ATE465081T1 - Verformbarer vorderer druckspant für ein flugzeug - Google Patents

Verformbarer vorderer druckspant für ein flugzeug

Info

Publication number
ATE465081T1
ATE465081T1 AT06849311T AT06849311T ATE465081T1 AT E465081 T1 ATE465081 T1 AT E465081T1 AT 06849311 T AT06849311 T AT 06849311T AT 06849311 T AT06849311 T AT 06849311T AT E465081 T1 ATE465081 T1 AT E465081T1
Authority
AT
Austria
Prior art keywords
dome
aircraft
crown panel
bulkhead
deformable
Prior art date
Application number
AT06849311T
Other languages
English (en)
Inventor
Barney Anderson
Jeffrey Swada
William Koch
Original Assignee
Boeing Co
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 Boeing Co filed Critical Boeing Co
Application granted granted Critical
Publication of ATE465081T1 publication Critical patent/ATE465081T1/de

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
    • B64C1/10—Bulkheads
    • 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
    • B64C1/36—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like adapted to receive antennas or radomes
    • 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
    • Y10T156/00—Adhesive bonding and miscellaneous chemical manufacture
    • Y10T156/10—Methods of surface bonding and/or assembly therefor

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Tires In General (AREA)
  • Buildings Adapted To Withstand Abnormal External Influences (AREA)
  • Pressure Vessels And Lids Thereof (AREA)
  • Catching Or Destruction (AREA)
  • Finger-Pressure Massage (AREA)
  • Measuring Pulse, Heart Rate, Blood Pressure Or Blood Flow (AREA)
AT06849311T 2006-01-19 2006-12-13 Verformbarer vorderer druckspant für ein flugzeug ATE465081T1 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US11/335,275 US7766277B2 (en) 2006-01-19 2006-01-19 Deformable forward pressure bulkhead for an aircraft
PCT/US2006/047460 WO2007084227A2 (en) 2006-01-19 2006-12-13 Deformable forward pressure bulkhead for an aircraft

Publications (1)

Publication Number Publication Date
ATE465081T1 true ATE465081T1 (de) 2010-05-15

Family

ID=38191126

Family Applications (1)

Application Number Title Priority Date Filing Date
AT06849311T ATE465081T1 (de) 2006-01-19 2006-12-13 Verformbarer vorderer druckspant für ein flugzeug

Country Status (7)

Country Link
US (3) US7766277B2 (de)
EP (1) EP1976751B1 (de)
JP (1) JP4804541B2 (de)
CN (1) CN101360648B (de)
AT (1) ATE465081T1 (de)
DE (1) DE602006013884D1 (de)
WO (1) WO2007084227A2 (de)

