BRPI1009128A2 - estrutura de célula de fuselagem para uma aeronave de construção híbrida - Google Patents

estrutura de célula de fuselagem para uma aeronave de construção híbrida

Info

Publication number: BRPI1009128A2
Authority: BR; Brazil
Prior art keywords: cell structure; hybrid construction; fuselage cell; construction aircraft; aircraft
Prior art date: 2009-03-17

Application number

BRPI1009128A

Other languages

English (en)

Inventor

hartwig Arne

Prowe Jens-Ulrich

Jörg Weber Markus

Müller Markus

Heltsch Norbert

Jörn Paul

Dolzinski Wolf-Dietrich

Original Assignee

Airbus Operation 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.)

2009-03-17

Filing date

2010-03-16

Publication date

2017-05-30

2010-03-16 Application filed by Airbus Operation GmbH filed Critical Airbus Operation GmbH

2017-05-30 Publication of BRPI1009128A2 publication Critical patent/BRPI1009128A2/pt

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
- B64C1/06—Frames; Stringers; Longerons ; Fuselage sections
- B64C1/064—Stringers; Longerons
- 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
- B64C1/065—Spars
- 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
- B64C2001/0054—Fuselage structures substantially made from particular materials
- B64C2001/0072—Fuselage structures substantially made from particular materials from composite materials
- 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)
Mechanical Engineering (AREA)
Aviation & Aerospace Engineering (AREA)
Body Structure For Vehicles (AREA)
Laminated Bodies (AREA)
Tents Or Canopies (AREA)

BRPI1009128A 2009-03-17 2010-03-16 estrutura de célula de fuselagem para uma aeronave de construção híbrida BRPI1009128A2 (pt)

Applications Claiming Priority (3)

Application Number	Priority Date	Filing Date	Title
US16087209P	2009-03-17	2009-03-17
DE102009013585A DE102009013585B4 (de)	2009-03-17	2009-03-17	Rumpfzellenstruktur für ein Flugzeug in Hybridbauweise
PCT/EP2010/053331 WO2010106040A2 (de)	2009-03-17	2010-03-16	Rumpfzellenstruktur für ein flugzeug in hybridbauweise

Publications (1)

Publication Number	Publication Date
BRPI1009128A2 true BRPI1009128A2 (pt)	2017-05-30

Family

ID=42628787

Family Applications (1)

Application Number	Title	Priority Date	Filing Date
BRPI1009128A BRPI1009128A2 (pt)	2009-03-17	2010-03-16	estrutura de célula de fuselagem para uma aeronave de construção híbrida

Country Status (9)

Country	Link
US (1)	US9586668B2 (pt)
EP (1)	EP2408665A2 (pt)
JP (1)	JP2012520787A (pt)
CN (1)	CN102427998B (pt)
BR (1)	BRPI1009128A2 (pt)
CA (1)	CA2755840A1 (pt)
DE (1)	DE102009013585B4 (pt)
RU (1)	RU2482995C1 (pt)
WO (1)	WO2010106040A2 (pt)

Families Citing this family (14)

* Cited by examiner, † Cited by third party
Publication number	Priority date	Publication date	Assignee	Title
DE102009013511B4 (de) *	2009-03-17	2015-05-21	Airbus Operations Gmbh	Fensterelement für ein doppelschaliges Hautfeld einer Flugzeugrumpfzelle
DE102009013585B4 (de)	2009-03-17	2012-01-26	Airbus Operations Gmbh	Rumpfzellenstruktur für ein Flugzeug in Hybridbauweise
ES2382765B1 (es) *	2009-06-29	2013-05-03	Airbus Operations, S.L.	Diseño de cuadernas de aeronave
GB201012552D0 (en)	2010-07-23	2010-11-17	Bae Systems Plc	Aircraft thermal insulation
GB201016279D0 (en) *	2010-09-28	2010-11-10	Airbus Operations Ltd	Stiffener run-out
US8985514B2 (en) *	2012-06-20	2015-03-24	The Boeing Company	Composite structural panels and aircraft fuselages
US8939406B2 (en) *	2012-07-02	2015-01-27	The Boeing Company	Joining composite fuselage sections along window belts
DE102012110862B4 (de)	2012-11-12	2016-03-31	Airbus Defence and Space GmbH	Flächenbauteil für ein Luftfahrzeug und Herstellungsverfahren hierfür
EP2818415B1 (en) *	2013-06-27	2019-01-02	Airbus Operations GmbH	Panel member for an airframe
EP2842865B1 (en) *	2013-08-28	2019-12-18	Airbus Operations GmbH	Window panel for an airframe and method of producing same
CN104890855A (zh) *	2015-04-24	2015-09-09	江西洪都航空工业集团有限责任公司	一种新型框板型材搭接结构
DE102016210079A1 (de) *	2016-06-08	2017-12-14	Airbus Operations Gmbh	Verfahren zum Herstellen eines Rumpfabschnitts
US10479471B2 (en) *	2016-11-30	2019-11-19	The Boeing Company	Fuselage skin panel connection system and method for connecting skin panels
ES2878279T3 (es)	2018-07-31	2021-11-18	Airbus Operations Sl	Cuaderna para cascos de fuselaje de una aeronave y casco de fuselaje

