aerovehicle system with automated tow line release
US8505846B1 (en) * 2010-05-11 2013-08-13 II Stanley Gordon Sanders Vertical takeoff and landing aircraft
DE102010021024B4 (de) 2010-05-19 2014-07-03 Eads Deutschland Gmbh Hauptrotorantrieb für Hubschrauber
DE102010021026A1 (de) 2010-05-19 2011-11-24 Eads Deutschland Gmbh Hybrides Antriebs- und Energiesystem für Fluggeräte
DE102010021025B4 (de) 2010-05-19 2014-05-08 Eads Deutschland Gmbh Hubschrauber mit Hybridantrieb
US8646719B2 (en) 2010-08-23 2014-02-11 Heliplane, Llc Marine vessel-towable aerovehicle system with automated tow line release
FR2977948B1 (fr) * 2011-07-12 2014-11-07 Eurocopter France Procede de pilotage automatique d'un aeronef a voilure tournante comprenant au moins une helice propulsive, dispositif de pilotage automatique et aeronef
US10054939B1 (en) 2012-09-22 2018-08-21 Paul G. Applewhite Unmanned aerial vehicle systems and methods of use
WO2014088443A1 (ru) * 2012-12-04 2014-06-12 КОЛЕСНИК, Яков Александрович Соосный скоростной вертолет
JP6213713B2 (ja) * 2013-05-16 2017-10-18 株式会社Ihi 垂直離着陸機
EP2899118B1 (en) * 2014-01-27 2019-01-16 AIRBUS HELICOPTERS DEUTSCHLAND GmbH Rotorcraft with a fuselage and at least one main rotor
US10464668B2 (en) 2015-09-02 2019-11-05 Jetoptera, Inc. Configuration for vertical take-off and landing system for aerial vehicles
IL257811B (en) 2015-09-02 2022-08-01 Jetoptera Inc Fluidic propulsive system
US11001378B2 (en) 2016-08-08 2021-05-11 Jetoptera, Inc. Configuration for vertical take-off and landing system for aerial vehicles
US10167078B2 (en) * 2015-09-21 2019-01-01 Sikorsky Aircraft Corporation Rotary or fixed wing aircraft with thrust vectoring tail
EP3645854A4 (en) 2017-06-27 2021-03-24 Jetoptera, Inc. VERTICAL TAKE-OFF AND LANDING SYSTEM CONFIGURATION FOR AIR VEHICLES
US10946956B2 (en) * 2018-08-30 2021-03-16 Textron Innovations Inc. Unmanned aerial systems having out of phase gimballing axes
JP6609760B1 (ja) * 2018-09-22 2019-11-27 株式会社エアロネクスト 飛行体
CN109737024A (zh) * 2019-03-08 2019-05-10 中国计量大学 一种光子推力叠加飞行器推进动力系统
GB201909464D0 (en) * 2019-07-01 2019-08-14 Rolls Royce Plc Aircraft control method
US11225323B2 (en) * 2019-08-15 2022-01-18 Textron Innovations Inc. Centerline tiltrotor
EP3889727B1 (en) * 2020-03-30 2024-04-03 Volocopter GmbH Method of controlling an aircraft, flight control device for an aircraft, and aircraft with such flight control device
US11834164B2 (en) 2020-05-18 2023-12-05 Iqinetics Technologies Inc. Pulse-induced cyclic control lift propeller
US11787539B2 (en) * 2021-04-01 2023-10-17 Xingkang Li Convertible aircraft system
US20220363376A1 (en) * 2021-04-04 2022-11-17 Autonomous Flight Systems Inc. Free Wing Multirotor Transitional S/VTOL Aircraft
US12151808B2 (en) 2022-08-17 2024-11-26 Honeywell International, Inc. Aircraft and methods of operating the same to increase descent angles thereof

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US2448392A (en) * 1946-04-04 1948-08-31 John C Quady Convertible type aircraft
US3118504A (en) * 1961-02-13 1964-01-21 Bell Aerospace Corp Method for control of rotary wing aircraft
US3166271A (en) * 1962-08-20 1965-01-19 Daniel R Zuck Airplane having non-stalling wings and wing-mounted propellers
US3284027A (en) * 1964-01-09 1966-11-08 Nord Aviation Vtol aircraft having freely pivoted propulsion means
US3430894A (en) * 1967-04-17 1969-03-04 Air Vehicle Corp Vtol aircraft having free-floating wings and independently tilting propellers
US3934843A (en) 1974-08-05 1976-01-27 Black John O Free wing for convertible aircraft structure
US4059247A (en) * 1976-09-15 1977-11-22 Prewitt Richard H Convertiblade
US4730795A (en) 1984-03-26 1988-03-15 David Constant V Heliplane
USRE36487E (en) * 1989-02-09 2000-01-11 Freewing Aerial Robotics Corporation Airplane with variable-incidence wing
CA1324366C (en) * 1989-06-28 1993-11-16 Peter Haseloh Gyroplane
US5863013A (en) * 1991-11-20 1999-01-26 Freewing Aerial Robotics Corporation STOL/VTOL free wing aircraft with improved shock dampening and absorbing means
US5839691A (en) * 1996-05-22 1998-11-24 Lariviere; Jean Soulez Vertical takeoff and landing aircraft
US5758844A (en) 1996-05-28 1998-06-02 Boeing North American, Inc. Vertical/short take-off and landing (V/STOL) air vehicle capable of providing high speed horizontal flight
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US6293492B1 (en) * 1998-09-02 2001-09-25 Engineering System Co., Ltd. Coaxial twin-rotor type helicopter
US6382556B1 (en) 1999-12-20 2002-05-07 Roger N. C. Pham VTOL airplane with only one tiltable prop-rotor
US6343768B1 (en) 2000-05-16 2002-02-05 Patrick John Muldoon Vertical/short take-off and landing aircraft
US6783096B2 (en) * 2001-01-31 2004-08-31 G. Douglas Baldwin Vertical lift flying craft

Also Published As

Publication number Publication date
WO2003106259A2 (en) 2003-12-24
EP1511671A2 (en) 2005-03-09
WO2003106259A3 (en) 2004-04-01
IL165682A0 (en) 2006-01-15
CA2489591A1 (en) 2003-12-24
AU2003248659A1 (en) 2003-12-31
US6863241B2 (en) 2005-03-08
AU2003248659A8 (en) 2003-12-31
EP1511671A4 (en) 2006-04-12
US20040075017A1 (en) 2004-04-22

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Legal Events

Date Code Title Description
B06H Technical and formal requirements: requirement cancelled [chapter 6.8 patent gazette]

Free format text: ANULACAO DA PUBLICACAO CODIGO 6.7 NA RPI NO 1884 DE 13/02/2007, POR TER SIDO INDEVIDA

B08F Application dismissed because of non-payment of annual fees [chapter 8.6 patent gazette]

Free format text: REFERENTE AS 9A, 10A, 11A, 12A E 13A ANUIDADES.

B08K Patent lapsed as no evidence of payment of the annual fee has been furnished to inpi [chapter 8.11 patent gazette]

Free format text: EM VIRTUDE DO ARQUIVAMENTO PUBLICADO NA RPI 2376 DE 19-07-2016 E CONSIDERANDO AUSENCIA DE MANIFESTACAO DENTRO DOS PRAZOS LEGAIS, INFORMO QUE CABE SER MANTIDO O ARQUIVAMENTO DO PEDIDO DE PATENTE, CONFORME O DISPOSTO NO ARTIGO 12, DA RESOLUCAO 113/2013.