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
EP2599711B1 (en) * 2011-12-01 2017-07-26 Airbus Operations S.L. Highly loaded frame of an aircraft fuselage with a lattice structured web
ES2692969T3 (es) 2013-11-21 2018-12-05 Airbus Operations Gmbh Componente de esquina de puerta de pasajero y procedimiento de fabricación para componente de esquina de puerta de pasajero de aeronave o nave espacial
ES2902069T3 (es) * 2014-10-16 2022-03-24 Airbus Operations Gmbh Deflector para aeronave y método asociado
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
JP6858329B2 (ja) * 2017-03-30 2021-04-14 サフラン キャビン インコーポレイティド 側壁パネル組立体
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
FR2927686A1 (fr) 2009-08-21
EP2242683A1 (fr) 2010-10-27
FR2927686B1 (fr) 2010-10-08
EP2242683B1 (fr) 2016-04-20
US20100320331A1 (en) 2010-12-23
CA2714433A1 (fr) 2009-09-17
ES2583555T3 (es) 2016-09-21
CA2714433C (fr) 2016-09-27
WO2009112735A1 (fr) 2009-09-17

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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.