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US7997529B2 (en) * 2006-01-19 2011-08-16 The Boeing Company Compliant panel for aircraft
US7766277B2 (en) * 2006-01-19 2010-08-03 The Boeing Company Deformable forward pressure bulkhead for an aircraft
DE102006029231B4 (de) * 2006-06-26 2013-09-26 Airbus Operations Gmbh Druckschott für einen Rumpf für die Luft- und Raumfahrt
DE102006051989B4 (de) * 2006-11-03 2010-09-30 Airbus Deutschland Gmbh Versteifte Beplankung für ein Luft- oder Raumfahrzeug mit einem Laminat-Stringer hoher Steifigkeit
DE102007018753B4 (de) * 2007-04-20 2012-11-08 Airbus Operations Gmbh Brandschutzraum für Flugzeugpassagiere mit Hilfe von Rumpfbehäutung aus Faser-Metall-Laminaten
DE102007052140B4 (de) * 2007-10-31 2012-10-25 Airbus Operations Gmbh Struktur, insbesondere Rumpfstruktur eines Luft- oder Raumfahrzeugs
DE102007054101A1 (de) * 2007-11-13 2009-05-20 Eads Deutschland Gmbh Druckschott für ein Flugzeug
EP2259965B1 (de) * 2008-03-31 2013-01-09 Honda Patents & Technologies North America, LLC Druckschott für ein flugzeug
FR2933375B1 (fr) * 2008-07-01 2011-04-15 Airbus France Agencement de fuselage d'avion
US20100155533A1 (en) * 2008-12-23 2010-06-24 Spirit Aerosystems, Inc. Composite forward pressure bulkhead
FR2940959B1 (fr) * 2009-01-15 2011-03-11 Airbus France Partie avant d'aeronef comportant une cloison concave separant une zone de radome non pressurisee et une zone pressurisee
FR2943311B1 (fr) * 2009-03-19 2011-03-04 Airbus France Raidisseurs sous bavette pour aeronef
DE102009049007A1 (de) * 2009-10-09 2011-04-21 Airbus Operations Gmbh Druckrumpf eines Flugzeuges mit heckseitiger Druckkalotte
FR2953193B1 (fr) * 2009-11-30 2012-03-16 Airbus Operations Sas Aeronef comportant une cloison interne
FR2970237B1 (fr) 2011-01-12 2013-02-08 Airbus Operations Sas Panneau superieur pour cockpit d'aeronef et aeronef comprenant un tel panneau
EP2675711B1 (de) 2011-02-18 2016-06-22 Airbus Operations Zentraler pylon für ein flugzeugcockpit und flugzeug mit einem solchen pylon
US8616500B2 (en) * 2011-03-04 2013-12-31 The Boeing Company Diamond shaped window for composite and/or metallic airframe
EP2761980B1 (de) * 2011-09-30 2020-01-15 Airbus Operations S.A.S. Stromzentrum für ein flugzeug
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US8931738B2 (en) * 2012-02-21 2015-01-13 Raytheon Company Releasable radome cover
FR2998544B1 (fr) 2012-11-28 2016-12-23 Airbus Operations Sas Dossier de siege d'aeronef comprenant une colonne structurale portant des dispositifs transversaux de support de l'occupant
FR2999344B1 (fr) * 2012-12-10 2018-04-13 Airbus Operations Antenne de radar meteorologique embarque pour aeronef et aeronef associe
FR2999524B1 (fr) * 2012-12-17 2015-02-20 Airbus Operations Sas Fond etanche avant d'aeronef comprenant des renfoncements pour le logement d'equipements de cockpit
US10189578B2 (en) 2013-06-12 2019-01-29 The Boeing Company Self-balancing pressure bulkhead
US9199713B2 (en) * 2013-07-08 2015-12-01 The Boeing Company Pressure panels
US9187168B2 (en) * 2013-07-30 2015-11-17 The Boeing Company Natural-path tearstraps and stiffeners for spherical composite pressure bulkheads
US9564681B2 (en) * 2013-11-11 2017-02-07 Gogo Llc Radome having localized areas of reduced radio signal attenuation
CN104002977B (zh) * 2014-05-06 2017-01-18 嘉兴美盾航空材料有限公司 防鸟撞挡板及其制备工艺
FR3033315B1 (fr) 2015-03-04 2018-06-15 Latecoere Procede de realisation d'un fond etanche avant de fuselage d'avion et fuselage equipe d'un tel fond etanche
EP3064429A1 (de) * 2015-03-06 2016-09-07 Airbus Operations GmbH Druckschott für unrunde Rumpfsektion
FR3036115B1 (fr) * 2015-05-11 2017-05-19 Michelin & Cie Composition de caoutchouc
EP3095688B1 (de) * 2015-05-20 2017-10-04 Airbus Operations GmbH Druckschott für einen flugzeugrumpf
EP3095689B1 (de) 2015-05-20 2017-10-04 Airbus Operations GmbH Druckschott für einen flugzeugrumpf
EP3176072B1 (de) * 2015-12-03 2019-04-03 Airbus Operations S.L. Druckschott
FR3045002B1 (fr) * 2015-12-11 2017-12-01 Airbus Operations Sas Systeme de maintien d'un fond etanche avant par des bielles liees au plancher et non paralleles entre elles
DE102016203410A1 (de) * 2016-03-02 2017-09-07 Efficient Energy Gmbh Wärmepumpe mit einer gasfalle, verfahren zum betreiben einer wärmepumpe mit einer gasfalle und verfahren zum herstellen einer wärmepumpe mit einer gasfalle
DE102016002844B3 (de) * 2016-03-10 2017-08-10 Premium Aerotec Gmbh Strukturbauteil, Verfahren zur Herstellung eines Strukturbauteils, Druckrumpf für ein Fahrzeug mit Strukturbauteil
US9776704B1 (en) 2016-05-16 2017-10-03 The Boeing Company Composite pressure bulkhead
CN105966596B (zh) * 2016-06-13 2019-03-29 江西洪都航空工业集团有限责任公司 一种变厚度薄壁蒙皮结构
US10926858B2 (en) 2017-08-07 2021-02-23 The Boeing Company Pressure bulkhead system
US10974806B2 (en) * 2017-10-05 2021-04-13 Gulfstream Aerospace Corporation Unified canopies for aircraft
EP3597527A1 (de) * 2018-07-20 2020-01-22 Bombardier Inc. Druckschott und verfahren zur installation
FR3085940B1 (fr) * 2018-09-13 2022-04-08 Airbus Operations Sas Plancher d'une zone anterieure d'un aeronef ayant une structure simplifiee
ES1235737Y (es) * 2019-07-24 2020-01-02 Citd Engineering & Tech Sl Mamparo de presion
CN111591433B (zh) * 2019-11-12 2021-10-22 中国科学院兰州化学物理研究所 一种柔性蒙皮及其制备方法和应用
CA3138153C (en) * 2021-01-28 2026-02-03 The Boeing Company Flat composite panel with tear arrestment and method of making the same
US11738851B2 (en) * 2021-09-17 2023-08-29 Blended Wing Aircraft, Inc. Systems and methods for modular aircraft
EP4554858A1 (de) * 2022-07-13 2025-05-21 Supernal, LLC An einer strukturellen säule montierter sitz und verfahren dafür
KR20240096158A (ko) * 2022-12-19 2024-06-26 현대자동차주식회사 충돌 하중 분산구조

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Also Published As

Publication number Publication date
EP1976751B1 (de) 2010-04-21
CN101360648B (zh) 2011-12-28
EP1976751A2 (de) 2008-10-08
CN101360648A (zh) 2009-02-04
US20130087657A9 (en) 2013-04-11
JP2009523655A (ja) 2009-06-25
DE602006013884D1 (de) 2010-06-02
US7766277B2 (en) 2010-08-03
US8434716B2 (en) 2013-05-07
US20070164159A1 (en) 2007-07-19
WO2007084227A3 (en) 2007-10-04
WO2007084227A2 (en) 2007-07-26
JP4804541B2 (ja) 2011-11-02
US20070164152A1 (en) 2007-07-19
US8398021B2 (en) 2013-03-19
US20110101164A1 (en) 2011-05-05

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