BRPI0821753A2 - Superfície de controle de aeronave - Google Patents

Superfície de controle de aeronave

Info

Publication number
BRPI0821753A2
BRPI0821753A2 BRPI0821753-0A BRPI0821753A BRPI0821753A2 BR PI0821753 A2 BRPI0821753 A2 BR PI0821753A2 BR PI0821753 A BRPI0821753 A BR PI0821753A BR PI0821753 A2 BRPI0821753 A2 BR PI0821753A2
Authority
BR
Brazil
Prior art keywords
control surface
aircraft control
aircraft
control
Prior art date
Application number
BRPI0821753-0A
Other languages
English (en)
Inventor
Afonso González Gozalbo
Jorge Pablo Verde Preckler
José Alberto Cabello Moreno
Raúl Carlos Llamas Sandin
Original Assignee
Airbus Operations Sl
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
Family has litigation
First worldwide family litigation filed litigation Critical https://patents.darts-ip.com/?family=40547516&utm_source=google_patent&utm_medium=platform_link&utm_campaign=public_patent_search&patent=BRPI0821753(A2) "Global patent litigation dataset” by Darts-ip is licensed under a Creative Commons Attribution 4.0 International License.
Application filed by Airbus Operations Sl filed Critical Airbus Operations Sl
Publication of BRPI0821753A2 publication Critical patent/BRPI0821753A2/pt
Publication of BRPI0821753B1 publication Critical patent/BRPI0821753B1/pt

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C9/00—Adjustable control surfaces or members, e.g. rudders
    • B64C9/02—Mounting or supporting thereof
    • 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
    • Y02T50/30—Wing lift efficiency
    • 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
    • Y02T50/40—Weight reduction

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Transmission Devices (AREA)
BRPI0821753-0 2007-12-21 2008-12-19 superfície de controle para uma superfície de sustentação aerodinâmica de aeronave BRPI0821753B1 (pt)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
ES200703402A ES2345584B1 (es) 2007-12-21 2007-12-21 Superficie de control de aeronave.
PCT/EP2008/067980 WO2009080736A1 (en) 2007-12-21 2008-12-19 Aircraft control surface

Publications (2)

Publication Number Publication Date
BRPI0821753A2 true BRPI0821753A2 (pt) 2015-06-16
BRPI0821753B1 BRPI0821753B1 (pt) 2019-12-03

Family

ID=40547516

Family Applications (1)

Application Number Title Priority Date Filing Date
BRPI0821753-0 BRPI0821753B1 (pt) 2007-12-21 2008-12-19 superfície de controle para uma superfície de sustentação aerodinâmica de aeronave

Country Status (7)

Country Link
US (1) US8038093B2 (pt)
EP (1) EP2234877B1 (pt)
BR (1) BRPI0821753B1 (pt)
CA (1) CA2710119C (pt)
ES (1) ES2345584B1 (pt)
RU (1) RU2492109C2 (pt)
WO (1) WO2009080736A1 (pt)

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US7992825B2 (en) * 2008-07-23 2011-08-09 Airbus Espana, S.L. Control surface of aircraft
FR2945790B1 (fr) * 2009-05-20 2011-07-22 Airbus France Procede pour l'amelioration de l'efficacite aerodynamique de l'empennage vertical d'un aeronef.
US9090326B2 (en) * 2010-10-13 2015-07-28 The Boeing Company Active flow control on a vertical stabilizer and rudder
DE102010051216A1 (de) * 2010-11-12 2012-05-16 Airbus Operations Gmbh Seitenrudersystem an einem Flugzeug
FR2973774B1 (fr) * 2011-04-06 2015-05-08 Airbus Operations Sas Procede d'amelioration de l'efficacite aerodynamique d'un empennage vertical d'aeronef.
EP2736804B1 (en) 2011-07-26 2015-09-02 Learjet Inc. Rudder bias gain changer
WO2013070296A2 (en) * 2011-08-19 2013-05-16 Aerovironment, Inc. Aircraft system for reduced observer visibility
DE102012006187B4 (de) * 2012-03-27 2020-03-12 Airbus Operations Gmbh Klappenanordnung und Flugzeug mit mindestens einer Klappenanordnung
UA79830U (ru) * 2013-03-12 2013-04-25 Юрий Григорьевич Сидоренко Привод управления подвижной аэродинамической поверхностью крыла самолета
US9278752B2 (en) 2014-03-17 2016-03-08 Lockheed Martin Corporation Apparatus and system for preventing wear to a component
US9643716B2 (en) * 2014-04-01 2017-05-09 The Boeing Company Air vehicle, actuator assembly and associated method of manufacture
RU2593178C1 (ru) * 2015-06-05 2016-07-27 Федеральное государственное унитарное предприятие "Центральный аэрогидродинамический институт имени профессора Н.Е. Жуковского" (ФГУП "ЦАГИ") Аэродинамический руль
US20170106970A1 (en) * 2015-10-15 2017-04-20 The Boeing Company Composite failsafe torque tube
EP3444483B1 (en) 2017-08-17 2020-12-16 Goodrich Actuation Systems Limited Multi-cylinder hydraulic actuator system
CN107878764B (zh) * 2017-11-29 2020-12-29 中国直升机设计研究所 一种整流罩防火墙排气管整体滑动结构
US10618627B2 (en) * 2018-02-13 2020-04-14 Bell Helicopter Textron Inc. Rudder twist lock method and apparatus
US10647407B2 (en) * 2018-03-30 2020-05-12 The Boeing Company Wing flap with torque member and method for forming thereof
US10597141B2 (en) * 2018-03-30 2020-03-24 The Boeing Company Wing flap with torque member and method for forming thereof
GB201905857D0 (en) * 2019-04-26 2019-06-12 Airbus Operations Gmbh Aerostructure assembly
RU2746534C1 (ru) * 2020-05-27 2021-04-15 Федеральное государственное унитарное предприятие "Центральный аэрогидродинамический институт имени профессора Н.Е. Жуковского" (ФГУП "ЦАГИ") Руль аэродинамической поверхности летательного аппарата
RU2749173C1 (ru) * 2020-10-13 2021-06-07 Федеральное государственное унитарное предприятие "Центральный аэрогидродинамический институт имени профессора Н.Е. Жуковского" (ФГУП "ЦАГИ") Руль аэродинамической поверхности летательного аппарата
US11945585B2 (en) * 2022-02-15 2024-04-02 Lockheed Martin Corporation Control surface support for an aircraft
FR3134797A1 (fr) * 2022-04-26 2023-10-27 Airbus (S.A.S.) Aéronef comprenant au moins un profilé flexible en matériau composite formant au moins un élément parmi un arbre d’accouplement d’une surface mobile et une surface mobile

