BRPI0813121A2 - Método e dispositivo para produção de uma célula de fuselagem de uma aeronave - Google Patents

Método e dispositivo para produção de uma célula de fuselagem de uma aeronave

Info

Publication number: BRPI0813121A2
Authority: BR; Brazil
Prior art keywords: fusel; aircraft; cell; production; fusel cell
Prior art date: 2007-06-22

Application number

BRPI0813121-0A2A

Other languages

English (en)

Inventor

Holger Frauen

Tomas Gnauck

Eike Klemkow

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.)

2007-06-22

Filing date

2008-06-20

Publication date

2014-12-23

2008-06-20 Application filed by Airbus Operations Gmbh filed Critical Airbus Operations Gmbh

2014-12-23 Publication of BRPI0813121A2 publication Critical patent/BRPI0813121A2/pt

Classifications

- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
- B64F5/00—Designing, manufacturing, assembling, cleaning, maintaining or repairing aircraft, not otherwise provided for; Handling, transporting, testing or inspecting aircraft components, not otherwise provided for
- B64F5/10—Manufacturing or assembling aircraft, e.g. jigs therefor
- 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
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/49616—Structural member making
- Y10T29/49622—Vehicular structural member making
- 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
- Y10T29/00—Metal working
- Y10T29/53—Means to assemble or disassemble
- Y10T29/53961—Means to assemble or disassemble with work-holder for assembly

Landscapes

Engineering & Computer Science (AREA)
Manufacturing & Machinery (AREA)
Transportation (AREA)
Aviation & Aerospace Engineering (AREA)
Automatic Assembly (AREA)
Body Structure For Vehicles (AREA)
Moulding By Coating Moulds (AREA)

BRPI0813121-0A2A 2007-06-22 2008-06-20 Método e dispositivo para produção de uma célula de fuselagem de uma aeronave BRPI0813121A2 (pt)

Applications Claiming Priority (3)

Application Number	Priority Date	Filing Date	Title
US93684607P	2007-06-22	2007-06-22
DE102007028918A DE102007028918A1 (de)	2007-06-22	2007-06-22	Verfahren zur Herstellung einer Rumpfzelle eines Flugzeugs sowie Vorrichtung
PCT/EP2008/057850 WO2009000761A2 (en)	2007-06-22	2008-06-20	Method and device for producing a fuselage cell of an airplane

Publications (1)

Publication Number	Publication Date
BRPI0813121A2 true BRPI0813121A2 (pt)	2014-12-23

Family

ID=40075841

Family Applications (1)

Application Number	Title	Priority Date	Filing Date
BRPI0813121-0A2A BRPI0813121A2 (pt)	2007-06-22	2008-06-20	Método e dispositivo para produção de uma célula de fuselagem de uma aeronave

Country Status (9)

Country	Link
US (1)	US7966729B2 (pt)
EP (1)	EP2158125B1 (pt)
JP (1)	JP2010530829A (pt)
CN (1)	CN101743163B (pt)
BR (1)	BRPI0813121A2 (pt)
CA (1)	CA2688137A1 (pt)
DE (1)	DE102007028918A1 (pt)
RU (1)	RU2467928C2 (pt)
WO (1)	WO2009000761A2 (pt)

Families Citing this family (21)