Family Cites Families (22)

* Cited by examiner, † Cited by third party
Publication number	Priority date	Publication date	Assignee	Title
US2334844A (en) *	1941-10-18	1943-11-23	Cessna Aircraft Co	Attachment for aircraft structures
US3145000A (en) *	1963-05-29	1964-08-18	William L Mackie	Light weight-high thermal resistant airfoil
US3655818A (en) *	1968-10-18	1972-04-11	Minnesota Mining & Mfg	Particulate adhesive containing polyepoxides carboxylated butadiene-acrylonitrile copolymer and a urea derivative as a curing agent
SU466724A1 (ru)	1973-06-22	1991-10-30	Предприятие П/Я В-2739	Многослойна сотова панель
US4344995A (en) *	1980-09-15	1982-08-17	The Boeing Company	Hybrid composite structures
US4606961A (en) *	1984-10-09	1986-08-19	The Boeing Company	Discretely stiffened composite panel
US5429326A (en) *	1992-07-09	1995-07-04	Structural Laminates Company	Spliced laminate for aircraft fuselage
DE19804718C2 (de)	1998-02-06	2001-09-13	Eurocopter Deutschland	Schall absorbierende Sandwichwand
FR2787509B1 (fr) *	1998-12-21	2001-03-30	Aerospatiale	Structure d'entree d'air pour moteur d'aeronef
JP4425422B2 (ja) *	2000-04-14	2010-03-03	本田技研工業株式会社	複合材製構造体の製造方法、及びそれにより製造される複合材製構造体
US7197852B2 (en) *	2002-09-20	2007-04-03	The Boeing Company	Internally stiffened composite panels and methods for their manufacture
US7325771B2 (en)	2004-09-23	2008-02-05	The Boeing Company	Splice joints for composite aircraft fuselages and other structures
US7182291B2 (en)	2005-03-23	2007-02-27	The Boeing Company	Integrated aircraft structural floor
DE102006002248B4 (de) *	2006-01-17	2008-01-03	Airbus Deutschland Gmbh	Strukturgebende Konstruktion für einen Flugzeugrumpf
US7628358B2 (en)	2006-10-26	2009-12-08	The Boeing Company	Wing panel structure
DE102007003275B4 (de)	2007-01-23	2013-11-28	Airbus Operations Gmbh	Schalenelement als Teil eines Flugzeugrumpfes
DE102007008988A1 (de)	2007-02-23	2008-08-28	Airbus Deutschland Gmbh	Rumpf eines Luft-oder Raumfahrzeugs und ein entsprechendes Luft-oder Raumfahrzeug
US7823833B2 (en) *	2007-03-05	2010-11-02	The Boeing Company	Window installation method and apparatus
DE102007029500B4 (de)	2007-06-25	2013-02-14	Airbus Operations Gmbh	Verfahren zum Koppeln von Versteifungsprofilelementen sowie Strukturbauteil
US8016237B2 (en) *	2007-12-12	2011-09-13	The Boeing Company	Methods and apparatus for an integrated aerodynamic panel
US7967250B2 (en) *	2008-05-12	2011-06-28	EMBRAER—Empresa Brasileira de Aeronáutica	Hybrid aircraft fuselage structural components and methods of making same
DE102009013585B4 (de)	2009-03-17	2012-01-26	Airbus Operations Gmbh	Rumpfzellenstruktur für ein Flugzeug in Hybridbauweise

