BRPI0810569A2 - elemento estrutural de fuselagem de uma aeronave - Google Patents
elemento estrutural de fuselagem de uma aeronaveInfo
- Publication number
- BRPI0810569A2 BRPI0810569A2 BRPI0810569A BRPI0810569A BRPI0810569A2 BR PI0810569 A2 BRPI0810569 A2 BR PI0810569A2 BR PI0810569 A BRPI0810569 A BR PI0810569A BR PI0810569 A BRPI0810569 A BR PI0810569A BR PI0810569 A2 BRPI0810569 A2 BR PI0810569A2
- Authority
- BR
- Brazil
- Prior art keywords
- aircraft
- structural element
- fuselage
- aircraft fuselage
- fuselage structural
- Prior art date
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
- B64C1/064—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
- B64C1/40—Sound or heat insulation, e.g. using insulation blankets
-
- 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)
- Connection Of Plates (AREA)
- Tires In General (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
- Gasket Seals (AREA)
- Body Structure For Vehicles (AREA)
- Mutual Connection Of Rods And Tubes (AREA)
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US91409707P | 2007-04-26 | 2007-04-26 | |
DE102007019821A DE102007019821B4 (de) | 2007-04-26 | 2007-04-26 | Strukturelement eines Flugzeugrumpfs |
PCT/EP2008/055084 WO2008132171A2 (en) | 2007-04-26 | 2008-04-25 | Structural element of an aircraft fuselage |
Publications (1)
Publication Number | Publication Date |
---|---|
BRPI0810569A2 true BRPI0810569A2 (pt) | 2017-05-09 |
Family
ID=39829141
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
BRPI0810569A BRPI0810569A2 (pt) | 2007-04-26 | 2008-04-25 | elemento estrutural de fuselagem de uma aeronave |
Country Status (10)
Country | Link |
---|---|
US (1) | US8905349B2 (pt) |
EP (1) | EP2137064B1 (pt) |
JP (1) | JP2010524771A (pt) |
CN (1) | CN101674978B (pt) |
AT (1) | ATE525281T1 (pt) |
BR (1) | BRPI0810569A2 (pt) |
CA (1) | CA2682969A1 (pt) |
DE (1) | DE102007019821B4 (pt) |
RU (1) | RU2470830C2 (pt) |
WO (1) | WO2008132171A2 (pt) |
Families Citing this family (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE102007032235B4 (de) * | 2007-07-11 | 2015-05-07 | Airbus Operations Gmbh | Leichtes Schienensystem zur Krafteinleitung großer Lasten in eine Struktur |
DE102007032233B4 (de) | 2007-07-11 | 2014-07-10 | Airbus Operations Gmbh | Installationssystem für ein Flugzeug |
DE102007052672B4 (de) * | 2007-11-05 | 2016-12-01 | Airbus Operations Gmbh | Rumpfzellenstruktur eines Flugzeugs zur vereinfachten Verlegung und Befestigung von Haltern zur Befestigung von Leitungen |
DE102008020789A1 (de) | 2008-04-25 | 2009-11-05 | Airbus Deutschland Gmbh | Befestigungssystem sowie Verfahren zum Befestigen eines Elementes einer Flugzeuginnenausstattung |
DE102009029120B4 (de) | 2009-09-02 | 2011-12-08 | Airbus Operations Gmbh | Anordnung, insbesondere im Luft- und Raumfahrtbereich |
WO2012084204A2 (en) * | 2010-12-23 | 2012-06-28 | Airbus Operations Gmbh | Aircraft system component carrier system and mounting method |
FR2976916B1 (fr) * | 2011-06-27 | 2013-07-26 | Airbus Operations Sas | Dispositif et procede d'assemblage de deux troncons de fuselage d'aeronef |
DE102012001797A1 (de) * | 2012-01-30 | 2013-08-01 | Airbus Operations Gmbh | System und Verfahren zur Montage von Flugzeugsystemkomponenten in der Crown Area eines Flugzeugs |
DE102012009312A1 (de) * | 2012-05-10 | 2013-11-14 | Airbus Operations Gmbh | Rumpfaufbau |
EP3266705B1 (en) * | 2016-07-05 | 2019-06-26 | Airbus Operations GmbH | Interior component carrier system and method for mounting an aircraft interior component carrier system |
DE102018210507A1 (de) * | 2018-06-27 | 2020-01-02 | Airbus Operations Gmbh | Montagesystem für eine automatisierte Innenmontage eines Flugzeugrumpfes |
CN111055995A (zh) * | 2019-12-31 | 2020-04-24 | 南京儒一航空机械装备有限公司 | 一种不易变形的主梁梁体及其加工工艺 |
Family Cites Families (29)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2382358A (en) * | 1944-02-03 | 1945-08-14 | Budd Edward G Mfg Co | Stressed skin airfoil joint |
US2819032A (en) * | 1953-10-20 | 1958-01-07 | Douglas Aircraft Co Inc | Aircraft fuselage having panel damping material |
US2945653A (en) * | 1956-12-28 | 1960-07-19 | Republic Aviat Corp | Aircraft skin construction |
SU613947A1 (ru) * | 1976-03-24 | 1978-07-05 | Предприятие П/Я М-5261 | Металлический корпус лихтера |
JPS5492585A (en) | 1977-12-29 | 1979-07-21 | Japan Organo Co Ltd | Ion exchange method |