* Cited by examiner, † Cited by third party
Publication number	Priority date	Publication date	Assignee	Title
DE102007028918A1 (de)	2007-06-22	2009-01-02	Airbus Deutschland Gmbh	Verfahren zur Herstellung einer Rumpfzelle eines Flugzeugs sowie Vorrichtung
CA2707110C (en) *	2007-11-29	2013-06-11	Airbus Operations Sas	Method of preparing the connection between two fuselage sections of an aircraft
DE102009018991A1 (de) *	2009-05-01	2010-11-04	Airbus Operations Gmbh	Vorrichtung zur räumlichen Ausrichtung von mindestens zwei Untergruppenbauteilen sowie Verfahren
DE102009021369A1 (de)	2009-05-12	2010-11-18	Airbus Operations Gmbh	Verfahren zur Herstellung eines Flugzeugrumpfes und Flugzeugrumpf
US8510952B2 (en)	2010-07-15	2013-08-20	The Boeing Company	Agile manufacturing apparatus and method for high throughput
FR2980456A1 (fr) *	2011-09-22	2013-03-29	Airbus Operations Sas	Procede de montage de cockpit et module de cockpit correspondant
CN102658870B (zh) *	2012-05-16	2014-06-04	浙江大学	一种基于折线逼近的壁板插配方法
DE102012015666A1 (de) *	2012-08-09	2014-02-13	Premium Aerotec Gmbh	Verfahren und Vorrichtung zur Montage von Spanten an einem Hautfeld bei der Herstellung eines Rumpfschalenbauteils für ein Flugzeug, sowie Verfahren zur Herstellung eines Rumpfschalenbauteils für ein Flugzeug
DE102013110684A1 (de)	2013-09-26	2015-03-26	Airbus Operations Gmbh	Verfahren zum Montieren eines Flugzeugrumpfs und Rumpffertigungsstation
US9874628B2 (en) *	2013-11-12	2018-01-23	The Boeing Company	Dual hidden point bars
FR3020347B1 (fr) *	2014-04-28	2016-05-20	Airbus Operations Sas	Procede d'assemblage d'une partie arriere d'aeronef
US10406593B2 (en)	2014-07-09	2019-09-10	The Boeing Company	Method of using a tower for accessing an interior of a fuselage assembly
EP2985232A1 (en) *	2014-08-13	2016-02-17	Airbus Operations GmbH	Method for assembling an aircraft fuselage
KR101687554B1 (ko) *	2014-12-30	2016-12-19	한국항공우주산업 주식회사	항공기 동체 자동 장착 및 탈착 장치
CN105129069B (zh) *	2015-08-04	2017-04-26	江西洪都航空工业集团有限责任公司	一种楔形块舱段连接装置
DE102016210089B4 (de) *	2016-06-08	2025-02-20	Airbus Operations Gmbh	Verfahren zum Fügen von Hautabschnitten eines umfänglich geschlossenen Rumpfes
DE102016210124B4 (de) *	2016-06-08	2024-08-29	Airbus Operations Gmbh	Verfahren zur Integration einer Hinterbaustruktur-Baugruppe in eine Struktur eines Luft- oder Raumfahrzeugs
CN106827557B (zh) *	2017-01-17	2018-11-02	成都飞机工业（集团）有限责任公司	复合材料共胶接加筋结构胶接面补偿方法
CN111003139B (zh) *	2019-12-27	2021-06-22	中国商用飞机有限责任公司	民用飞机的气密地板
FR3138122A1 (fr) *	2022-07-25	2024-01-26	Airbus Operations	Système de transport de grille de plancher de cabine d’aéronef en vue d’un assemblage d’un corps de fuselage d’aéronef et procédé de calibration dudit système de transport.
CN118494773B (zh) *	2024-07-17	2024-09-13	中航成飞民用飞机有限责任公司	用于大飞机机头总装多段组件的对合工装及对合方法

Family Cites Families (16)

* Cited by examiner, † Cited by third party
Publication number	Priority date	Publication date	Assignee	Title
US4674712A (en) *	1985-01-22	1987-06-23	The Boeing Company	Double-lobe fuselage composite airplane
FR2649665B1 (fr) *	1989-07-12	1991-11-08	Airbus Ind	Fuselage de grande capacite pour avion
JPH0414598U (pt) *	1990-05-30	1992-02-05
RU2121452C1 (ru) *	1997-01-24	1998-11-10	Закрытое акционерное общество "Саратовский авиационный завод"	Способ сборки фюзеляжа самолета
RU2123965C1 (ru) *	1997-01-28	1998-12-27	Государственное акционерное общество "Ташкентское авиационное производственное объединение им.В.П.Чкалова"	Способ сборки объемных агрегатов летательных аппаратов
EP0857648B1 (de) *	1997-02-05	2003-01-15	Anatoli J. Prof. Dr. Vassiliev	Flugzeug für Personen- und/oder Frachttransport
DE19834703C1 (de) *	1998-07-31	1999-12-30	Daimler Chrysler Aerospace	Verfahren zur Herstellung, Ausrüstung und Ausstattung eines Flugzeugrumpfes und Vorrichtung zur Durchführung des Verfahrens
US6505393B2 (en) *	1998-07-31	2003-01-14	Airbus Deutschland Gmbh	Two-part riveting apparatus and method for riveting barrel-shaped components such as aircraft fuselage components
DE19929471C1 (de) *	1999-06-26	2001-01-18	Eads Airbus Gmbh	Verfahren und Vorrichtung zur Herstellung eines dreidimensionalen Großbauteiles
RU28859U1 (ru) *	2002-10-11	2003-04-20	Федеральное государственное унитарное предприятие Казанское авиационное производственное объединение им. С.П.Горбунова	Устройство для сборки отсека фюзеляжа летательного аппарата
US7234667B1 (en) *	2003-12-11	2007-06-26	Talmage Jr Robert N	Modular aerospace plane
US7325771B2 (en) *	2004-09-23	2008-02-05	The Boeing Company	Splice joints for composite aircraft fuselages and other structures
DE102004056286B4 (de) *	2004-11-22	2015-12-24	Airbus Operations Gmbh	Vorrichtung und Verfahren zum form- und/oder abmessungsunabhängigen Zusammenfügen und Heften von mehreren Einzelkomponenten zur Bildung von eigensteifen, transportfähigen Sektionen für Verkehrsmittel, insbesondere für Luftfahrzeuge
DE102005023886A1 (de) *	2005-05-24	2006-12-07	Airbus Deutschland Gmbh	Flugzeugrumpf-Montagekonzept
FR2906785B1 (fr) *	2006-10-10	2009-12-04	Airbus France	Fuselage d'aeronef realise a partir de panneaux longitudinaux et procede de realisation d'un tel fuselage
DE102007028918A1 (de)	2007-06-22	2009-01-02	Airbus Deutschland Gmbh	Verfahren zur Herstellung einer Rumpfzelle eines Flugzeugs sowie Vorrichtung

