BRPI0509723A - sistema de aumento de sustentação para uso em uma aeronave, e, célula de avião incluindo um sistema de aumento de sustentação - Google Patents

sistema de aumento de sustentação para uso em uma aeronave, e, célula de avião incluindo um sistema de aumento de sustentação

Info

Publication number
BRPI0509723A
BRPI0509723A BRPI0509723-1A BRPI0509723A BRPI0509723A BR PI0509723 A BRPI0509723 A BR PI0509723A BR PI0509723 A BRPI0509723 A BR PI0509723A BR PI0509723 A BRPI0509723 A BR PI0509723A
Authority
BR
Brazil
Prior art keywords
lift
aircraft
airplane
cell including
airplane cell
Prior art date
Application number
BRPI0509723-1A
Other languages
English (en)
Inventor
John R Lee
Craig Lee
Charles Eastlake
James G Ladesic
Peter Mahr
Peter S Pierpont
Richard P Anderson
Original Assignee
John R Lee
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 John R Lee filed Critical John R Lee
Publication of BRPI0509723A publication Critical patent/BRPI0509723A/pt

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C3/00—Wings
    • B64C3/38—Adjustment of complete wings or parts thereof
    • B64C3/54—Varying in area
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C23/00—Influencing air flow over aircraft surfaces, not otherwise provided for
    • B64C23/06—Influencing air flow over aircraft surfaces, not otherwise provided for by generating vortices
    • B64C23/065—Influencing air flow over aircraft surfaces, not otherwise provided for by generating vortices at the wing tips
    • B64C23/069—Influencing air flow over aircraft surfaces, not otherwise provided for by generating vortices at the wing tips using one or more wing tip airfoil devices, e.g. winglets, splines, wing tip fences or raked wingtips
    • B64C23/072—Influencing air flow over aircraft surfaces, not otherwise provided for by generating vortices at the wing tips using one or more wing tip airfoil devices, e.g. winglets, splines, wing tip fences or raked wingtips the wing tip airfoil devices being moveable in their entirety
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C11/00—Propellers, e.g. of ducted type; Features common to propellers and rotors for rotorcraft
    • B64C11/001—Shrouded propellers
    • 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
    • B64C3/00—Wings
    • B64C3/58—Wings provided with fences or spoilers
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C39/00—Aircraft not otherwise provided for
    • B64C39/04—Aircraft not otherwise provided for having multiple fuselages or tail booms
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U30/00—Means for producing lift; Empennages; Arrangements thereof
    • B64U30/10—Wings
    • B64U30/12—Variable or detachable wings, e.g. wings with adjustable sweep
    • B64U30/14—Variable or detachable wings, e.g. wings with adjustable sweep detachable
    • 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)
  • Emergency Lowering Means (AREA)
  • Forklifts And Lifting Vehicles (AREA)

Abstract

SISTEMA DE AUMENTO DE SUSTENTAçãO PARA USO EM UMA AERONAVE, E, CéLULA DE AVIãO INCLUINDO UM SISTEMA DE AUMENTO DE SUSTENTAçãO. Esta invenção se refere geralmente a um sistema de aumento de sustentação para uma célula de avião. Mais particularmente, a invenção se refere à combinação de pontas de asa extensíveis/retraíveis com ao célula de avião para aumentar a sustentação bem como asas que podem pivotar para uma posição estendida. Elementos de superfície flexíveis podem ser rolados para se alojar e desenrolados para se estender com pelo menos um sendo na superfície de sucção da asa e pelo menos um sendo na superfície de pressão da asa.
BRPI0509723-1A 2004-04-07 2005-04-07 sistema de aumento de sustentação para uso em uma aeronave, e, célula de avião incluindo um sistema de aumento de sustentação BRPI0509723A (pt)

Applications Claiming Priority (7)

Application Number Priority Date Filing Date Title
US55997204P 2004-04-07 2004-04-07
US55997004P 2004-04-07 2004-04-07
US55997104P 2004-04-07 2004-04-07
US56096204P 2004-04-12 2004-04-12
US57502804P 2004-05-28 2004-05-28
US61640804P 2004-10-07 2004-10-07
PCT/US2005/011541 WO2005099380A2 (en) 2004-04-07 2005-04-07 Lift augmentation system

Publications (1)

Publication Number Publication Date
BRPI0509723A true BRPI0509723A (pt) 2007-09-25

Family

ID=35150425

Family Applications (1)

Application Number Title Priority Date Filing Date
BRPI0509723-1A BRPI0509723A (pt) 2004-04-07 2005-04-07 sistema de aumento de sustentação para uso em uma aeronave, e, célula de avião incluindo um sistema de aumento de sustentação

Country Status (5)

Country Link
EP (1) EP1755945A2 (pt)
BR (1) BRPI0509723A (pt)
CA (1) CA2561366A1 (pt)
IL (1) IL178431A0 (pt)
WO (1) WO2005099380A2 (pt)

