DE602006013884D1 - Verformbarer vorderer druckspant für ein flugzeug - Google Patents

Verformbarer vorderer druckspant für ein flugzeug

Info

Publication number
DE602006013884D1
DE602006013884D1 DE602006013884T DE602006013884T DE602006013884D1 DE 602006013884 D1 DE602006013884 D1 DE 602006013884D1 DE 602006013884 T DE602006013884 T DE 602006013884T DE 602006013884 T DE602006013884 T DE 602006013884T DE 602006013884 D1 DE602006013884 D1 DE 602006013884D1
Authority
DE
Germany
Prior art keywords
dome
crown panel
bulkhead
deformable
birds
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.)
Active
Application number
DE602006013884T
Other languages
English (en)
Inventor
Barney B Anderson
Jeffrey R Swada
William J Koch
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Boeing Co
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
Publication of DE602006013884D1 publication Critical patent/DE602006013884D1/de
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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)
  • Catching Or Destruction (AREA)
  • Measuring Pulse, Heart Rate, Blood Pressure Or Blood Flow (AREA)
  • Finger-Pressure Massage (AREA)
  • Pressure Vessels And Lids Thereof (AREA)
DE602006013884T 2006-01-19 2006-12-13 Verformbarer vorderer druckspant für ein flugzeug Active DE602006013884D1 (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
DE602006013884D1 true DE602006013884D1 (de) 2010-06-02

Family

ID=38191126

Family Applications (1)

Application Number Title Priority Date Filing Date
DE602006013884T Active DE602006013884D1 (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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DE102006029231B4 (de) * 2006-06-26 2013-09-26 Airbus Operations Gmbh Druckschott für einen Rumpf für die Luft- und Raumfahrt
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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
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US20100155533A1 (en) * 2008-12-23 2010-06-24 Spirit Aerosystems, Inc. Composite forward pressure bulkhead
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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
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EP2675711B1 (de) 2011-02-18 2016-06-22 Airbus Operations Zentraler pylon für ein flugzeugcockpit und flugzeug mit einem solchen pylon
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CN103843475B (zh) * 2011-09-30 2016-10-26 空中客车运营简化股份公司 航空器的电力中枢
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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
EP3095689B1 (de) 2015-05-20 2017-10-04 Airbus Operations GmbH Druckschott für einen flugzeugrumpf
EP3095688B1 (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
US11738851B2 (en) * 2021-09-17 2023-08-29 Blended Wing Aircraft, Inc. Systems and methods for modular aircraft

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Also Published As

Publication number Publication date
CN101360648A (zh) 2009-02-04
WO2007084227A2 (en) 2007-07-26
EP1976751B1 (de) 2010-04-21
US7766277B2 (en) 2010-08-03
JP4804541B2 (ja) 2011-11-02
ATE465081T1 (de) 2010-05-15
WO2007084227A3 (en) 2007-10-04
JP2009523655A (ja) 2009-06-25
US20130087657A9 (en) 2013-04-11
EP1976751A2 (de) 2008-10-08
US20070164152A1 (en) 2007-07-19
CN101360648B (zh) 2011-12-28
US20110101164A1 (en) 2011-05-05
US8434716B2 (en) 2013-05-07
US20070164159A1 (en) 2007-07-19
US8398021B2 (en) 2013-03-19

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