ATE396037T1 - Teilweise gefüllte wabenplatte - Google Patents

Teilweise gefüllte wabenplatte

Info

Publication number
ATE396037T1
ATE396037T1 AT04251623T AT04251623T ATE396037T1 AT E396037 T1 ATE396037 T1 AT E396037T1 AT 04251623 T AT04251623 T AT 04251623T AT 04251623 T AT04251623 T AT 04251623T AT E396037 T1 ATE396037 T1 AT E396037T1
Authority
AT
Austria
Prior art keywords
honeycomb core
skin
partially filled
honeycomb plate
cells
Prior art date
Application number
AT04251623T
Other languages
English (en)
Inventor
Chandrakant Himatlal Shah
Tod Palm
Timothy Alan Dyer
Carl A Reis
Original Assignee
Northrop Grumman Corp
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 Northrop Grumman Corp filed Critical Northrop Grumman Corp
Application granted granted Critical
Publication of ATE396037T1 publication Critical patent/ATE396037T1/de

Links

Classifications

    • 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
    • B32B3/10—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 a discontinuous layer, i.e. formed of separate pieces of material
    • B32B3/12—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 a discontinuous layer, i.e. formed of separate pieces of material characterised by a layer of regularly- arranged cells, e.g. a honeycomb structure
    • 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
    • B32B7/00—Layered products characterised by the relation between layers; Layered products characterised by the relative orientation of features between layers, or by the relative values of a measurable parameter between layers, i.e. products comprising layers having different physical, chemical or physicochemical properties; Layered products characterised by the interconnection of layers
    • B32B7/04—Interconnection of layers
    • B32B7/12—Interconnection of layers using interposed adhesives or interposed materials with bonding properties
    • 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
    • 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
    • B32B2305/00—Condition, form or state of the layers or laminate
    • B32B2305/02—Cellular or porous
    • B32B2305/028—Hollow fillers; Syntactic material
    • 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
    • B32B2305/00—Condition, form or state of the layers or laminate
    • B32B2305/30—Fillers, e.g. particles, powders, beads, flakes, spheres, chips
    • 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
    • Y10T428/23—Sheet including cover or casing
    • Y10T428/234—Sheet including cover or casing including elements cooperating to form cells
    • Y10T428/236—Honeycomb type cells extend perpendicularly to nonthickness layer
    • 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.]
    • Y10T428/24149—Honeycomb-like
    • Y10T428/24157—Filled honeycomb cells [e.g., solid substance in cavities, etc.]
    • 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
    • Y10T428/249921—Web or sheet containing structurally defined element or component
    • Y10T428/249953—Composite having voids in a component [e.g., porous, cellular, etc.]
    • Y10T428/249976—Voids specified as closed

Landscapes

  • Engineering & Computer Science (AREA)
  • Architecture (AREA)
  • Civil Engineering (AREA)
  • Structural Engineering (AREA)
  • Laminated Bodies (AREA)
  • Superstructure Of Vehicle (AREA)
  • Exhaust Gas After Treatment (AREA)
  • Superconductors And Manufacturing Methods Therefor (AREA)
  • Bending Of Plates, Rods, And Pipes (AREA)
AT04251623T 2003-06-12 2004-03-22 Teilweise gefüllte wabenplatte ATE396037T1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US10/461,178 US7048986B2 (en) 2003-06-12 2003-06-12 End gaps of filled honeycomb

Publications (1)

Publication Number Publication Date
ATE396037T1 true ATE396037T1 (de) 2008-06-15

Family

ID=33418102

Family Applications (1)

Application Number Title Priority Date Filing Date
AT04251623T ATE396037T1 (de) 2003-06-12 2004-03-22 Teilweise gefüllte wabenplatte

Country Status (9)

Country Link
US (2) US7048986B2 (de)
EP (1) EP1488919B1 (de)
JP (1) JP2005001374A (de)
AT (1) ATE396037T1 (de)
BR (1) BRPI0401752B8 (de)
CA (1) CA2459656A1 (de)
DE (1) DE602004013884D1 (de)
IL (1) IL161013A (de)
RU (1) RU2004110392A (de)

