BRPI1011310A2 - aeronave - Google Patents

aeronave

Info

Publication number
BRPI1011310A2
BRPI1011310A2 BRPI1011310A BRPI1011310A BRPI1011310A2 BR PI1011310 A2 BRPI1011310 A2 BR PI1011310A2 BR PI1011310 A BRPI1011310 A BR PI1011310A BR PI1011310 A BRPI1011310 A BR PI1011310A BR PI1011310 A2 BRPI1011310 A2 BR PI1011310A2
Authority
BR
Brazil
Prior art keywords
aircraft
Prior art date
Application number
BRPI1011310A
Other languages
English (en)
Inventor
Guillaume Gallant
Romain Delahaye
Original Assignee
Airbus Operations Sas
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 Sas filed Critical Airbus Operations Sas
Publication of BRPI1011310A2 publication Critical patent/BRPI1011310A2/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
    • B64C1/18—Floors
    • 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
    • B64C1/061—Frames
BRPI1011310A 2009-05-28 2010-05-28 aeronave BRPI1011310A2 (pt)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR0953514A FR2946008B1 (fr) 2009-05-28 2009-05-28 Aeronef comprenant des traverses de support de plancher
PCT/FR2010/051032 WO2010136734A1 (fr) 2009-05-28 2010-05-28 Aeronef comprenant des traverses de support de plancher et paliers comprenant un materiau souple et reliant la traverse au support

Publications (1)

Publication Number Publication Date
BRPI1011310A2 true BRPI1011310A2 (pt) 2016-03-15

Family

ID=41560402

Family Applications (1)

Application Number Title Priority Date Filing Date
BRPI1011310A BRPI1011310A2 (pt) 2009-05-28 2010-05-28 aeronave

Country Status (9)

Country Link
US (1) US8936215B2 (pt)
EP (1) EP2435300B1 (pt)
JP (1) JP5689459B2 (pt)
CN (1) CN102574573B (pt)
BR (1) BRPI1011310A2 (pt)
CA (1) CA2763531A1 (pt)
FR (1) FR2946008B1 (pt)
RU (1) RU2528074C2 (pt)
WO (1) WO2010136734A1 (pt)

Families Citing this family (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2946024B1 (fr) * 2009-05-27 2011-07-22 Airbus France Installation de realisation d'un troncon de fuselage d'aeronef.
EP2733059A1 (en) 2012-11-20 2014-05-21 Airbus Operations GmbH Aircraft structure arrangement
PL2905228T3 (pl) * 2014-02-06 2018-05-30 Airbus Helicopters Deutschland GmbH Płatowiec kadłubowy i zbiornik
FR3021624B1 (fr) * 2014-05-30 2017-12-22 Airbus Operations Sas Liaison coulissante entre la structure plancher et la structure de coque d'un aeronef.
US10676942B2 (en) * 2016-01-26 2020-06-09 The Boeing Company Scaffolding apparatus and related methods
WO2018102183A1 (en) * 2016-12-03 2018-06-07 Ge Aviation Systems Llc Spherical bearing system
US10589835B2 (en) 2017-03-29 2020-03-17 The Boeing Company Floor panel fastener assembly
US10800509B2 (en) 2017-05-15 2020-10-13 The Boeing Company Aircraft floor panel connection system
US10717515B2 (en) 2017-05-15 2020-07-21 The Boeing Company Offset flange floor panel connection system
US10836463B2 (en) * 2017-07-06 2020-11-17 The Boeing Company Aircraft floor panel floating connection system
FR3082823A1 (fr) * 2018-06-25 2019-12-27 Airbus Operations Module pour aeronef presentant une conception facilitant son assemblage dans un espace interieur defini par le fuselage de l'aeronef
US11203407B2 (en) * 2020-01-02 2021-12-21 The Boeing Company Floor grid for aircraft
FR3117996A1 (fr) * 2020-12-17 2022-06-24 Airbus Operations Partie d’aéronef comportant un dispositif de liaison entre deux structures
EP4197918A1 (fr) * 2021-12-16 2023-06-21 Airbus Operations (S.A.S.) Pièce de coin flexible destinée à contribuer à une liaison entre au moins trois parois d' au moins un caisson d' aéronef
FR3130745A1 (fr) * 2021-12-16 2023-06-23 Airbus Operations Partie d’aéronef comportant un plancher lié à un tronçon de fuselage par l’intermédiaire de bielles élastiques.
EP4303118A1 (de) * 2022-07-07 2024-01-10 Airbus Operations GmbH Flugzeugrumpfsektion für ein flugzeug und flugzeug damit