2007
- 2007-06-22 DE DE102007028918A patent/DE102007028918A1/de not_active Withdrawn
2008
- 2008-06-20 JP JP2010512700A patent/JP2010530829A/ja active Pending
- 2008-06-20 CA CA002688137A patent/CA2688137A1/en not_active Abandoned
- 2008-06-20 WO PCT/EP2008/057850 patent/WO2009000761A2/en not_active Ceased
- 2008-06-20 BR BRPI0813121-0A2A patent/BRPI0813121A2/pt not_active IP Right Cessation
- 2008-06-20 RU RU2010101163/11A patent/RU2467928C2/ru not_active IP Right Cessation
- 2008-06-20 EP EP08761264.4A patent/EP2158125B1/en active Active
- 2008-06-20 CN CN200880021373.XA patent/CN101743163B/zh active Active
2009
- 2009-12-10 US US12/635,302 patent/US7966729B2/en active Active

Also Published As

Publication number	Publication date
EP2158125A2 (en)	2010-03-03
RU2467928C2 (ru)	2012-11-27
WO2009000761A4 (en)	2009-05-28
CN101743163A (zh)	2010-06-16
WO2009000761A2 (en)	2008-12-31
JP2010530829A (ja)	2010-09-16
WO2009000761A3 (en)	2009-04-09
EP2158125B1 (en)	2019-08-07
CA2688137A1 (en)	2008-12-31
DE102007028918A1 (de)	2009-01-02
RU2010101163A (ru)	2011-07-27
US7966729B2 (en)	2011-06-28
US20100192376A1 (en)	2010-08-05
CN101743163B (zh)	2016-01-13

Publication	Publication Date	Title
BRPI0813121A2 (pt)	2014-12-23	Método e dispositivo para produção de uma célula de fuselagem de uma aeronave
IL259567A (en)	2018-07-31	System and method for inspecting a substrate
BR112012001100A2 (pt)	2016-02-23	aparelho e método para construções de estrutura e tijolo
DOP2011000384A (es)	2012-12-15	Metodos para el cultivo de celulas madre y progenitoras
BRPI0910371A2 (pt)	2015-10-20	método para confeccionar uma estrutura laminada e estrutura laminada
BRPI0822518A2 (pt)	2015-06-16	Método e disposição para a fabricação de uma estrutura laminada
BR112012010469A2 (pt)	2016-03-08	adesivo estrutural e metodo para aplicar adesivo estrutural
BRPI1013624A2 (pt)	2016-04-19	aparelho de exibição e método para fabricação do aparelho de exibição
BRPI0822737A2 (pt)	2015-06-23	Método e disposição para obscurecer uma imagem
BR112012026270A2 (pt)	2018-02-27	método para compensar uma variação de impedância e sistema para compensar uma variação de impedância
BRPI0923566A2 (pt)	2016-01-26	método e sistema para detecção de uma expressão vocal relevante
BRPI0923613A2 (pt)	2018-05-29	método e sistema para manter desempenho operacional de uma transparência
BRPI0918294A2 (pt)	2015-12-22	dispositivo e método para produzir explosões
BRPI1012813A2 (pt)	2018-01-16	aparelho e método para modelar projetos de poço e desempenho de poço
BR112012005568A2 (pt)	2016-05-17	aparelho e métodos para medir processos biológicos
BRPI1008617A2 (pt)	2016-03-15	método e aparelho para lipoaspiração
BRPI1015922A2 (pt)	2016-04-26	sistemas e métodos para testar analitos
BRPI0820426A2 (pt)	2015-05-19	Método e dispositivo para controlar uma célula eletrolítica
BRPI1009549A2 (pt)	2016-03-22	aparelho para fabricação de estrutura de aeronave
FI20086032A0 (fi)	2008-10-31	Menetelmä ja laitteisto nestemäisen biopolttoaineen tuottamiseksi kiinteästä biomassasta
BRPI0920860A2 (pt)	2015-12-22	aparelho e método de fabricação de uma estrutura conformada conicamente
BRPI0924019A2 (pt)	2018-06-05	método de fermentação e aparelhos adaptados para o método
BRPI0914120A2 (pt)	2015-10-20	método e aparelho para determinação estrutural
BRPI1012150A2 (pt)	2016-03-29	método de fabricar um fuselagem de aeronave e uma fuselagem de aeronave
BRPI0924254A2 (pt)	2018-07-31	método e sistema para atualizar um equipamento de integração computador-telefone

Legal Events

Date	Code	Title	Description
2015-12-01	B08F	Application dismissed because of non-payment of annual fees [chapter 8.6 patent gazette]	Free format text: REFERENTE AS 6A E 7A ANUIDADES.
2016-03-29	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.