BRPI0908084A2 - Painel compósito monolítico autoreforçado e articulado, principalmente para uma parte móvel de uma aeronave - Google Patents

Painel compósito monolítico autoreforçado e articulado, principalmente para uma parte móvel de uma aeronave

Info

Publication number
BRPI0908084A2
BRPI0908084A2 BRPI0908084-8A BRPI0908084A BRPI0908084A2 BR PI0908084 A2 BRPI0908084 A2 BR PI0908084A2 BR PI0908084 A BRPI0908084 A BR PI0908084A BR PI0908084 A2 BRPI0908084 A2 BR PI0908084A2
Authority
BR
Brazil
Prior art keywords
aircraft
articulated
reinforcing
self
mainly
Prior art date
Application number
BRPI0908084-8A
Other languages
English (en)
Inventor
Philippe Valee
Original Assignee
Socata
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 Socata filed Critical Socata
Publication of BRPI0908084A2 publication Critical patent/BRPI0908084A2/pt

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C1/06—Frames; Stringers; Longerons ; Fuselage sections
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C25/00—Alighting gear
    • B64C25/02—Undercarriages
    • B64C25/08—Undercarriages non-fixed, e.g. jettisonable
    • B64C25/10—Undercarriages non-fixed, e.g. jettisonable retractable, foldable, or the like
    • B64C25/16—Fairings movable in conjunction with undercarriage elements
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C9/00—Adjustable control surfaces or members, e.g. rudders
    • 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
    • Y02T50/40—Weight reduction
    • 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
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00—Stock material or miscellaneous articles
    • Y10T428/23—Sheet including cover or casing

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Moulding By Coating Moulds (AREA)
  • Body Structure For Vehicles (AREA)
  • Superstructure Of Vehicle (AREA)
  • Securing Of Glass Panes Or The Like (AREA)
BRPI0908084-8A 2008-02-20 2009-02-19 Painel compósito monolítico autoreforçado e articulado, principalmente para uma parte móvel de uma aeronave BRPI0908084A2 (pt)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR0851087A FR2927686B1 (fr) 2008-02-20 2008-02-20 Panneau composite monolithique auto-raidi et pivotant, notamment pour une partie mobile d'aeronef.
PCT/FR2009/050270 WO2009112735A1 (fr) 2008-02-20 2009-02-19 Panneau composite monolithique auto-raidi et pivotant, notamment pour une partie mobile d'aeronef

Publications (1)

Publication Number Publication Date
BRPI0908084A2 true BRPI0908084A2 (pt) 2015-08-25

Family

ID=39855738

Family Applications (1)

Application Number Title Priority Date Filing Date
BRPI0908084-8A BRPI0908084A2 (pt) 2008-02-20 2009-02-19 Painel compósito monolítico autoreforçado e articulado, principalmente para uma parte móvel de uma aeronave

Country Status (8)

Country Link
US (1) US20100320331A1 (pt)
EP (1) EP2242683B1 (pt)
JP (1) JP2011512298A (pt)
BR (1) BRPI0908084A2 (pt)
CA (1) CA2714433C (pt)
ES (1) ES2583555T3 (pt)
FR (1) FR2927686B1 (pt)
WO (1) WO2009112735A1 (pt)

Families Citing this family (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP5134258B2 (ja) 2007-02-09 2013-01-30 ユニ・チャーム株式会社 動物用トイレ砂
US8703268B2 (en) * 2009-11-13 2014-04-22 The Boeing Company Morphing panel structure
CN102501966B (zh) * 2011-11-07 2016-04-13 中国商用飞机有限责任公司 一种用于飞机舱门的扰流片及装有该扰流片的飞机舱门
ES2645628T3 (es) 2011-12-01 2017-12-07 Airbus Operations S.L. Cuaderna altamente cargada de un fuselaje de aeronave con un alma con estructura de celosía
EP2876044B1 (en) * 2013-11-21 2018-09-12 Airbus Operations GmbH Passenger door corner component and manufacturing method for passenger door corner component of aircraft or spacecraft
EP3009344B1 (en) * 2014-10-16 2019-05-29 Airbus Operations GmbH Panel structure and associated method
US10724258B2 (en) * 2015-05-05 2020-07-28 West Virginia University Durable, fire resistant, energy absorbing and cost-effective strengthening systems for structural joints and members
EP3173331B1 (en) 2015-11-30 2019-04-24 Airbus Operations GmbH Cover panel for a structural component
US20180099736A1 (en) * 2016-10-12 2018-04-12 The Boeing Company Aircraft wings, aircraft, and related methods
WO2018183750A1 (en) * 2017-03-30 2018-10-04 C&D Zodiac, Inc. Sidewall panel assembly
CN108194817A (zh) * 2018-01-18 2018-06-22 安徽道智能制造技术有限公司 一种汽车专用宽板线框型面板结构
CN111140763A (zh) * 2018-11-02 2020-05-12 彭志军 一种带加强筋与锁扣结构的复合型板材
FR3107254A1 (fr) * 2020-02-18 2021-08-20 Airbus Operations (S.A.S.) Procédé de fabrication d’une structure aérodynamique mobile d’aéronef et structure aérodynamique mobile d’aéronef ainsi obtenue
WO2025222269A1 (en) * 2024-04-23 2025-10-30 Safran Landing Systems Canada Inc. Articulated landing gear door with drive linkage

