AU1822997A - Composite honeycomb sandwich structure - Google Patents

Composite honeycomb sandwich structure

Info

Publication number
AU1822997A
AU1822997A AU18229/97A AU1822997A AU1822997A AU 1822997 A AU1822997 A AU 1822997A AU 18229/97 A AU18229/97 A AU 18229/97A AU 1822997 A AU1822997 A AU 1822997A AU 1822997 A AU1822997 A AU 1822997A
Authority
AU
Australia
Prior art keywords
sandwich structure
honeycomb sandwich
composite honeycomb
composite
sandwich
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.)
Abandoned
Application number
AU18229/97A
Inventor
Darrell H. Corbett
Dave G. Erickson
Dale E. Hartz
William B. Hopkins
Christopher L. Pederson
Stuart A. Smith
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
Priority claimed from US08/587,160 external-priority patent/US5604010A/en
Priority claimed from US08/616,903 external-priority patent/US5895699A/en
Priority claimed from US08/620,829 external-priority patent/US5685940A/en
Application filed by Boeing Co filed Critical Boeing Co
Publication of AU1822997A publication Critical patent/AU1822997A/en
Abandoned legal-status Critical Current

Links

Classifications

    • G—PHYSICS
    • G10—MUSICAL INSTRUMENTS; ACOUSTICS
    • G10K—SOUND-PRODUCING DEVICES; METHODS OR DEVICES FOR PROTECTING AGAINST, OR FOR DAMPING, NOISE OR OTHER ACOUSTIC WAVES IN GENERAL; ACOUSTICS NOT OTHERWISE PROVIDED FOR
    • G10K11/00—Methods or devices for transmitting, conducting or directing sound in general; Methods or devices for protecting against, or for damping, noise or other acoustic waves in general
    • G10K11/16—Methods or devices for protecting against, or for damping, noise or other acoustic waves in general
    • G10K11/172—Methods or devices for protecting against, or for damping, noise or other acoustic waves in general using resonance effects
    • 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 form; Layered products 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 form; Layered products 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 form; Layered products 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
    • 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
AU18229/97A 1996-01-11 1997-01-06 Composite honeycomb sandwich structure Abandoned AU1822997A (en)

Applications Claiming Priority (7)

Application Number Priority Date Filing Date Title
US616903 1984-06-04
US587160 1996-01-11
US08/587,160 US5604010A (en) 1996-01-11 1996-01-11 Composite honeycomb sandwich structure
US08/616,903 US5895699A (en) 1996-03-15 1996-03-15 Tiedown ply for reducing core crush in composite honeycomb sandwich structure
US08/620,829 US5685940A (en) 1996-03-20 1996-03-20 Adhering tiedown plies in composite construction
US620829 1996-03-20
PCT/US1997/000075 WO1997025198A1 (en) 1996-01-11 1997-01-06 Composite honeycomb sandwich structure

Publications (1)

Publication Number Publication Date
AU1822997A true AU1822997A (en) 1997-08-01

Family

ID=27416496

Family Applications (1)

Application Number Title Priority Date Filing Date
AU18229/97A Abandoned AU1822997A (en) 1996-01-11 1997-01-06 Composite honeycomb sandwich structure

Country Status (5)

Country Link
EP (1) EP0883484A1 (en)
JP (2) JP3913275B2 (en)
CN (1) CN1101751C (en)
AU (1) AU1822997A (en)
WO (1) WO1997025198A1 (en)

