TR201900901T4 - Kompozit yapısal paneller ve hava aracı gövdeleri. - Google Patents

Kompozit yapısal paneller ve hava aracı gövdeleri. Download PDF

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Publication number
TR201900901T4
TR201900901T4 TR2019/00901T TR201900901T TR201900901T4 TR 201900901 T4 TR201900901 T4 TR 201900901T4 TR 2019/00901 T TR2019/00901 T TR 2019/00901T TR 201900901 T TR201900901 T TR 201900901T TR 201900901 T4 TR201900901 T4 TR 201900901T4
Authority
TR
Turkey
Prior art keywords
shell
composite structural
structural panels
aircraft bodies
mating
Prior art date
Application number
TR2019/00901T
Other languages
English (en)
Inventor
Cardin Rachel
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 TR201900901T4 publication Critical patent/TR201900901T4/tr

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
    • 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
    • B64C1/08—Geodetic or other open-frame structures
    • 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
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29D—PRODUCING PARTICULAR ARTICLES FROM PLASTICS OR FROM SUBSTANCES IN A PLASTIC STATE
    • B29D99/00—Subject matter not provided for in other groups of this subclass
    • B29D99/001—Producing wall or panel-like structures, e.g. for hulls, fuselages, or buildings
    • 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
    • B64C1/069—Joining arrangements therefor
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B3/00—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form
    • B32B3/02—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form characterised by features of form at particular places, e.g. in edge regions
    • B32B3/06—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form characterised by features of form at particular places, e.g. in edge regions for securing layers together; for attaching the product to another member, e.g. to a support, or to another product, e.g. groove/tongue, interlocking
    • 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
    • B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
    • B64F5/00—Designing, manufacturing, assembling, cleaning, maintaining or repairing aircraft, not otherwise provided for; Handling, transporting, testing or inspecting aircraft components, not otherwise provided for
    • 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
    • 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
    • Y10T29/00—Metal working
    • Y10T29/49—Method of mechanical manufacture
    • Y10T29/49616—Structural member making
    • Y10T29/49622—Vehicular structural member making
    • 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
    • Y10T428/19—Sheets or webs edge spliced or joined
    • Y10T428/192—Sheets or webs coplanar

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Architecture (AREA)
  • Civil Engineering (AREA)
  • Structural Engineering (AREA)
  • Lining Or Joining Of Plastics Or The Like (AREA)
  • Standing Axle, Rod, Or Tube Structures Coupled By Welding, Adhesion, Or Deposition (AREA)
  • Laminated Bodies (AREA)
  • Connection Of Plates (AREA)
  • Moulding By Coating Moulds (AREA)
  • Pressure Welding/Diffusion-Bonding (AREA)
  • Vehicle Interior And Exterior Ornaments, Soundproofing, And Insulation (AREA)

Abstract

Buluş, bir hava aracı gövde düzeneği (100) ile ilgili olup, aşağıdakileri içerir: her biri ayrıca bir eşleşme kenarına sahip olan ve çok sayıda kompozit malzeme katmanı içeren birinci (112) ve ikinci (114) kabuk bölümleri, burada eşleşme kenarları (116, 118), birbiri ile kenar hattı hizalaması halinde yerleştirilmiştir; her biri ikinci kabuk (114) bölümünün iç yüzeyi boyunca birinci kabuk (112) bölümünün eşleşme kenarından (116) uzunlamasına olarak uzanan çok sayıda tırnak (120), burada her bir tırnak (120), ikinci kabuk (114) bölümünün iç yüzeyinin (132) karşılık kısımları ile yüz yüze örtüşme durumunda bir dış yüzey (124) içermekte olup, söz konusu tırnakların (120) her biri ayrıca birinci (112) ve ikinci (114) kabuk bölümlerinin birleştirilmesi için söz konusu dış yüzey (124) ve söz konusu karşılık kısmı arasına yapıştırma malzemesinin (140) enjekte edilmesi için oluşturulmuş en az bir enjeksiyon deliği (142) içerir.
TR2019/00901T 2012-06-20 2013-06-11 Kompozit yapısal paneller ve hava aracı gövdeleri. TR201900901T4 (tr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US13/528,553 US8985514B2 (en) 2012-06-20 2012-06-20 Composite structural panels and aircraft fuselages

Publications (1)

Publication Number Publication Date
TR201900901T4 true TR201900901T4 (tr) 2019-02-21

Family

ID=48747303

Family Applications (1)

Application Number Title Priority Date Filing Date
TR2019/00901T TR201900901T4 (tr) 2012-06-20 2013-06-11 Kompozit yapısal paneller ve hava aracı gövdeleri.

