DE3684588D1 - Aerodynamische strukturen auf verbundwerkstoffen. - Google Patents

Aerodynamische strukturen auf verbundwerkstoffen.

Info

Publication number
DE3684588D1
DE3684588D1 DE8686201377T DE3684588T DE3684588D1 DE 3684588 D1 DE3684588 D1 DE 3684588D1 DE 8686201377 T DE8686201377 T DE 8686201377T DE 3684588 T DE3684588 T DE 3684588T DE 3684588 D1 DE3684588 D1 DE 3684588D1
Authority
DE
Germany
Prior art keywords
composites
aerodynamic structures
aerodynamic
structures
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
DE8686201377T
Other languages
English (en)
Inventor
James Hunt
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
Application granted granted Critical
Publication of DE3684588D1 publication Critical patent/DE3684588D1/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
    • B64C3/00—Wings
    • B64C3/20—Integral or sandwich constructions
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C3/00—Wings
    • B64C3/26—Construction, shape, or attachment of separate skins, e.g. panels
    • 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
    • Y10T428/00—Stock material or miscellaneous articles
    • Y10T428/24—Structurally defined web or sheet [e.g., overall dimension, etc.]
    • Y10T428/24058—Structurally defined web or sheet [e.g., overall dimension, etc.] including grain, strips, or filamentary elements in respective layers or components in angular relation
    • Y10T428/24124—Fibers

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Moulding By Coating Moulds (AREA)
  • Laminated Bodies (AREA)
DE8686201377T 1985-12-30 1986-08-04 Aerodynamische strukturen auf verbundwerkstoffen. Expired - Lifetime DE3684588D1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US06/814,383 US4741943A (en) 1985-12-30 1985-12-30 Aerodynamic structures of composite construction

Publications (1)

Publication Number Publication Date
DE3684588D1 true DE3684588D1 (de) 1992-04-30

Family

ID=25214905

Family Applications (1)

Application Number Title Priority Date Filing Date
DE8686201377T Expired - Lifetime DE3684588D1 (de) 1985-12-30 1986-08-04 Aerodynamische strukturen auf verbundwerkstoffen.

Country Status (4)

Country Link
US (1) US4741943A (de)
EP (1) EP0230682B1 (de)
JP (1) JP2665531B2 (de)
DE (1) DE3684588D1 (de)