US4310132A (en) * | 1978-02-16 | 1982-01-12 | Nasa | Fuselage structure using advanced technology fiber reinforced composites |
JPS624054Y2 (pt) * | 1979-07-04 | 1987-01-29 | ||
JPS5671680A (en) * | 1979-11-16 | 1981-06-15 | Mitsubishi Heavy Ind Ltd | Manufacture of beam material with opening |
DE3341564A1 (de) * | 1983-11-17 | 1985-05-30 | Messerschmitt-Bölkow-Blohm GmbH, 8012 Ottobrunn | Gekruemmtes flaechenbauteil, insbesondere fuer luftfahrzeuge und vorrichtung zu deren herstellung |
JP2591093B2 (ja) | 1988-08-20 | 1997-03-19 | 富士通株式会社 | 接触抵抗測定装置 |
CH681383A5 (pt) * | 1990-04-11 | 1993-03-15 | Alusuisse Lonza Services Ag | |
JPH0613834B2 (ja) | 1990-05-02 | 1994-02-23 | 住友金属工業株式会社 | トンネル掘削における排土搬出方法および装置 |
JPH0414598U (pt) * | 1990-05-30 | 1992-02-05 | ||
JPH08156897A (ja) * | 1994-12-06 | 1996-06-18 | Mitsubishi Heavy Ind Ltd | 舵面構造 |
DE19639339B4 (de) * | 1996-09-25 | 2004-06-24 | Dwa Deutsche Waggonbau Gmbh | Schalenstruktur aus faserverstärktem Kunststoff für Fahrzeuge oder Behälter, insbesondere für Wagenkästen von Schienenfahrzeugen |
US5931415A (en) * | 1997-05-09 | 1999-08-03 | The Boeing Company | Plug-type overwing emergency exit door assembly |
RU2143365C1 (ru) * | 1999-07-06 | 1999-12-27 | Закрытое акционерное общество "Интеллект" | Стрингер судна |
DE19955397C1 (de) | 1999-11-18 | 2001-01-04 | Eads Airbus Gmbh | An einem Stringer einer Flugzeugzellenstruktur befestigte Haltevorrichtung |
SE519185C2 (sv) * | 2001-06-07 | 2003-01-28 | Saab Ab | Flygplanspanel |
US6648273B2 (en) | 2001-10-30 | 2003-11-18 | The Boeing Company | Light weight and high strength fuselage |
US6712316B2 (en) * | 2002-08-01 | 2004-03-30 | The Boeing Company | Snap-on sidewall assembly |
US20050005544A1 (en) | 2003-07-10 | 2005-01-13 | Borowiecki Fabian A. | One piece decorative insulation and interior panel assembly |
US7059565B2 (en) * | 2003-10-21 | 2006-06-13 | The Boeing Company | Aircraft frame hole patterns and brackets, and associated methods |
US7040575B2 (en) * | 2004-03-29 | 2006-05-09 | The Boeing Company | Foam composite insulation for aircraft |
US7261256B2 (en) * | 2004-03-29 | 2007-08-28 | The Boeing Company | Variable-duct support assembly |
JP2008505005A (ja) * | 2004-07-01 | 2008-02-21 | スリーエム イノベイティブ プロパティズ カンパニー | 遮断方法 |
DE102004035170B3 (de) * | 2004-07-21 | 2005-08-18 | Gerd K.H. Prof. h.c. Prof. Dr.-Ing. Sepold | Verfahren zur Fertigung eines zylindrisch gekrümmten Blechteils, insbesondere eines Außenhaut-Blechteils eines Flugkörpers |
US7325771B2 (en) * | 2004-09-23 | 2008-02-05 | The Boeing Company | Splice joints for composite aircraft fuselages and other structures |
JP4354463B2 (ja) * | 2006-02-28 | 2009-10-28 | 三菱重工業株式会社 | 複合材を用いた構造部材の成形方法及び複合材料を用いた構造部材 |
-
2007
- 2007-04-26 DE DE102007019821A patent/DE102007019821B4/de not_active Expired - Fee Related
-
2008
- 2008-04-25 BR BRPI0810569A patent/BRPI0810569A2/pt not_active IP Right Cessation
- 2008-04-25 EP EP08736584A patent/EP2137064B1/en not_active Not-in-force
- 2008-04-25 JP JP2010504711A patent/JP2010524771A/ja active Pending
- 2008-04-25 RU RU2009136665/11A patent/RU2470830C2/ru not_active IP Right Cessation
- 2008-04-25 CA CA002682969A patent/CA2682969A1/en not_active Abandoned
- 2008-04-25 US US12/595,230 patent/US8905349B2/en not_active Expired - Fee Related
- 2008-04-25 CN CN200880013652.1A patent/CN101674978B/zh not_active Expired - Fee Related
- 2008-04-25 WO PCT/EP2008/055084 patent/WO2008132171A2/en active Application Filing
- 2008-04-25 AT AT08736584T patent/ATE525281T1/de not_active IP Right Cessation
Also Published As
Publication number | Publication date |
---|---|
EP2137064B1 (en) | 2011-09-21 |
RU2470830C2 (ru) | 2012-12-27 |
DE102007019821B4 (de) | 2012-11-22 |
DE102007019821A1 (de) | 2008-11-13 |
US8905349B2 (en) | 2014-12-09 |
WO2008132171A4 (en) | 2009-02-26 |
EP2137064A2 (en) | 2009-12-30 |
WO2008132171A3 (en) | 2009-01-15 |
CN101674978A (zh) | 2010-03-17 |
WO2008132171A2 (en) | 2008-11-06 |
ATE525281T1 (de) | 2011-10-15 |
CA2682969A1 (en) | 2008-11-06 |
CN101674978B (zh) | 2015-04-29 |
RU2009136665A (ru) | 2011-04-20 |
JP2010524771A (ja) | 2010-07-22 |
US20100243805A1 (en) | 2010-09-30 |
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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] | ||
B350 | Update of information on the portal [chapter 15.35 patent gazette] |