Country Status (11)

Country Link
US (1) US8985514B2 (tr)
EP (1) EP2676877B1 (tr)
JP (1) JP6255172B2 (tr)
KR (1) KR102022727B1 (tr)
CN (1) CN103507942B (tr)
AU (1) AU2013205455B2 (tr)
BR (1) BR102013015047B1 (tr)
CA (1) CA2815489C (tr)
ES (1) ES2715841T3 (tr)
RU (1) RU2634853C2 (tr)
TR (1) TR201900901T4 (tr)

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* Cited by examiner, † Cited by third party
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US7325771B2 (en) * 2004-09-23 2008-02-05 The Boeing Company Splice joints for composite aircraft fuselages and other structures
US9303671B2 (en) * 2013-01-15 2016-04-05 GM Global Technology Operations LLC Method of isolating metallic fasteners in composite panels
US9415853B2 (en) * 2013-01-30 2016-08-16 The Boeing Company Surface sealing system
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
US9579875B2 (en) * 2014-02-04 2017-02-28 The Boeing Company Bonded tab and tooling device
US10864999B1 (en) 2019-07-18 2020-12-15 QMI, Inc. Cessna tail-cone reinforcement angle splice, installation kit, and method for installation thereof
FR3099915A1 (fr) * 2019-08-13 2021-02-19 Airbus Operations Partie antérieure de nacelle d’un ensemble propulsif d’aéronef dont la lèvre d’entrée d’air est liée au panneau extérieur par emboitement
US11851213B1 (en) * 2022-10-14 2023-12-26 The Boeing Company Methods and structural gap filler for one-up assembly

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US3885071A (en) * 1972-08-10 1975-05-20 Lockheed Aircraft Corp Fiber-reinforced epoxy composite joints
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GB9508065D0 (en) * 1995-04-20 1995-06-07 Saf T Glo Ltd Emergency lighting
US6374570B1 (en) * 2000-08-25 2002-04-23 Lockheed Martin Corporation Apparatus and method for joining dissimilar materials to form a structural support member
US6582539B2 (en) * 2001-06-08 2003-06-24 Lockheed Martin Corporation Method for making large composite structures without use of an autoclave
US7527222B2 (en) 2004-04-06 2009-05-05 The Boeing Company Composite barrel sections for aircraft fuselages and other structures, and methods and systems for manufacturing such barrel sections
US7325771B2 (en) * 2004-09-23 2008-02-05 The Boeing Company Splice joints for composite aircraft fuselages and other structures
DE102005033992B3 (de) * 2005-07-21 2007-04-19 Airbus Deutschland Gmbh Verfahren zum Verbinden von mindestens zwei Flächengebilden, insbesondere von mindestens zwei Metallblechen für eine Leichtbaustruktur sowie Verbindung und Leichtbaustruktur
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Also Published As

Publication number Publication date
US8985514B2 (en) 2015-03-24
JP2014159262A (ja) 2014-09-04
EP2676877B1 (en) 2018-12-19
KR102022727B1 (ko) 2019-09-18
KR20130142903A (ko) 2013-12-30
CA2815489A1 (en) 2013-12-20
CN103507942A (zh) 2014-01-15
JP6255172B2 (ja) 2017-12-27
EP2676877A2 (en) 2013-12-25
AU2013205455A1 (en) 2014-01-16
CN103507942B (zh) 2017-05-17
US20140224932A1 (en) 2014-08-14
RU2013127785A (ru) 2014-12-27
EP2676877A3 (en) 2017-11-01
ES2715841T3 (es) 2019-06-06
AU2013205455B2 (en) 2016-12-08
BR102013015047B1 (pt) 2021-10-13
RU2634853C2 (ru) 2017-11-07
CA2815489C (en) 2016-08-30
BR102013015047A2 (pt) 2015-06-23

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