Families Citing this family (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
BRPI0603262B1 (pt) * 2006-08-08 2021-02-23 Yaborã Indústria Aeronáutica S.A asa de aeronave incluindo um slat no bordo de ataque da asa e um fence rígido preso a uma porção estruturalmente rígida não móvel da asa
EP2303685B1 (en) 2008-06-20 2015-10-07 Aviation Partners, Inc. Curved wing tip
US9302766B2 (en) 2008-06-20 2016-04-05 Aviation Partners, Inc. Split blended winglet
GB201011843D0 (en) 2010-07-14 2010-09-01 Airbus Operations Ltd Wing tip device
ES2856270T3 (es) 2011-06-09 2021-09-27 Aviation Partners Inc El winglet integrado doble
RU2537350C1 (ru) * 2013-06-04 2015-01-10 Максим Петрович Смирнов Аппарат на воздушной подушке
KR20230145238A (ko) 2015-09-02 2023-10-17 제톱테라 잉크. 유체 추진 시스템
US11001378B2 (en) 2016-08-08 2021-05-11 Jetoptera, Inc. Configuration for vertical take-off and landing system for aerial vehicles
USD868627S1 (en) 2018-04-27 2019-12-03 Jetoptera, Inc. Flying car
US10464668B2 (en) 2015-09-02 2019-11-05 Jetoptera, Inc. Configuration for vertical take-off and landing system for aerial vehicles
CN106541795A (zh) * 2016-09-26 2017-03-29 清华大学 旋翼气动式精确转向陆空移动机器人装置
WO2019005937A1 (en) 2017-06-27 2019-01-03 Jetoptera, Inc. CONFIGURATION FOR A VERTICAL TAKE-OFF AND LANDING SYSTEM FOR AERIAL VEHICLES

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2752110A (en) * 1951-07-11 1956-06-26 Adolphe C Peterson Variable wing aircraft
US2858091A (en) * 1954-01-12 1958-10-28 Kapenkin Vladimir Retractable wing airplane
US4725021A (en) * 1986-10-17 1988-02-16 The United States Of America As Represented By The United States Department Of Energy Inflatable wing

Also Published As

Publication number Publication date
EP1755945A2 (en) 2007-02-28
IL178431A0 (en) 2007-05-15
WO2005099380A2 (en) 2005-10-27
CA2561366A1 (en) 2005-10-27
WO2005099380A3 (en) 2007-03-01

Similar Documents

Publication Publication Date Title
BRPI0509723A (pt) sistema de aumento de sustentação para uso em uma aeronave, e, célula de avião incluindo um sistema de aumento de sustentação
BR112018009344A8 (pt) veículo aéreo com componentes desdobráveis
BR112015013009A2 (pt) aeronave conversível dotada de dois rotores carenados na extremidade da asa e de uma ventoinha horizontal na fuselagem
BRPI0713167A2 (pt) compartimento de acomodação de trem de aterrisagem dianteiro para um avião, parte dianteira de aeronave e aeronave
ATE411940T1 (de) Langstreckenflugzeug
BRPI0512353A (pt) aeronave comercial com um andar principal e um andar inferior
DE602007011896D1 (de) Ausfallsichere steuerflächentropfenverbindung
WO2008154066A3 (en) Methods and apparatus for aircraft
BR112013002800A2 (pt) cone de cauda em forma de aerofólio
ATE492468T1 (de) Luftfahrzeug
BR112012024319A2 (pt) montagem de plataforma apainelada para veículo tranportador
BR112014009917A2 (pt) coluna de carenagem dirigível
BRPI0810474A2 (pt) Dispositivo de fixação de um elemento de sustentação na fuselagem de um avião
DE602008005032D1 (de) Luftfahrzeug mit Zugangsöffnung zur Beladung
BR112015014692A2 (pt) dispositivo auxiliar de aeronave voando em elevada altitude
GB2470524A (en) Leading edge element of aircraft, method for manufacturing one, wing and stabilizer
BR112012013575A2 (pt) trem de pouso de avião
ATE542739T1 (de) Flugzeugflügel
ATE331657T1 (de) Fluggerät mit auftrieb erzeugendem rumpf
WO2008054503A3 (en) Aircraft wings having hinged vanes and aircraft having said wings
DE602006000356D1 (de) Fluggerät mit vorwärts ausfahrbarer Vorderkante des Rumpfes und der Tragflügel
DE602004005602D1 (de) Starrer flügel mit variablem auftrieb aufgrund des ausklappens eines flexiblen flügels
GB2605197B (en) Aircraft wing with trailing edge panel
EA200600483A1 (ru) Крылатый летательный аппарат с флюгерным горизонтальным оперением
BR112015023282A2 (pt) Indexação modular para interior de aeronave

Legal Events

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

Free format text: REFERENTE AS 5A, 6A E 7A 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: REFERENTE AO DESPACHO 8.6 PUBLICADO NA RPI 2158 DE 15/05/2012.