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2451131A (en) * 1940-09-06 1948-10-12 Vidal Corp Method of making reinforced structures
US3300354A (en) * 1962-04-18 1967-01-24 Whittaker Corp Method of making a filament wound sandwich core
US5262220A (en) * 1991-06-18 1993-11-16 Chem-Tronics, Inc. High strength structure assembly and method of making the same
ATE284346T1 (de) * 2001-01-26 2004-12-15 Fischer Adv Components Gmbh Einrichtung zum verbinden beweglicher teile mit strukturbauteilen von flugzeugen od. dgl.
DE102005057907B4 (de) * 2005-12-02 2012-03-22 Eurocopter Deutschland Gmbh Luftfahrzeug-Druckkabinentür aus Faserverbundwerkstoff

Also Published As

Publication number Publication date
JP2011512298A (ja) 2011-04-21
WO2009112735A1 (fr) 2009-09-17
CA2714433C (fr) 2016-09-27
EP2242683B1 (fr) 2016-04-20
US20100320331A1 (en) 2010-12-23
EP2242683A1 (fr) 2010-10-27
CA2714433A1 (fr) 2009-09-17
ES2583555T3 (es) 2016-09-21
FR2927686A1 (fr) 2009-08-21
FR2927686B1 (fr) 2010-10-08

Similar Documents

Publication Publication Date Title
BRPI0716761A2 (pt) painel de revestimento para uma fuselagem de aeronave
BRPI0820878A2 (pt) fuselagem com atenuação acústica para aeronave
BR112012013602A2 (pt) conjunto de asinha para aeronave.
BRPI0816483A2 (pt) Quadro de estrutura material compósito, notadamente para fuselagem de aeronave,e, fuselagem de aeronave
BRPI0909003A2 (pt) junta compósita para aeronave
BRPI0907617A2 (pt) Peça de compósito de fibras para uma aeronave ou espaçonave
EP2240364B8 (de) Fussbodensystem für eine rumpfzelle eines flugzeugs
BRPI0914324A2 (pt) dispositivo de carenagem de nacela para de uma unidade de potência propulsora, e, unidade de potência propulsora
BRPI0920950A2 (pt) aeronave e método de controlar a direção a direção de vôo de uma aeronave
BRPI0812818A2 (pt) Turbo-reator para aeronave
EP2160321A4 (en) Engine anticipation for rotary wing aircraft
BRPI0810296A2 (pt) estrutura de corda e método para formar uma estrutura de corda
BRPI0814157A2 (pt) Composição de catalisador e processos para a preparação e uma composição de catalisador e para desalquilação de etil-benzeno
BR112012005210A2 (pt) composição polimerizável e sistema para cobertura de uma superfície de unha
BRPI0917714A2 (pt) método para preparar uma microesfera de liberação prolongada, e, microesfera de liberação prolongada
BRPI0908079A2 (pt) Conjunto motor para aeronave, e, aeronave
BRPI0924616A2 (pt) junta compósita para estrutura de avião
BRPI0814543A2 (pt) Cabine de pilotagem aperfeiçoada de avião
BRPI0907771A2 (pt) Conjunto motor para aeronave, e, aeronave
BRPI0911572A2 (pt) unidade de propulsão para uma aeronave e estrutura de entrada de ar para a referida unidade de propulsão
BRPI0810535A2 (pt) Nacela para turbojato e avião.
BRPI0904623A2 (pt) Estrutura de isolamento para isolar termicamente e acusticamente uma eronave
BRPI0910895A2 (pt) rebite maciço para a junção de componente de construção compostos
BRPI0910290A2 (pt) estrutura de fuselagem para aeronave
GB0810500D0 (en) Aircraft wing

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 E 6A 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 2344 DE 08-12-2015 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.