DE602004032122D1 - Kontaktversteifer für konstruktionshaut - Google Patents

Kontaktversteifer für konstruktionshaut

Info

Publication number
DE602004032122D1
DE602004032122D1 DE602004032122T DE602004032122T DE602004032122D1 DE 602004032122 D1 DE602004032122 D1 DE 602004032122D1 DE 602004032122 T DE602004032122 T DE 602004032122T DE 602004032122 T DE602004032122 T DE 602004032122T DE 602004032122 D1 DE602004032122 D1 DE 602004032122D1
Authority
DE
Germany
Prior art keywords
contact maker
construction skin
skin
construction
maker
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 - Lifetime
Application number
DE602004032122T
Other languages
English (en)
Inventor
James Donn Hethcock
Rodney H Jones
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.)
Bell Helicopter Textron Inc
Original Assignee
Bell Helicopter Textron Inc
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 Bell Helicopter Textron Inc filed Critical Bell Helicopter Textron Inc
Publication of DE602004032122D1 publication Critical patent/DE602004032122D1/de
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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
    • B64C1/068—Fuselage sections
    • 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
    • B64C3/00—Wings
    • B64C3/18—Spars; Ribs; Stringers
    • 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)
  • Rod-Shaped Construction Members (AREA)
  • Connection Of Plates (AREA)
  • Building Environments (AREA)
DE602004032122T 2003-02-24 2004-02-24 Kontaktversteifer für konstruktionshaut Expired - Lifetime DE602004032122D1 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US45009603P 2003-02-24 2003-02-24
PCT/US2004/005585 WO2004076769A2 (en) 2003-02-24 2004-02-24 Contact stiffeners for structural skins

Publications (1)

Publication Number Publication Date
DE602004032122D1 true DE602004032122D1 (de) 2011-05-19

Family

ID=32927611

Family Applications (2)

Application Number Title Priority Date Filing Date
DE602004032122T Expired - Lifetime DE602004032122D1 (de) 2003-02-24 2004-02-24 Kontaktversteifer für konstruktionshaut
DE04714198T Active DE04714198T8 (de) 2003-02-24 2004-02-24 Kontaktversteifer für konstruktionshaut

Family Applications After (1)

Application Number Title Priority Date Filing Date
DE04714198T Active DE04714198T8 (de) 2003-02-24 2004-02-24 Kontaktversteifer für konstruktionshaut

Country Status (7)

Country Link
US (2) US8156711B2 (de)
EP (1) EP1616061B1 (de)
CN (1) CN100434634C (de)
BR (1) BRPI0407749A (de)
CA (1) CA2515149C (de)
DE (2) DE602004032122D1 (de)
WO (1) WO2004076769A2 (de)

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US9308988B2 (en) 2013-01-16 2016-04-12 Otto Aviation Group Aircraft main landing gear and method of operating the same
US9669939B2 (en) 2013-01-16 2017-06-06 Otto Aviation Group Aircraft supplemental thrust device and method of operating the same
DE102013102812B4 (de) * 2013-03-19 2017-01-26 Airbus Operations Gmbh Rumpfstruktur für ein Verkehrsmittel, Verkehrsmittel und Verfahren zum Herstellen einer Rumpfstruktur für ein Verkehrsmittel
US9674899B2 (en) * 2013-06-04 2017-06-06 The Boeing Company Shim manufacturing system
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DE102014103438A1 (de) * 2013-07-16 2015-01-22 Airbus Operations Gmbh Spritzgussverfahren zur Herstellung eines Primärstrukturverbindungselements
FR3015426B1 (fr) * 2013-12-20 2017-10-27 Airbus Operations Sas Procede de realisation d'un caisson central de voilure
US9399507B2 (en) 2014-01-22 2016-07-26 The Boeing Company Joints between a composite skin and a load-bearing component and methods of forming same
US9719490B2 (en) * 2014-10-31 2017-08-01 General Electric Company Wind turbine blade with bond paste inspection window and associated method
EP3112256B1 (de) * 2015-07-03 2018-03-14 Airbus Operations, S.L. Flugzeugaussenteil mit aufblasbaren platten
US10479477B2 (en) 2016-02-08 2019-11-19 Bell Helicopter Textron Inc. Engagement member for splicing a spar assembly
US10399285B2 (en) 2016-02-08 2019-09-03 Bell Helicopter Textron Inc. Composite wing structure and methods of manufacture
US10513324B2 (en) 2016-02-08 2019-12-24 Bell Helicopter Textron Inc. Composite rib assembly
EP3272640B1 (de) 2016-07-21 2019-04-17 AIRBUS HELICOPTERS DEUTSCHLAND GmbH Hubschrauber mit einem rumpf und einem verbundstoffheckausleger
EP3556650A4 (de) * 2016-12-16 2020-08-19 Manuel Torres Martinez Verfahren zur herstellung verstärkter schalenbaustrukturen und erhaltene struktur
US10597134B2 (en) * 2017-02-20 2020-03-24 Textron Innovations Inc. Adhesive joints for aircraft
CN107747578B (zh) * 2017-10-13 2020-12-25 重庆大学 一种多层级点阵夹芯圆柱
CN109774911B (zh) * 2017-11-10 2023-08-22 南京未来正客企业管理有限公司 囊体与加强筋的连接方法及气囊及浮空器
US11433990B2 (en) * 2018-07-09 2022-09-06 Rohr, Inc. Active laminar flow control system with composite panel
CN109305328B (zh) * 2018-11-12 2024-01-16 中国商用飞机有限责任公司北京民用飞机技术研究中心 一种翼盒及飞机
US11161592B2 (en) 2019-09-11 2021-11-02 Textron Innovations Inc. Torque box sleeves for aircraft wing assemblies
EP3805091B1 (de) 2019-10-08 2021-08-25 AIRBUS HELICOPTERS DEUTSCHLAND GmbH Schott für einen ausleger eines flugzeugs
US11591061B2 (en) 2020-12-02 2023-02-28 Airbus Helicopters Deutschland GmbH Watertight bulkhead for a boom of an aircraft
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Also Published As

Publication number Publication date
CA2515149C (en) 2011-01-11
CN100434634C (zh) 2008-11-19
EP1616061B1 (de) 2011-04-06
EP1616061A4 (de) 2009-04-29
US8632712B2 (en) 2014-01-21
WO2004076769A3 (en) 2006-05-11
BRPI0407749A (pt) 2006-02-14
EP1616061A2 (de) 2006-01-18
WO2004076769A2 (en) 2004-09-10
CA2515149A1 (en) 2004-09-10
DE04714198T8 (de) 2007-06-06
US20120199269A1 (en) 2012-08-09
DE04714198T1 (de) 2006-12-28
CN1826451A (zh) 2006-08-30
US20070011970A1 (en) 2007-01-18
US8156711B2 (en) 2012-04-17

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