BRPI0816899A2 - componente estrutural e fuselagem de uma aeronave ou espaçonave - Google Patents

componente estrutural e fuselagem de uma aeronave ou espaçonave

Info

Publication number
BRPI0816899A2
BRPI0816899A2 BRPI0816899A BRPI0816899A BRPI0816899A2 BR PI0816899 A2 BRPI0816899 A2 BR PI0816899A2 BR PI0816899 A BRPI0816899 A BR PI0816899A BR PI0816899 A BRPI0816899 A BR PI0816899A BR PI0816899 A2 BRPI0816899 A2 BR PI0816899A2
Authority
BR
Brazil
Prior art keywords
spaceship
fuselage
aircraft
structural component
structural
Prior art date
Application number
BRPI0816899A
Other languages
English (en)
Inventor
Gensch Hinnik
Roming Thorsten
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 BRPI0816899A2 publication Critical patent/BRPI0816899A2/pt

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C1/00Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C1/00Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C1/06Frames; Stringers; Longerons ; Fuselage sections
    • B64C1/061Frames
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C1/00Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C1/06Frames; Stringers; Longerons ; Fuselage sections
    • B64C1/064Stringers; Longerons
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C1/00Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C1/06Frames; Stringers; Longerons ; Fuselage sections
    • B64C1/066Interior liners
    • B64C1/067Interior liners comprising means for preventing icing or condensation conditions
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C1/00Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C1/06Frames; Stringers; Longerons ; Fuselage sections
    • B64C1/10Bulkheads
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16LPIPES; JOINTS OR FITTINGS FOR PIPES; SUPPORTS FOR PIPES, CABLES OR PROTECTIVE TUBING; MEANS FOR THERMAL INSULATION IN GENERAL
    • F16L3/00Supports for pipes, cables or protective tubing, e.g. hangers, holders, clamps, cleats, clips, brackets
    • YGENERAL 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00Aeronautics or air transport
    • Y02T50/40Weight reduction

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Moulding By Coating Moulds (AREA)
  • Connection Of Plates (AREA)
  • Arc Welding In General (AREA)
BRPI0816899A 2007-09-18 2008-06-11 componente estrutural e fuselagem de uma aeronave ou espaçonave BRPI0816899A2 (pt)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US99429607P 2007-09-18 2007-09-18
DE102007044389A DE102007044389A1 (de) 2007-09-18 2007-09-18 Strukturbauteil und Rumpf eines Luft- oder Raumfahrzeugs
PCT/EP2008/057272 WO2009037006A1 (de) 2007-09-18 2008-06-11 Strukturbauteil und rumpf eines luft- oder raumfahrzeugs

Publications (1)

Publication Number Publication Date
BRPI0816899A2 true BRPI0816899A2 (pt) 2017-05-16

Family

ID=40384068

Family Applications (1)

Application Number Title Priority Date Filing Date
BRPI0816899A BRPI0816899A2 (pt) 2007-09-18 2008-06-11 componente estrutural e fuselagem de uma aeronave ou espaçonave

Country Status (9)

Country Link
US (1) US8800921B2 (pt)
EP (1) EP2200898B1 (pt)
JP (1) JP2010538890A (pt)
CN (1) CN101932503B (pt)
BR (1) BRPI0816899A2 (pt)
CA (1) CA2699643A1 (pt)
DE (1) DE102007044389A1 (pt)
RU (1) RU2475411C2 (pt)
WO (1) WO2009037006A1 (pt)

Families Citing this family (22)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102009014377A1 (de) 2009-03-23 2010-09-30 Airbus Deutschland Gmbh Flugzeugstruktur mit in Strukturelemente integrierte Luftführungsschächte
DE102009033444A1 (de) * 2009-07-16 2011-01-27 Airbus Operations Gmbh Schalensegment zur Herstellung einer Rumpfzellensektion für eine Rumpfzelle eines Flugzeugs
DE102010029710A1 (de) * 2010-06-04 2011-12-08 Brose Fahrzeugteile Gmbh & Co. Kg, Hallstadt Kraftfahrzeugelement mit längserstreckter Fahrzeugkomponente und Verfahren zur Montage einer längserstreckten Fahrzeugkomponente an ein Kraftfahrzeugelement
EP2404824B1 (fr) 2010-07-08 2015-09-09 Airbus Opérations SAS Structure d'aeronef et Procédé de réalisation d'une telle structure
DE102010063076A1 (de) 2010-12-14 2012-06-14 Airbus Operations Gmbh Befestigungsanordnung sowie Befestigungsbeschlag zum Befestigen eines Bauteils an ein Strukturbauteil eines Luft- oder Raumfahrzeuges
FR2977860B1 (fr) * 2011-07-13 2015-01-02 Eads Europ Aeronautic Defence Module de structure d'aeronef, structure et aeronef associes
DE102011083553A1 (de) 2011-09-27 2013-03-28 Airbus Operations Gmbh Rumpfzelle für ein Luftfahrzeug, insbesondere ein Flugzeug
FR2984845B1 (fr) * 2011-12-21 2014-07-11 Airbus Operations Sas Element de structure de fuselage d'aeronef anti deversement
FR2984844B1 (fr) 2011-12-21 2014-02-28 Airbus Operations Sas Element de structure de fuselage d'aeronef anti deversement
FR3001088B1 (fr) * 2013-01-11 2015-03-06 Airbus Operations Sas Dispositif de montage de systemes d'alimentation pour aeronef
JP6245998B2 (ja) 2014-01-17 2017-12-13 三菱航空機株式会社 航空機の消火設備および航空機
JP6251050B2 (ja) * 2014-01-17 2017-12-20 三菱航空機株式会社 航空機の消火設備および航空機
WO2015138317A1 (en) 2014-03-10 2015-09-17 Stryker Corporation Limb positioning system
PL2979975T3 (pl) * 2014-07-30 2018-01-31 Airbus Helicopters Deutschland GmbH Statek powietrzny ze strukturą ramową, która zawiera co najmniej jedną pustą ramę
CN107112738B (zh) * 2014-12-19 2020-07-10 Fi.Mo.技术股份公司 用于对尤其是辐射同轴电缆的细长体进行墙壁固定的改善的装置
US9951904B2 (en) 2015-03-24 2018-04-24 Stryker Corporation Rotatable seat clamps for rail clamp
CN104890857A (zh) * 2015-04-24 2015-09-09 江西洪都航空工业集团有限责任公司 一种新型钢构架口盖连接结构
US10814954B2 (en) * 2017-01-17 2020-10-27 The Boeing Company Insulation system
DE102017211764B4 (de) * 2017-07-10 2021-05-12 Siemens Healthcare Gmbh C-Bogen für eine medizinische Untersuchungs- oder Behandlungseinrichtung
EP3546362B1 (en) 2018-03-28 2024-01-24 Airbus Operations GmbH Fuselage assembly for an aircraft
EP3584175B1 (de) 2018-06-15 2023-03-29 ArianeGroup GmbH Verwendung zumindest einer sekundärstruktur in einem raumflugkörper, raumflugkörper und verfahren
US11312468B2 (en) * 2018-08-08 2022-04-26 The Boeing Company Elongate structures, structural assemblies with elongate structures, and methods for supporting a structural load

