ATE452821T1 - Monolithische selbst-versteifende platten - Google Patents

Monolithische selbst-versteifende platten

Info

Publication number
ATE452821T1
ATE452821T1 AT06777729T AT06777729T ATE452821T1 AT E452821 T1 ATE452821 T1 AT E452821T1 AT 06777729 T AT06777729 T AT 06777729T AT 06777729 T AT06777729 T AT 06777729T AT E452821 T1 ATE452821 T1 AT E452821T1
Authority
AT
Austria
Prior art keywords
skin
panel
forming
frame
box
Prior art date
Application number
AT06777729T
Other languages
English (en)
Inventor
Bruno Cacciaguerra
Original Assignee
Airbus France
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 France filed Critical Airbus France
Application granted granted Critical
Publication of ATE452821T1 publication Critical patent/ATE452821T1/de

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C25/00—Alighting gear
    • B64C25/02—Undercarriages
    • B64C25/08—Undercarriages non-fixed, e.g. jettisonable
    • B64C25/10—Undercarriages non-fixed, e.g. jettisonable retractable, foldable, or the like
    • B64C25/16—Fairings movable in conjunction with undercarriage elements
    • 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
    • B64C2001/0054—Fuselage structures substantially made from particular materials
    • B64C2001/0072—Fuselage structures substantially made from particular materials from composite materials
    • 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
    • B64C2001/0081—Fuselage structures substantially made from particular materials from metallic 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)
  • Laminated Bodies (AREA)
  • Connection Of Plates (AREA)
  • Securing Of Glass Panes Or The Like (AREA)
  • Underground Structures, Protecting, Testing And Restoring Foundations (AREA)
  • Panels For Use In Building Construction (AREA)
  • Sampling And Sample Adjustment (AREA)
  • Body Structure For Vehicles (AREA)
  • Superstructure Of Vehicle (AREA)
  • Blow-Moulding Or Thermoforming Of Plastics Or The Like (AREA)
AT06777729T 2005-07-20 2006-07-12 Monolithische selbst-versteifende platten ATE452821T1 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR0552255A FR2888816B1 (fr) 2005-07-20 2005-07-20 Panneau auto-raidi monolithique
PCT/EP2006/064154 WO2007009923A2 (fr) 2005-07-20 2006-07-12 Panneau auto-raidi monolithique

Publications (1)

Publication Number Publication Date
ATE452821T1 true ATE452821T1 (de) 2010-01-15

Family

ID=36121279

Family Applications (1)

Application Number Title Priority Date Filing Date
AT06777729T ATE452821T1 (de) 2005-07-20 2006-07-12 Monolithische selbst-versteifende platten

Country Status (11)

Country Link
US (1) US8083182B2 (de)
EP (1) EP1904366B1 (de)
JP (1) JP5027806B2 (de)
CN (1) CN101223080B (de)
AT (1) ATE452821T1 (de)
BR (1) BRPI0613628A2 (de)
CA (1) CA2614448C (de)
DE (1) DE602006011324D1 (de)
FR (1) FR2888816B1 (de)
RU (1) RU2434783C2 (de)
WO (1) WO2007009923A2 (de)

