IN2012DN06466A - - Google Patents

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Publication number
IN2012DN06466A
IN2012DN06466A IN6466DEN2012A IN2012DN06466A IN 2012DN06466 A IN2012DN06466 A IN 2012DN06466A IN 6466DEN2012 A IN6466DEN2012 A IN 6466DEN2012A IN 2012DN06466 A IN2012DN06466 A IN 2012DN06466A
Authority
IN
India
Prior art keywords
honeycomb core
attaching
stiffened structure
fitting
walls
Prior art date
Application number
Inventor
Carl A May
James D Hethcock
John R Mccullough
Ronald K Cox
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 IN2012DN06466A publication Critical patent/IN2012DN06466A/en

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16B—DEVICES FOR FASTENING OR SECURING CONSTRUCTIONAL ELEMENTS OR MACHINE PARTS TOGETHER, e.g. NAILS, BOLTS, CIRCLIPS, CLAMPS, CLIPS OR WEDGES; JOINTS OR JOINTING
    • F16B5/00—Joining sheets or plates, e.g. panels, to one another or to strips or bars parallel to them
    • F16B5/01—Joining sheets or plates, e.g. panels, to one another or to strips or bars parallel to them by means of fastening elements specially adapted for honeycomb panels
    • E—FIXED CONSTRUCTIONS
    • E04—BUILDING
    • E04C—STRUCTURAL ELEMENTS; BUILDING MATERIALS
    • E04C2/00—Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels
    • E04C2/30—Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels characterised by the shape or structure
    • E04C2/34—Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels characterised by the shape or structure composed of two or more spaced sheet-like parts
    • E04C2/36—Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels characterised by the shape or structure composed of two or more spaced sheet-like parts spaced apart by transversely-placed strip material, e.g. honeycomb panels
    • E04C2/365—Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels characterised by the shape or structure composed of two or more spaced sheet-like parts spaced apart by transversely-placed strip material, e.g. honeycomb panels by honeycomb structures
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16B—DEVICES FOR FASTENING OR SECURING CONSTRUCTIONAL ELEMENTS OR MACHINE PARTS TOGETHER, e.g. NAILS, BOLTS, CIRCLIPS, CLAMPS, CLIPS OR WEDGES; JOINTS OR JOINTING
    • F16B11/00—Connecting constructional elements or machine parts by sticking or pressing them together, e.g. cold pressure welding
    • F16B11/006—Connecting constructional elements or machine parts by sticking or pressing them together, e.g. cold pressure welding by gluing
    • 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
    • Y10T24/00—Buckles, buttons, clasps, etc.
    • Y10T24/33—Buckles, buttons, clasps, etc. having adhesive fastener

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Architecture (AREA)
  • Mechanical Engineering (AREA)
  • Civil Engineering (AREA)
  • Structural Engineering (AREA)
  • Laminated Bodies (AREA)
  • Connection Of Plates (AREA)
  • Insertion Pins And Rivets (AREA)

Abstract

An apparatus for attaching a member to a honeycomb core stiffened structure includes a body and one or more elements extending from the body configured to be adhesively bonded to one or more walls of a honeycomb core of the honeycomb core stiffened structure. The apparatus further includes a fitting for attaching the member to the apparatus. A honeycomb core stiffened structure includes a honeycomb core and an apparatus for attaching a member to the honeycomb core. The apparatus includes a body and one or more elements extending from the body configured to be adhesively bonded to one or more walls of the honeycomb core of the honeycomb core stiffened structure. The apparatus further includes a fitting for attaching the member to the apparatus.
IN6466DEN2012 2010-02-05 2011-02-02 IN2012DN06466A (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US30169210P 2010-02-05 2010-02-05
PCT/US2011/023455 WO2011097283A1 (en) 2010-02-05 2011-02-02 Apparatus for attaching a member to a core-stiffened structure and a combination thereof

Publications (1)

Publication Number Publication Date
IN2012DN06466A true IN2012DN06466A (en) 2015-10-09

Family

ID=44355751

Family Applications (1)

Application Number Title Priority Date Filing Date
IN6466DEN2012 IN2012DN06466A (en) 2010-02-05 2011-02-02

Country Status (6)

Country Link
US (2) US9175474B2 (en)
EP (1) EP2531665B1 (en)
CN (1) CN102753767B (en)
CA (1) CA2787421C (en)
IN (1) IN2012DN06466A (en)
WO (1) WO2011097283A1 (en)

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US9145277B2 (en) 2013-03-01 2015-09-29 Bell Helicopter Textron Inc. System and method of manufacturing composite core
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US10195836B2 (en) * 2017-01-18 2019-02-05 The Boeing Company Splices comprising honeycomb cores supported by tie clips and methods of forming thereof
US10746215B2 (en) * 2017-05-05 2020-08-18 The Boeing Company Blade-and-slot joints that unite composite panels via internal blades
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DE102017213501A1 (en) * 2017-08-03 2019-02-07 Lufthansa Technik Ag Sandwich structure with recessed connecting element
US11059559B2 (en) 2018-03-05 2021-07-13 General Electric Company Acoustic liners with oblique cellular structures
US11047304B2 (en) 2018-08-08 2021-06-29 General Electric Company Acoustic cores with sound-attenuating protuberances
US10823059B2 (en) 2018-10-03 2020-11-03 General Electric Company Acoustic core assemblies with mechanically joined acoustic core segments, and methods of mechanically joining acoustic core segments
US11434819B2 (en) 2019-03-29 2022-09-06 General Electric Company Acoustic liners with enhanced acoustic absorption and reduced drag characteristics
US11732740B2 (en) 2020-05-12 2023-08-22 Sky Climber Fasteners LLC Blind fastener
CN212643246U (en) * 2020-06-11 2021-03-02 刘劲松 Invisible connecting piece and connecting structure
EP4182576A4 (en) 2020-07-20 2024-08-07 Sky Climber Fasteners LLC RIVETLESS NUT PLATE
US11668236B2 (en) 2020-07-24 2023-06-06 General Electric Company Acoustic liners with low-frequency sound wave attenuating features
CN112064808B (en) * 2020-09-30 2025-06-24 吴兆圣 Building deformation joint waterproofing system and method with adhesive built-in water stop structure
US11970992B2 (en) 2021-06-03 2024-04-30 General Electric Company Acoustic cores and tools and methods for forming the same
WO2023014964A1 (en) 2021-08-06 2023-02-09 Sky Climber Fasteners LLC Panel fastener
US12142253B2 (en) 2021-10-05 2024-11-12 General Electric Company Solid adhesive film for acoustic liner and method
US11965425B2 (en) 2022-05-31 2024-04-23 General Electric Company Airfoil for a turbofan engine
US12312969B2 (en) 2023-01-17 2025-05-27 General Electric Company Airfoils for turbofan engines

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JP5176211B2 (en) * 2008-12-25 2013-04-03 ポップリベット・ファスナー株式会社 Spacer clip

Also Published As

Publication number Publication date
WO2011097283A1 (en) 2011-08-11
US9175474B2 (en) 2015-11-03
CN102753767B (en) 2014-10-22
CA2787421A1 (en) 2011-08-11
US10180151B2 (en) 2019-01-15
EP2531665A1 (en) 2012-12-12
EP2531665B1 (en) 2015-08-26
EP2531665A4 (en) 2014-01-08
CA2787421C (en) 2014-12-30
US20160053785A1 (en) 2016-02-25
CN102753767A (en) 2012-10-24
US20120284970A1 (en) 2012-11-15

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