Family Cites Families (19)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
SU6941A1 (ru) 1926-09-13 1928-10-31 Дорнье К. Металлическа пустотела балка, в частности дл летательных аппаратов
US1922371A (en) * 1930-07-17 1933-08-15 Russell G Jones Aircraft
FR883527A (fr) * 1942-02-20 1943-07-07 Sebia Sa Perfectionnement aux avions avec moteurs à compresseur
US2755216A (en) * 1952-08-16 1956-07-17 Douglas Aircraft Co Inc Process for forming a multi-ducted shell
US2941760A (en) * 1954-12-14 1960-06-21 Rolls Royce Aircraft structure
US3087982A (en) * 1959-12-01 1963-04-30 Northrop Corp Vacuum tube mounts
US4726426A (en) * 1986-01-24 1988-02-23 The Boeing Company Fire extinguishment system for an aircraft passenger cabin
IT1221636B (it) * 1987-03-09 1990-07-12 Franco Pietrosanti Tubo flessibile ed appiattibile particolarmente per irrigazione con bocchettoni di presa lungo di esso
JPH08150930A (ja) 1994-11-30 1996-06-11 Central Japan Railway Co 鉄道車両における車体
US5893534A (en) * 1995-12-22 1999-04-13 The Boeing Company Structural apparatus and design to prevent oil can movement of webs in aircraft pressure bulkheads
DE19707519B4 (de) * 1997-02-25 2007-11-08 Scandinavian Bellyloading Co.Ab Einrichtung zum Beladen eines Laderaums insbesondere eines Flugzeuges mit Stückgut
RU2176970C2 (ru) 1999-12-17 2001-12-20 Открытое акционерное общество Таганрогский авиационный научно-технический комплекс им. Г.М. Бериева Отсек фюзеляжа летательного аппарата с пилонами внешней подвески
US7059565B2 (en) 2003-10-21 2006-06-13 The Boeing Company Aircraft frame hole patterns and brackets, and associated methods
US6883753B1 (en) 2004-03-25 2005-04-26 The Boeing Company Overhead bin and monument attachment support system
US7380754B2 (en) * 2004-09-30 2008-06-03 The Boeing Company Clamp block assemblies and methods
DE102006002248B4 (de) 2006-01-17 2008-01-03 Airbus Deutschland Gmbh Strukturgebende Konstruktion für einen Flugzeugrumpf
DE102006026918B4 (de) * 2006-06-09 2017-01-12 Airbus Operations Gmbh Rumpfstruktur
DE102007052140B4 (de) * 2007-10-31 2012-10-25 Airbus Operations Gmbh Struktur, insbesondere Rumpfstruktur eines Luft- oder Raumfahrzeugs
FR2936219B1 (fr) * 2008-09-23 2010-09-17 Airbus France Structure de fuselage pour fixation combinee de matelas d'isolation et d'equipements, aeronef incorporant une telle structure.

Also Published As

Publication number Publication date
RU2010108428A (ru) 2011-09-20
DE102007044389A1 (de) 2009-04-02
RU2475411C2 (ru) 2013-02-20
WO2009037006A1 (de) 2009-03-26
CN101932503A (zh) 2010-12-29
EP2200898B1 (de) 2014-10-22
CA2699643A1 (en) 2009-03-26
US20130187001A1 (en) 2013-07-25
JP2010538890A (ja) 2010-12-16
CN101932503B (zh) 2014-06-18
US8800921B2 (en) 2014-08-12
EP2200898A1 (de) 2010-06-30

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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]