JP5027806B2 - 一体型自己補剛パネル - Google Patents

一体型自己補剛パネル Download PDF

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Publication number
JP5027806B2
JP5027806B2 JP2008521941A JP2008521941A JP5027806B2 JP 5027806 B2 JP5027806 B2 JP 5027806B2 JP 2008521941 A JP2008521941 A JP 2008521941A JP 2008521941 A JP2008521941 A JP 2008521941A JP 5027806 B2 JP5027806 B2 JP 5027806B2
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JP
Japan
Prior art keywords
panel
skin
wall
composite
fitting
Prior art date
Legal status (The legal status 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 status listed.)
Expired - Fee Related
Application number
JP2008521941A
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English (en)
Japanese (ja)
Other versions
JP2009501665A5 (enExample
JP2009501665A (ja
Inventor
カッチャグェッラ．ブルーノ
Original Assignee
エアバス オペラシオン（エス．ア．エス）
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.)
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Publication date
Application filed by エアバス オペラシオン（エス．ア．エス） filed Critical エアバス オペラシオン（エス．ア．エス）
Publication of JP2009501665A publication Critical patent/JP2009501665A/ja
Publication of JP2009501665A5 publication Critical patent/JP2009501665A5/ja
Application granted granted Critical
Publication of JP5027806B2 publication Critical patent/JP5027806B2/ja
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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)
  • Blow-Moulding Or Thermoforming Of Plastics Or The Like (AREA)
  • Superstructure Of Vehicle (AREA)
  • Sampling And Sample Adjustment (AREA)
  • Body Structure For Vehicles (AREA)
JP2008521941A 2005-07-20 2006-07-12 一体型自己補剛パネル Expired - Fee Related JP5027806B2 (ja)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
FR0552255 2005-07-20
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 (3)

Publication Number Publication Date
JP2009501665A JP2009501665A (ja) 2009-01-22
JP2009501665A5 JP2009501665A5 (enExample) 2012-02-16
JP5027806B2 true JP5027806B2 (ja) 2012-09-19

Family

ID=36121279

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2008521941A Expired - Fee Related JP5027806B2 (ja) 2005-07-20 2006-07-12 一体型自己補剛パネル

Country Status (11)

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

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DE102006026168A1 (de) 2006-06-06 2008-01-31 Airbus Deutschland Gmbh Flugzeugrumpfstruktur und Verfahren zu deren Herstellung
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
IN2009KN04568A (enExample) 2007-06-01 2015-08-28 Univ Princeton
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
US20200172223A1 (en) * 2017-05-18 2020-06-04 Bae Systems Plc Door assembly for a vehicle
EP3403917A1 (en) * 2017-05-18 2018-11-21 BAE SYSTEMS plc Door assembly for a vehicle
EP3456624B1 (en) 2017-09-14 2020-01-01 AIRBUS HELICOPTERS DEUTSCHLAND GmbH A composite sandwich panel with a sandwich area
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 (en) * 2022-06-20 2023-12-27 Airbus Operations GmbH Thermoplastic cover panel for a structure in an interior space of an aircraft
CN115384806B (zh) * 2022-08-19 2024-11-12 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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US4893964A (en) * 1989-02-06 1990-01-16 Grumman Aerospace Corporation Interlocking structural members utilizing overlying composite strips
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RU2143366C1 (ru) * 1999-07-08 1999-12-27 Закрытое акционерное общество "Интеллект" Крышка люка судна
RU2144484C1 (ru) * 1999-07-08 2000-01-20 Закрытое акционерное общество "Интеллект" Крышка люка летательного аппарата слоистая
JP4416900B2 (ja) * 2000-03-10 2010-02-17 富士重工業株式会社 複合材パネルおよびその製造方法
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EP1773665B1 (fr) * 2004-08-03 2008-02-13 Airbus Porte renforcee
RU2389658C2 (ru) * 2004-08-03 2010-05-20 Эрбюс Дверь, предназначенная для закрытия прохода внутри воздушного судна
BRPI0513650A (pt) * 2004-08-03 2008-05-13 Airbus porta de segurança para aeronave e aeronave
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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
RU2008106430A (ru) 2009-08-27
DE602006011324D1 (de) 2010-02-04
WO2007009923A2 (fr) 2007-01-25
FR2888816B1 (fr) 2007-08-31
CA2614448C (fr) 2013-12-17
CN101223080B (zh) 2012-12-26
JP2009501665A (ja) 2009-01-22
WO2007009923A3 (fr) 2007-04-26
BRPI0613628A2 (pt) 2012-11-06
CN101223080A (zh) 2008-07-16
US8083182B2 (en) 2011-12-27
US20090101756A1 (en) 2009-04-23
FR2888816A1 (fr) 2007-01-26
ATE452821T1 (de) 2010-01-15
RU2434783C2 (ru) 2011-11-27
EP1904366A2 (fr) 2008-04-02
CA2614448A1 (fr) 2007-01-25
EP1904366B1 (fr) 2009-12-23

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