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Publication number Priority date Publication date Assignee Title
GB462904A (en) * 1935-09-14 1937-03-15 Richard Vogt Improvements in spars for the wings of aircraft
US2511504A (en) * 1942-07-02 1950-06-13 Lockheed Aircraft Corp Airplane wing and slotted flap
GB560480A (en) * 1942-11-11 1944-04-05 Blackburn Aircraft Ltd Improvements in and relating to the construction of aircraft control surfaces
DE897953C (de) * 1945-02-15 1953-11-26 Kurt Schaefer Traeger, insbesondere fuer Kraftfahrzeuge
US2595363A (en) * 1948-06-30 1952-05-06 United Aircraft Corp Hinged fins for providing directional control and stability in tailless airplanes
US3706432A (en) * 1971-09-14 1972-12-19 United Aircraft Corp Redundant stabilizer support
US3958779A (en) * 1975-05-27 1976-05-25 Fairchild Industries Inc. Aircraft control system with a jam isolating coupling
US4213587A (en) * 1978-12-04 1980-07-22 The Boeing Company Hinge arrangement for control surfaces
US4542866A (en) * 1983-09-30 1985-09-24 The Boeing Company Aircraft with directional controlling canards
RU2026240C1 (ru) * 1988-01-20 1995-01-09 Экспериментальный машиностроительный завод им.В.М.Мясищева Способ регулирования распределения аэродинамических нагрузок на крыле летательного аппарата и крыло летательного аппарата (варианты)
RU2022878C1 (ru) * 1988-12-29 1994-11-15 Летно-исследовательский институт им.М.М.Громова Устройство для управления аэродинамической поверхностью летательного аппарата
US5884872A (en) * 1993-05-26 1999-03-23 The United States Of America As Represented By The Secretary Of The Navy Oscillating flap lift enhancement device
DE19630681A1 (de) * 1996-07-30 1998-02-05 Gerhard Fink Flugzeugruder
US6089503A (en) * 1999-01-15 2000-07-18 Northrop Grumman Corp Selectively rotatable and torsionally flexible aerodynamic control apparatus

Also Published As

Publication number Publication date
RU2492109C2 (ru) 2013-09-10
ES2345584A1 (es) 2010-09-27
WO2009080736A1 (en) 2009-07-02
US20090159755A1 (en) 2009-06-25
ES2345584B1 (es) 2011-07-18
US8038093B2 (en) 2011-10-18
EP2234877B1 (en) 2012-09-26
RU2010130317A (ru) 2012-01-27
EP2234877A1 (en) 2010-10-06
CA2710119A1 (en) 2009-07-02
CA2710119C (en) 2016-07-12
BRPI0821753B1 (pt) 2019-12-03

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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]
B06T Formal requirements before examination [chapter 6.20 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: 10 (DEZ) ANOS CONTADOS A PARTIR DE 03/12/2019, OBSERVADAS AS CONDICOES LEGAIS. (CO) 10 (DEZ) ANOS CONTADOS A PARTIR DE 03/12/2019, OBSERVADAS AS CONDICOES LEGAIS