Family Cites Families (24)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2472724A (en) * 1944-06-26 1949-06-07 Republic Aviat Corp Seal
US3251489A (en) * 1963-02-11 1966-05-17 American Mach & Foundry Cargo handling apparatus
US3420470A (en) * 1966-11-18 1969-01-07 Trw Inc Band retainer for satellite separation system
US3632065A (en) * 1969-11-19 1972-01-04 Vlm Corp The Rotary wing aircraft
US3912206A (en) * 1974-03-01 1975-10-14 Mc Donnell Douglas Corp Load lift and skid pad assembly
SE440926B (sv) * 1980-10-15 1985-08-26 Scanding Byggkonsult Kopplingselement for fackverk innefattande skiv- eller skalformiga kroppar
DE3141869C2 (de) * 1981-10-22 1984-02-02 Messerschmitt-Bölkow-Blohm GmbH, 8000 München Fußbodenkonstruktion für den oberen Laderaum eines Luftfahrzeuges
EP0101235A3 (en) * 1982-08-13 1986-02-12 Avon Rubber Plc Resilient assemblies
DE3419967C2 (de) * 1984-05-29 1986-07-10 Boge Gmbh, 5208 Eitorf Elastisches Gelenk, Kupplung oder dergleichen
US5176339A (en) * 1991-09-30 1993-01-05 Lord Corporation Resilient pivot type aircraft mounting
AT404926B (de) * 1997-07-07 1999-03-25 Fischer Adv Components Gmbh Einrichtung zur lösbaren befestigung von abdeckplatten od. dgl.
US6158690A (en) * 1998-10-30 2000-12-12 Sikorsky Aircraft Corporation Cabin interior panel system for reducing noise transmission in an aircraft
GB0021719D0 (en) * 2000-09-05 2000-10-18 Meritor Heavy Vehicle Sys Ltd Pivot bearing
FR2872782B1 (fr) * 2004-07-08 2007-10-05 Airbus France Sas Plancher pour aeronef
FR2872781B1 (fr) * 2004-07-08 2007-10-05 Airbus France Sas Plancher pour aeronef
FR2872780B1 (fr) * 2004-07-08 2006-11-17 Airbus France Sas Plancher pour aeronef
DE102005045181A1 (de) * 2005-09-21 2007-04-05 Eads Deutschland Gmbh Fußbodenstruktur für Flugzeuge
FR2900125B1 (fr) * 2006-04-20 2009-01-16 Airbus France Sas Plancher d'aeronef, utilisation d'un tel plancher et troncon d'aeronef muni d'un tel plancher
DE102006026168A1 (de) * 2006-06-06 2008-01-31 Airbus Deutschland Gmbh Flugzeugrumpfstruktur und Verfahren zu deren Herstellung
US7775478B2 (en) * 2006-09-29 2010-08-17 The Boeing Company Floor beam assembly, system, and associated method
FR2915173B1 (fr) * 2007-04-17 2009-10-23 Airbus Sa Sa Dispositif de fixation d'un organe de sustentation au fuselage d'un avion.
DE102008007838B4 (de) * 2008-02-07 2013-07-18 Airbus Operations Gmbh Fußbodensystem für eine Rumpfzelle eines Flugzeugs
FR2947525B1 (fr) * 2009-07-02 2011-09-02 Airbus Operations Sas Plancher d'aeronef a encombrement optimise
FR2947524B1 (fr) * 2009-07-02 2011-12-30 Airbus Operations Sas Procede de fabrication d'un aeronef comprenant un plancher

Also Published As

Publication number Publication date
US20120061513A1 (en) 2012-03-15
FR2946008A1 (fr) 2010-12-03
CN102574573A (zh) 2012-07-11
JP5689459B2 (ja) 2015-03-25
JP2012528039A (ja) 2012-11-12
US8936215B2 (en) 2015-01-20
FR2946008B1 (fr) 2012-12-28
RU2528074C2 (ru) 2014-09-10
EP2435300A1 (fr) 2012-04-04
CN102574573B (zh) 2015-12-02
RU2011151480A (ru) 2013-07-10
WO2010136734A1 (fr) 2010-12-02
EP2435300B1 (fr) 2016-03-23
CA2763531A1 (fr) 2010-12-02

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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]
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 2465 DE 03-04-2018 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.