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DE102006026169B4 (de) * 2006-06-06 2012-06-21 Airbus Operations Gmbh Flugzeugrumpfstruktur und Verfahren zu deren Herstellung
DE102006026170B4 (de) * 2006-06-06 2012-06-21 Airbus Operations Gmbh Flugzeugrumpfstruktur und Verfahren zu deren Herstellung
US7861969B2 (en) * 2007-05-24 2011-01-04 The Boeing Company Shaped composite stringers and methods of making
JP5616220B2 (ja) 2007-06-01 2014-10-29 ザ トラスティーズ オブ プリンストン ユニバーシティ 宿主細胞代謝経路の調節によるウイルス感染治療
US7879276B2 (en) 2007-11-08 2011-02-01 The Boeing Company Foam stiffened hollow composite stringer
US8540921B2 (en) 2008-11-25 2013-09-24 The Boeing Company Method of forming a reinforced foam-filled composite stringer
DE102009023401B4 (de) * 2009-05-29 2014-06-26 Airbus Operations Gmbh Halter zur Befestigung einer zur Montage in einem Flugzeugrumpfelement vorgesehenen Interieurkomponente an einer Transportvorrichtung sowie Transportvorrichtung
US8500066B2 (en) 2009-06-12 2013-08-06 The Boeing Company Method and apparatus for wireless aircraft communications and power system using fuselage stringers
US8570152B2 (en) 2009-07-23 2013-10-29 The Boeing Company Method and apparatus for wireless sensing with power harvesting of a wireless signal
US8617687B2 (en) 2009-08-03 2013-12-31 The Boeing Company Multi-functional aircraft structures
GB0921960D0 (en) * 2009-12-16 2010-02-03 Airbus Operations Ltd Landing gear with noise reduction apparatus
CN103523201B (zh) * 2012-07-06 2015-12-02 哈尔滨飞机工业集团有限责任公司 直升机壁板
CN106995049A (zh) * 2017-03-23 2017-08-01 西安飞机工业（集团）有限责任公司 一种飞机匣体结构
EP3403917A1 (de) * 2017-05-18 2018-11-21 BAE SYSTEMS plc Türrahmen für ein fahrzeug
EP3625122B1 (de) * 2017-05-18 2024-08-28 BAE Systems PLC Türrahmen für ein fahrzeug
EP3456624B1 (de) 2017-09-14 2020-01-01 AIRBUS HELICOPTERS DEUTSCHLAND GmbH Sandwichverbundplatte mit einem sandwichbereich
GB2583751B (en) * 2019-05-09 2022-02-02 Safran Nacelles Ltd Acoustic panel
GB2588204B (en) 2019-10-15 2022-09-14 Safran Nacelles Ltd Aircraft nacelle inlet
FR3103782B1 (fr) 2019-12-02 2024-03-15 Latecoere Porte de cabine pressurisée d’aéronef à structure formée de poutres à section évolutive
EP4296156A1 (de) * 2022-06-20 2023-12-27 Airbus Operations GmbH Thermoplastische deckplatte für eine struktur in einem innenraum eines flugzeuges
CN115384806A (zh) * 2022-08-19 2022-11-25 大连长丰实业总公司 一种飞机座舱盖再制造过程的弧框开度控制方法

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ATE284346T1 (de) * 2001-01-26 2004-12-15 Fischer Adv Components Gmbh Einrichtung zum verbinden beweglicher teile mit strukturbauteilen von flugzeugen od. dgl.
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CA2576760C (en) * 2004-08-03 2013-09-10 Airbus Door for closing an opening inside an aircraft
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US7721995B2 (en) * 2006-12-13 2010-05-25 The Boeing Company Rib support for wing panels
US7861969B2 (en) * 2007-05-24 2011-01-04 The Boeing Company Shaped composite stringers and methods of making
US7851048B2 (en) * 2008-02-12 2010-12-14 Milliken & Co. Fiber reinforced core panel
FR2928620B1 (fr) * 2008-03-14 2012-02-03 Latecoere Panneau ouvrant d'aeronef, notamment une porte de cabine d'avion

Also Published As

Publication number Publication date
FR2888816B1 (fr) 2007-08-31
DE602006011324D1 (de) 2010-02-04
WO2007009923A3 (fr) 2007-04-26
FR2888816A1 (fr) 2007-01-26
RU2434783C2 (ru) 2011-11-27
RU2008106430A (ru) 2009-08-27
WO2007009923A2 (fr) 2007-01-25
CN101223080A (zh) 2008-07-16
BRPI0613628A2 (pt) 2012-11-06
EP1904366B1 (de) 2009-12-23
CA2614448C (fr) 2013-12-17
US20090101756A1 (en) 2009-04-23
JP2009501665A (ja) 2009-01-22
US8083182B2 (en) 2011-12-27
EP1904366A2 (de) 2008-04-02
CN101223080B (zh) 2012-12-26
JP5027806B2 (ja) 2012-09-19
CA2614448A1 (fr) 2007-01-25

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