BRPI0821427A2 - Componente estrutural de fuselagem da asa para a ligação duas asas de sustentação e uma seção de fuselagem em um avião. - Google Patents

Componente estrutural de fuselagem da asa para a ligação duas asas de sustentação e uma seção de fuselagem em um avião.

Info

Publication number
BRPI0821427A2
BRPI0821427A2 BRPI0821427-1A BRPI0821427A BRPI0821427A2 BR PI0821427 A2 BRPI0821427 A2 BR PI0821427A2 BR PI0821427 A BRPI0821427 A BR PI0821427A BR PI0821427 A2 BRPI0821427 A2 BR PI0821427A2
Authority
BR
Brazil
Prior art keywords
fuselage
airplane
structural member
wing
lift wings
Prior art date
Application number
BRPI0821427-1A
Other languages
English (en)
Inventor
Claus-Peter Gross
Original Assignee
Airbus Operations Gmbh
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 Airbus Operations Gmbh filed Critical Airbus Operations Gmbh
Publication of BRPI0821427A2 publication Critical patent/BRPI0821427A2/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
    • B64C1/12—Construction or attachment of skin panels
    • 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
    • B64C1/26—Attaching the wing or tail units or stabilising surfaces

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Toys (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Connection Of Plates (AREA)
  • Joining Of Building Structures In Genera (AREA)
  • Tires In General (AREA)
BRPI0821427-1A 2007-12-30 2008-12-30 Componente estrutural de fuselagem da asa para a ligação duas asas de sustentação e uma seção de fuselagem em um avião. BRPI0821427A2 (pt)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US1764907P 2007-12-30 2007-12-30
DE102007063159A DE102007063159A1 (de) 2007-12-30 2007-12-30 Flügel-Rumpf-Strukturbauteil zur Verbindung von zwei Tragflügeln und einer Rumpfsektion an einem Flugzeug
PCT/EP2008/011152 WO2009083262A2 (de) 2007-12-30 2008-12-30 Flügel-rumpf-strukturbauteil zur verbindung von zwei tragflügeln und einer rumpfsektion an einem flugzeug

Publications (1)

Publication Number Publication Date
BRPI0821427A2 true BRPI0821427A2 (pt) 2015-06-16

Family

ID=40824765

Family Applications (1)

Application Number Title Priority Date Filing Date
BRPI0821427-1A BRPI0821427A2 (pt) 2007-12-30 2008-12-30 Componente estrutural de fuselagem da asa para a ligação duas asas de sustentação e uma seção de fuselagem em um avião.

Country Status (8)

Country Link
US (1) US8356773B2 (pt)
EP (1) EP2229317B1 (pt)
CN (1) CN101909989B (pt)
BR (1) BRPI0821427A2 (pt)
CA (1) CA2711105A1 (pt)
DE (1) DE102007063159A1 (pt)
RU (1) RU2482997C2 (pt)
WO (1) WO2009083262A2 (pt)

Families Citing this family (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102006058491B4 (de) * 2006-10-02 2018-03-15 Johnson Controls Interiors Gmbh & Co. Kg Mehrteiliges Fahrzeugausstattungsteil und Verbindungsverfahren
CN102730182B (zh) * 2012-06-20 2014-10-01 中国航天时代电子公司 一种无人机机翼与机身连接装置
US8985514B2 (en) * 2012-06-20 2015-03-24 The Boeing Company Composite structural panels and aircraft fuselages
EP2783838B1 (en) * 2013-03-27 2015-11-18 Airbus Operations GmbH Composite reinforcement component, structural element, aircraft or spacecraft and method for producing a composite reinforcement component
US9441652B2 (en) 2013-05-31 2016-09-13 The Boeing Company Joint assembly and method of assembling the same
CN105253289B (zh) * 2015-11-10 2017-10-03 康福斯（苏州）航空工业有限公司 飞机翼身连接结构
CN110582446B (zh) * 2017-05-01 2023-03-31 庞巴迪公司 具有压力翼刀的飞机机翼单元
US11661170B2 (en) 2017-05-01 2023-05-30 Bombardier Inc. Aircraft wing unit with upper wing skin defining pressure floor
US11149770B2 (en) * 2018-06-11 2021-10-19 Rockwell Collins, Inc. Load-transferring connection between structurally loaded components
US11174042B2 (en) 2018-10-09 2021-11-16 The Boeing Company Wing join system and method for a wing assembly
CA3135682A1 (fr) * 2019-04-01 2020-10-08 Olivier Lamaille Appareil pour la navigation aerienne et ses dispositifs
CN115056962B (zh) * 2022-06-10 2023-04-18 白鲸航线(北京)科技有限公司 一种上单翼飞机翼身连接结构