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US7842145B2 (en) * 2004-10-05 2010-11-30 The Boeing Company Method for laying composite tape
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US20060237588A1 (en) * 2005-03-31 2006-10-26 The Boeing Company Composite structural member having an undulating web and method for forming the same
US7721495B2 (en) * 2005-03-31 2010-05-25 The Boeing Company Composite structural members and methods for forming the same
US8201371B2 (en) * 2005-03-31 2012-06-19 The Boeing Company Composite beam chord between reinforcement plates
US20060222837A1 (en) * 2005-03-31 2006-10-05 The Boeing Company Multi-axial laminate composite structures and methods of forming the same
US7740932B2 (en) * 2005-03-31 2010-06-22 The Boeing Company Hybrid fiberglass composite structures and methods of forming the same
US7748119B2 (en) * 2005-06-03 2010-07-06 The Boeing Company Method for manufacturing composite components
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US20070050104A1 (en) * 2005-08-24 2007-03-01 The Boeing Company Methods and systems for logistics health status reasoner
US20070052554A1 (en) * 2005-08-24 2007-03-08 The Boeing Company Methods and systems for logistics health status display
US8318291B2 (en) * 2005-09-07 2012-11-27 The Boeing Company Composite member defining a contour surface
US10086921B2 (en) * 2005-10-31 2018-10-02 The Boeing Company Aircraft having a forward-facing section that deflects elastically under impact loads
US7393184B2 (en) * 2005-11-10 2008-07-01 General Electric Company Modular blades and methods for making same
US7837148B2 (en) * 2006-06-13 2010-11-23 The Boeing Company Composite wing-body joint
EP1918193A1 (de) * 2006-10-31 2008-05-07 Airbus Espana, S.L. Integrierte Verbundhaut für Flugzeug-Midbox-Hebeoberflächen
US7849729B2 (en) 2006-12-22 2010-12-14 The Boeing Company Leak detection in vacuum bags
GB2447964B (en) * 2007-03-29 2012-07-18 Gurit Uk Ltd Moulding material
US8568551B2 (en) * 2007-05-22 2013-10-29 The Boeing Company Pre-patterned layup kit and method of manufacture
US9770871B2 (en) * 2007-05-22 2017-09-26 The Boeing Company Method and apparatus for layup placement
US8449709B2 (en) 2007-05-25 2013-05-28 The Boeing Company Method of fabricating fiber reinforced composite structure having stepped surface
ITTO20070557A1 (it) * 2007-07-27 2009-01-28 Alenia Aeronautica Spa Procedimento di fabbricazione di un elemento curvo in materiale composito
US8936695B2 (en) 2007-07-28 2015-01-20 The Boeing Company Method for forming and applying composite layups having complex geometries
US8333864B2 (en) * 2008-09-30 2012-12-18 The Boeing Company Compaction of prepreg plies on composite laminate structures
US8707766B2 (en) 2010-04-21 2014-04-29 The Boeing Company Leak detection in vacuum bags
US7851040B2 (en) * 2007-10-24 2010-12-14 Embraer - Empresa Brasileira De Aeronautica S.A. Methods for making composite material components especially useful for aircraft, and composite material components thereof
US8916010B2 (en) 2007-12-07 2014-12-23 The Boeing Company Composite manufacturing method
US8752293B2 (en) 2007-12-07 2014-06-17 The Boeing Company Method of fabricating structures using composite modules and structures made thereby
US9108718B2 (en) * 2009-10-08 2015-08-18 Mitsubishi Heavy Industries, Ltd. Composite-material structure and aircraft main wing and aircraft fuselage provided with the same
FR2956856A1 (fr) * 2010-02-26 2011-09-02 Eurocopter France Pale a vrillage adaptatif, et rotor muni d'une telle pale
US8348196B2 (en) * 2010-08-17 2013-01-08 The Boeing Company Multi-spar port box joint
ES2402463B1 (es) * 2010-11-30 2014-03-13 Airbus Operations, S.L. Un revestimiento de una superficie sustentadora de una aeronave.
JP5808111B2 (ja) 2011-02-04 2015-11-10 三菱重工業株式会社 航空機用複合材構造体、これを備えた航空機主翼および航空機胴体
JP5808112B2 (ja) 2011-02-04 2015-11-10 三菱重工業株式会社 複合材構造体およびこれを備えた航空機主翼
GB201103122D0 (en) * 2011-02-23 2011-04-06 Airbus Uk Ltd Composite structure
US9878773B2 (en) 2012-12-03 2018-01-30 The Boeing Company Split resistant composite laminate
US8973871B2 (en) * 2013-01-26 2015-03-10 The Boeing Company Box structures for carrying loads and methods of making the same
US10059429B2 (en) 2015-04-24 2018-08-28 The Boeing Company Embedded tear straps in metal structures
US10207789B2 (en) * 2016-08-16 2019-02-19 The Boeing Company Aircraft composite wingbox integration
US10745104B2 (en) * 2018-03-02 2020-08-18 The Boeing Company Stringer transition through a common base charge
US11932389B1 (en) * 2020-01-06 2024-03-19 United States Of America As Represented By The Secretary Of The Air Force Morphing airfoil
EP3922443A1 (de) * 2020-06-12 2021-12-15 Airbus Operations, S.L.U. Verbundstruktur und herstellungsverfahren
CA3138153A1 (en) * 2021-01-28 2022-07-28 The Boeing Company Flat composite panel with tear arrestment and method of making the same

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Also Published As

Publication number Publication date
JP2665531B2 (ja) 1997-10-22
EP0230682A2 (de) 1987-08-05
EP0230682B1 (de) 1992-03-25
JPS62157894A (ja) 1987-07-13
US4741943A (en) 1988-05-03
EP0230682A3 (en) 1989-03-15

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Legal Events

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8320 Willingness to grant licences declared (paragraph 23)