2009
- 2009-03-17 DE DE102009013585A patent/DE102009013585B4/de not_active Expired - Fee Related
2010
- 2010-03-16 CA CA2755840A patent/CA2755840A1/en not_active Abandoned
- 2010-03-16 WO PCT/EP2010/053331 patent/WO2010106040A2/de not_active Ceased
- 2010-03-16 EP EP10713432A patent/EP2408665A2/de not_active Withdrawn
- 2010-03-16 US US13/257,367 patent/US9586668B2/en not_active Expired - Fee Related
- 2010-03-16 JP JP2012500215A patent/JP2012520787A/ja active Pending
- 2010-03-16 BR BRPI1009128A patent/BRPI1009128A2/pt not_active IP Right Cessation
- 2010-03-16 CN CN201080021424.6A patent/CN102427998B/zh not_active Expired - Fee Related
- 2010-03-16 RU RU2011141820/11A patent/RU2482995C1/ru not_active IP Right Cessation

Also Published As

Publication number	Publication date
DE102009013585B4 (de)	2012-01-26
US20120056037A1 (en)	2012-03-08
WO2010106040A2 (de)	2010-09-23
EP2408665A2 (de)	2012-01-25
WO2010106040A3 (de)	2011-03-31
RU2011141820A (ru)	2013-04-27
CN102427998B (zh)	2014-10-15
CN102427998A (zh)	2012-04-25
RU2482995C1 (ru)	2013-05-27
CA2755840A1 (en)	2010-09-23
DE102009013585A1 (de)	2010-09-23
US9586668B2 (en)	2017-03-07
JP2012520787A (ja)	2012-09-10

Publication	Publication Date	Title
BRPI1009128A2 (pt)	2017-05-30	estrutura de célula de fuselagem para uma aeronave de construção híbrida
ZA201204833B (en)	2013-03-27	Aircraft wingtip arrangement
GB201013261D0 (en)	2010-09-22	Propellers for aircraft
GB2494089B (en)	2017-04-19	Aircraft fuelling arrangement
ES2626492T8 (es)	2018-07-13	Procedimiento para la expansión de células T
PL2571764T3 (pl)	2018-01-31	Napęd hybrydowy helikoptera
GB0902685D0 (en)	2009-04-01	Aircraft wing assembly
GB201012832D0 (en)	2010-09-15	Aircraft propeller
BRPI1009549A2 (pt)	2016-03-22	aparelho para fabricação de estrutura de aeronave
BRPI1007254A2 (pt)	2016-02-10	célula de bateria, disposição de bateria, método para produção de uma célula de bateria
FR2962977B1 (fr)	2012-08-17	Nacelle pour aeronef
BR112014008974A2 (pt)	2017-04-11	carenagem para uma separação de cabine-trailer de caminhão
GB201020189D0 (en)	2011-01-12	An aircraft structure
EP2694369A4 (en)	2015-01-21	Aircraft galley
BR112013009281A2 (pt)	2016-07-26	método para fabricar uma hélice de separador
ZA201306092B (en)	2014-04-30	Aircraft with improved aerodynamic performance
GB2483472B (en)	2012-08-15	Aircraft landing gear
PL2469074T3 (pl)	2016-12-30	Instalacja wiatrowa z platformą do załadunku helikoptera
DE102010006144B8 (de)	2013-12-24	Verkleidung für eine Flugzeugstruktur
BRPI0910290A2 (pt)	2015-09-29	estrutura de fuselagem para aeronave
BRPI0816902A2 (pt)	2015-03-17	Processo para produção de uma célula de fuselagem de um avião
BR112014000739A2 (pt)	2017-06-27	conjunto de propulsão de aeronave e nacela para um conjunto de propulsão
SG11201400299WA (en)	2014-03-28	An aircraft structure
GB201008186D0 (en)	2010-06-30	A structural assembly for an aircraft
GB201001177D0 (en)	2010-03-10	Aircraft taxiing actuator

Legal Events

Date	Code	Title	Description
2017-06-06	B08F	Application dismissed because of non-payment of annual fees [chapter 8.6 patent gazette]
2017-09-19	B08K	Patent lapsed as no evidence of payment of the annual fee has been furnished to inpi [chapter 8.11 patent gazette]