Family Cites Families (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3735524A (en) * 1972-07-19 1973-05-29 Mattel Inc Wing assembly for toy airplanes
SU1037539A1 (ru) * 1981-12-11 1996-09-20 А.С. Прытков Неразъемный технологический стык центроплана самолета с крылом
US4904109A (en) * 1987-12-11 1990-02-27 Grumman Aerospace Corporation Interlocking structural members employing transverse locking wedges
US4875795A (en) * 1987-12-11 1989-10-24 Grumman Aerospace Corporation Structural connector utilizing tabbed support substructure
JPH06255587A (ja) * 1993-03-09 1994-09-13 Honda Motor Co Ltd 航空機
DE19529706C2 (de) * 1995-08-11 2001-08-02 Deutsch Zentr Luft & Raumfahrt Flächentragwerk, insbesondere für ein Luftfahrzeug
RU2154003C2 (ru) * 1998-05-18 2000-08-10 Самарский государственный аэрокосмический университет им.С.П.Королева Соединение крыла и фюзеляжа
DE10007995C2 (de) * 2000-02-22 2002-03-07 Airbus Gmbh Strukturbauteil, insbesondere für ein Flugzeug und Verfahren zur Herstellung eines Strukturbauteils
US6726149B2 (en) * 2002-05-31 2004-04-27 The Boeing Company Derivative aircraft and methods for their manufacture
CA2444869A1 (en) * 2002-10-21 2004-04-21 The Boeing Company Method and apparatus for actuating movable components, including canards, over multiple ranges
FR2867151B1 (fr) * 2004-03-04 2007-05-25 Airbus France Longeron de fuselage pour aeronef et caisson central equipe d'un tel longeron
US7097133B2 (en) * 2004-08-19 2006-08-29 Raytheon Company Articulated folding wing structure and method
GB2435547B (en) * 2006-02-23 2009-09-23 Wen-Chao Shen Satellite dish antenna assembly
GB2435457B (en) 2006-02-28 2011-03-09 Hal Errikos Calamvokis Aircraft wings and their assembly
FR2901240B1 (fr) * 2006-05-17 2009-01-09 Airbus France Sas Poutre interne composite pour renforcer la structure d'un aeronef
US7735779B2 (en) * 2006-11-02 2010-06-15 The Boeing Company Optimized fuselage structure
US7887009B2 (en) * 2007-12-05 2011-02-15 The Boeing Company Methods and systems for attaching aircraft wings to fuselages

Also Published As

Publication number Publication date
EP2229317A2 (de) 2010-09-22
CN101909989A (zh) 2010-12-08
EP2229317B1 (de) 2012-07-04
WO2009083262A2 (de) 2009-07-09
RU2010131843A (ru) 2012-02-10
CN101909989B (zh) 2013-04-10
DE102007063159A1 (de) 2010-07-08
US20100301165A1 (en) 2010-12-02
US8356773B2 (en) 2013-01-22
CA2711105A1 (en) 2009-07-09
WO2009083262A3 (de) 2009-10-01
RU2482997C2 (ru) 2013-05-27

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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 4A, 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: EM VIRTUDE DO ARQUIVAMENTO PUBLICADO NA RPI 2343 DE 01-12-2015 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.