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US20080260992A1 (en) * 2005-06-08 2008-10-23 Kabushiki Kaisha Shizuka Sandwich Panel Including Honeycomb Structure Body and Method of Producing the Sandwich Panel
US8367183B2 (en) 2005-06-08 2013-02-05 Kabushiki Kaisha Shizuka Sandwich panel including honeycomb structure body and method of producing the sandwich panel
ES2298034B1 (es) * 2006-05-12 2009-02-01 Jesus Fco. Barberan Latorre Sistema de fabricacion de paneles con nido de abeja.
EP1914719B1 (de) * 2006-10-18 2010-05-26 Yamaha Corporation Schalldämpfender Körper
DE102007003275B4 (de) * 2007-01-23 2013-11-28 Airbus Operations Gmbh Schalenelement als Teil eines Flugzeugrumpfes
DE102007003277B4 (de) * 2007-01-23 2012-08-02 Airbus Operations Gmbh Rumpf eines Luft- oder Raumfahrzeuges in CFK-Metall Hybridbauweise mit einem Metallrahmen
US7842147B2 (en) * 2007-01-31 2010-11-30 M.C. Gill Corporation Composite panel having in-situ thermoset foamed core
US9783233B2 (en) * 2009-10-28 2017-10-10 Boulder Electric Vehicle Composite land vehicle frame
US10369772B2 (en) * 2012-07-10 2019-08-06 Textron Innovations Inc. Method of making core-stiffened structure
WO2013026489A1 (de) * 2011-08-25 2013-02-28 Inventio Ag Boden für eine aufzugskabine
US9096316B2 (en) * 2012-02-01 2015-08-04 Textron Innovations Inc. Optimized core for a structural assembly
US9015941B2 (en) 2012-10-30 2015-04-28 Bell Helicopter Textron Inc. Method of repairing honeycomb core using pourable structural foam
US9597826B2 (en) * 2012-10-30 2017-03-21 Bell Helicopter Textron Inc. Method of repairing, splicing, joining, machining, and stabilizing honeycomb core using pourable structural foam and a structure incorporating the same
US9149999B2 (en) 2012-10-30 2015-10-06 Bell Helicopter Textron Inc. Method of repairing, splicing, joining, machining, and stabilizing honeycomb core using pourable structural foam and a structure incorporating the same
US9333684B2 (en) 2012-10-30 2016-05-10 Bell Helicopter Textron Inc. Method of repairing, splicing, joining, machining, and stabilizing honeycomb core using pourable structural foam and a structure incorporating the same
US10018052B2 (en) 2012-12-28 2018-07-10 United Technologies Corporation Gas turbine engine component having engineered vascular structure
US10036258B2 (en) 2012-12-28 2018-07-31 United Technologies Corporation Gas turbine engine component having vascular engineered lattice structure
US10071537B2 (en) * 2013-12-06 2018-09-11 The Boeing Company Ceramic matrix composite component and method of forming thereof
JP6489399B2 (ja) * 2014-06-19 2019-03-27 キョーラク株式会社 樹脂製サンドイッチパネル
US10094287B2 (en) 2015-02-10 2018-10-09 United Technologies Corporation Gas turbine engine component with vascular cooling scheme
US10273935B2 (en) * 2016-01-15 2019-04-30 General Electric Company Rotor blades having structural skin insert and methods of making same
US10221694B2 (en) 2016-02-17 2019-03-05 United Technologies Corporation Gas turbine engine component having vascular engineered lattice structure
CN110418711B (zh) * 2017-03-13 2022-05-24 泽费罗斯股份有限公司 包括蜂窝芯和阻尼或衰减材料层的复合夹芯板
DE102017220331A1 (de) * 2017-11-15 2019-05-16 Siemens Aktiengesellschaft Verfahren zur Herstellung eines Sandwichelements und Sandwichelement
US10836502B2 (en) * 2017-12-15 2020-11-17 The Boeing Company Wave-shaped acoustic insert and core
US10774653B2 (en) 2018-12-11 2020-09-15 Raytheon Technologies Corporation Composite gas turbine engine component with lattice structure
CN109703731B (zh) * 2019-01-03 2021-02-05 北京空天技术研究所 缓冲结构、缓冲吸能回收装置及飞行器
US10751971B1 (en) * 2019-04-19 2020-08-25 Goodrich Corporation Edge damage tolerant heated and unheated composite panels with rotated honeycomb edge pieces
US20230011302A1 (en) * 2021-07-08 2023-01-12 The Boeing Company Foam sheet core for composite sandwich structures and method of making the same
JP7296537B2 (ja) * 2021-08-19 2023-06-23 株式会社グランツ ハニカムパネル
FR3131707B1 (fr) * 2022-01-13 2024-08-23 Safran Drapage d’une peau en matériau thermoplastique sur un corps multicellulaire

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Also Published As

Publication number Publication date
RU2004110392A (ru) 2005-10-20
IL161013A (en) 2006-08-01
DE602004013884D1 (de) 2008-07-03
BRPI0401752A (pt) 2005-01-25
BRPI0401752B1 (pt) 2014-09-23
US20040253407A1 (en) 2004-12-16
EP1488919B1 (de) 2008-05-21
BRPI0401752B8 (pt) 2014-10-29
US7048986B2 (en) 2006-05-23
CA2459656A1 (en) 2004-12-12
US20090205779A1 (en) 2009-08-20
EP1488919A1 (de) 2004-12-22
IL161013A0 (en) 2004-08-31
US7575650B1 (en) 2009-08-18
JP2005001374A (ja) 2005-01-06

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