Families Citing this family (27)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
BR9911045B1 (en) * 1998-05-22 2009-08-11 use of a stiffness-treated fabric, method for producing a stiffness-treated fabric, stiffness-treated fabric, use of a stiffness-treated fabric raw material, method for producing a stiffness-treated fabric raw material stiffness, use of a stiffness-treated prepreg layer, method for producing a stiffness-treated prepreg layer for a stiffness-treated honeycomb precursor, stiffness-treated honeycomb structure produce a stiffness-treated honeycomb precursor and method of producing a stiffness-treated honeycomb sandwich structure.
JP4663174B2 (en) 2001-08-03 2011-03-30 富士重工業株式会社 Method for forming honeycomb sandwich structure composite material
ATE406998T1 (en) 2003-07-08 2008-09-15 Airbus Gmbh LIGHTWEIGHT STRUCTURE
EP1495858B1 (en) 2003-07-08 2019-08-07 Airbus Operations GmbH Lightweight material structure made of metal composite material
JP2007098819A (en) * 2005-10-06 2007-04-19 Mitsubishi Rayon Co Ltd Manufacturing method of sandwich panel
FR2908737B1 (en) * 2006-11-16 2009-12-04 Airbus France ACOUSTIC COATING FOR AIRCRAFT INCORPORATING A JELLY EFFECT FROST TREATMENT SYSTEM.
US8046915B2 (en) * 2007-12-12 2011-11-01 General Electric Company Methods for making composite containment casings
US20090155524A1 (en) * 2007-12-13 2009-06-18 Rapp Robert A Composite panel and method of manufacturing the same
US8343298B2 (en) * 2007-12-13 2013-01-01 The Boeing Company Aircraft structures bonded with adhesive including magnetostrictive material
BE1017910A3 (en) 2007-12-21 2009-11-03 Sonaca Sociutu Anonyme METHOD FOR MANUFACTURING A PANEL COMPRISING AT LEAST ONE NANNED BODY AND A FIRST SKIN REALIZED IN COMPOSITE MATERIAL
US8491743B2 (en) * 2009-12-15 2013-07-23 The Boeing Company Composite ply stabilizing method
JP5619485B2 (en) * 2010-06-22 2014-11-05 豊和繊維工業株式会社 Laminated vehicle interior substrate and manufacturing method thereof
US8844873B2 (en) 2011-09-23 2014-09-30 The Boeing Company Stabilizer torque box assembly and method
FR2987307B1 (en) 2012-02-29 2017-02-10 Daher Aerospace METHOD AND DEVICE FOR THE COMPACTION AND CONSOLIDATION OF A HIGH THERMOPLASTIC DIE COMPOSITE PANEL
CN102700181B (en) * 2012-05-15 2014-09-03 西安交通大学 Light multifunctional composite structure
US9517594B2 (en) * 2012-10-04 2016-12-13 The Boeing Company Composite structure having a stabilizing element
CN102909899B (en) * 2012-10-25 2015-03-11 溧阳二十八所***装备有限公司 Production method for waterproof paper honeycomb compound sandwich board
CN103161391A (en) * 2013-03-07 2013-06-19 苏州市江诚人防设备有限公司 Inorganic protective door
EP3024642B1 (en) * 2013-07-26 2020-04-22 Learjet Inc. Composite material incorporating water ingress barrier
US9579875B2 (en) 2014-02-04 2017-02-28 The Boeing Company Bonded tab and tooling device
JP5992946B2 (en) * 2014-03-25 2016-09-14 富士重工業株式会社 Honeycomb structure and method for manufacturing honeycomb structure
CN105539809A (en) * 2014-10-28 2016-05-04 哈尔滨飞机工业集团有限责任公司 Sectional honeycomb sandwich structure
KR20190089880A (en) * 2016-10-27 2019-07-31 루아그 슈바이쯔 아게 Fabrication method of fiber reinforced polymer
JP7039401B2 (en) 2018-06-28 2022-03-22 三菱重工業株式会社 Composite material and method of curing composite material
JP7114367B2 (en) 2018-06-28 2022-08-08 三菱重工業株式会社 Forming method for composite structure
CN109159518A (en) * 2018-08-28 2019-01-08 丹阳丹金航空材料科技有限公司 A kind of aviation aircraft composite plate
CN111186147B (en) * 2020-02-24 2021-10-08 江苏亨睿碳纤维科技有限公司 Forming method for preparing lightweight automobile parts by using continuous fiber mixed chopped fibers

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CA985151A (en) * 1972-03-23 1976-03-09 Paul V. Oliva Honeycomb core structural panels
FR2198835B1 (en) * 1972-09-11 1975-03-07 Rhone Poulenc Ind
CA1239572A (en) * 1983-09-21 1988-07-26 Roger A. Stonier Method for cocuring a composite skin directly to honeycomb core
US4598007A (en) * 1985-02-28 1986-07-01 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Light weight fire resistant graphite composites
GB8817669D0 (en) * 1988-07-25 1988-09-01 Short Brothers Ltd Means for attenuating sound energy
US4954382A (en) * 1988-11-01 1990-09-04 American Cyanamid Company Interleaf layer in fiber reinforced resin laminate composites
FR2726500B1 (en) * 1994-11-09 1997-01-10 Eurocopter France PROCESS FOR PRODUCING COMPOSITE SANDWICH PANELS AND PANELS OBTAINED THEREBY

Also Published As

Publication number Publication date
JP2000502968A (en) 2000-03-14
CN1211947A (en) 1999-03-24
CN1101751C (en) 2003-02-19
JP2007015385A (en) 2007-01-25
JP3913275B2 (en) 2007-05-09
EP0883484A1 (en) 1998-12-16
WO1997025198A1 (en) 1997-07-17
JP4407964B2 (en) 2010-02-03

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