JPS6478946A - Interior fitting material - Google Patents

Interior fitting material

Info

Publication number
JPS6478946A
JPS6478946A JP62232390A JP23239087A JPS6478946A JP S6478946 A JPS6478946 A JP S6478946A JP 62232390 A JP62232390 A JP 62232390A JP 23239087 A JP23239087 A JP 23239087A JP S6478946 A JPS6478946 A JP S6478946A
Authority
JP
Japan
Prior art keywords
prepregs
interior fitting
flame
decola
thermohardening
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.)
Pending
Application number
JP62232390A
Other languages
Japanese (ja)
Inventor
Akira Koizumi
Yuuji Itou
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.)
Yokohama Rubber Co Ltd
Original Assignee
Yokohama Rubber Co Ltd
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 Yokohama Rubber Co Ltd filed Critical Yokohama Rubber Co Ltd
Priority to JP62232390A priority Critical patent/JPS6478946A/en
Publication of JPS6478946A publication Critical patent/JPS6478946A/en
Pending legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B60VEHICLES IN GENERAL
    • B60RVEHICLES, VEHICLE FITTINGS, OR VEHICLE PARTS, NOT OTHERWISE PROVIDED FOR
    • B60R13/00Elements for body-finishing, identifying, or decorating; Arrangements or adaptations for advertising purposes
    • B60R13/02Internal Trim mouldings ; Internal Ledges; Wall liners for passenger compartments; Roof liners

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Laminated Bodies (AREA)
  • Vehicle Interior And Exterior Ornaments, Soundproofing, And Insulation (AREA)

Abstract

PURPOSE:To prevent penetration of flame by interposing an inorganic liner between thermohardening fiber reinforced prepregs. of an interior fitting for airplane formed by laminating the prepregs. plus DECOLA sheets over and under a honeycomb core. CONSTITUTION:An interior fitting for airplane is formed from thermohardening fiber reinforced prepregs. 2a, 2b of epoxy resin etc., and DECOLA sheets 3a, 3b, which are laminated over and under a honeycomb core 1 in a sandwich structure. Flame penetration preventive layers 4a, 4b in the form of sheet are interposed between these prepregs. 2a, 2b, and they are formed into a single body. These flame penetration preventive layers are made from metal material (foil of aluminum, titanium, etc.) and inorganic liner (sheet of ceramic, mica, etc.). This conforms to the new U.S. specifications for combustion tests (FAA).
JP62232390A 1987-09-18 1987-09-18 Interior fitting material Pending JPS6478946A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP62232390A JPS6478946A (en) 1987-09-18 1987-09-18 Interior fitting material

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP62232390A JPS6478946A (en) 1987-09-18 1987-09-18 Interior fitting material

Publications (1)

Publication Number Publication Date
JPS6478946A true JPS6478946A (en) 1989-03-24

Family

ID=16938489

Family Applications (1)

Application Number Title Priority Date Filing Date
JP62232390A Pending JPS6478946A (en) 1987-09-18 1987-09-18 Interior fitting material

Country Status (1)

Country Link
JP (1) JPS6478946A (en)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102009050787A1 (en) * 2009-10-27 2011-05-05 Airbus Operations Gmbh Use of inorganic particles to produce a barrier on aircraft components
CN102241166A (en) * 2011-04-15 2011-11-16 天津全华时代航天科技发展有限公司 Special-purposed cellular composite material used for small unmanned air vehicle
JP2017104493A (en) * 2015-08-27 2017-06-15 ザ・ボーイング・カンパニーThe Boeing Company Method, system and apparatus for lining aircraft cargo compartment
US11370144B2 (en) 2019-10-08 2022-06-28 Goodrich Corporation Method and system for sequencing veneer to lumbercore
JP2023090668A (en) * 2021-12-17 2023-06-29 上緯新材料科技股▲フン▼有限公司 Highly flame-retardant laminated composite material and method for preparing the same

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102009050787A1 (en) * 2009-10-27 2011-05-05 Airbus Operations Gmbh Use of inorganic particles to produce a barrier on aircraft components
US10723853B2 (en) 2009-10-27 2020-07-28 Airbus Operations Gmbh Use of inorganic particles to produce a barrier layer on aircraft components
CN102241166A (en) * 2011-04-15 2011-11-16 天津全华时代航天科技发展有限公司 Special-purposed cellular composite material used for small unmanned air vehicle
JP2017104493A (en) * 2015-08-27 2017-06-15 ザ・ボーイング・カンパニーThe Boeing Company Method, system and apparatus for lining aircraft cargo compartment
US11370144B2 (en) 2019-10-08 2022-06-28 Goodrich Corporation Method and system for sequencing veneer to lumbercore
JP2023090668A (en) * 2021-12-17 2023-06-29 上緯新材料科技股▲フン▼有限公司 Highly flame-retardant laminated composite material and method for preparing the same

Similar Documents

Publication Publication Date Title
US4687691A (en) Honeycomb spliced multilayer foam core aircraft composite parts and method for making same
GB1446335A (en) Thermal insulation
CA2175523A1 (en) Multi-layered, unbalanced sandwich panel
TW371285B (en) Foiled UD-prepreg and PWB laminate prepared therefrom
MY101241A (en) Corrugated paper board.
EP1614531A3 (en) Titanium-polymer hybrid laminates
WO1982000974A1 (en) Hybrid composite structures
DE3760904D1 (en) Composite blade with a double spar and torsional box and with a honeycomb sandwich layered coating, and production process
ATE78225T1 (en) COMPOSITE LAMINATE OF METAL LAYERS AND PLASTIC LAYERS REINFORCED WITH CONTINUOUS THREADS.
EP0136673A3 (en) Stampable sheets of bonded laminate of metal sheet and fiber mat reinforced poly(arylene sulfide) and method of preparation using radio frequency energy
GB2281545B (en) Aircraft wings
CA2473346A1 (en) Lightweight structure particularly for aircraft
GB1265835A (en)
JPS6478946A (en) Interior fitting material
EP0078174A3 (en) Process for producing metal/thermoplastic resin/metal sandwich laminate
GB2238283B (en) The protection of aircraft structures
EP1701881B1 (en) Aircraft fuselage
PALM Impact resistance and residual compression strength of composite sandwich panels
Wong Sandwich construction in the Starship
JPS53108182A (en) Laminated composite
HOOPER Starship- A model for future designs
JPS64129A (en) Interleaf-containing, fiber-reinforced epoxy resin prepreg material
GB2185438B (en) Liner material
FUKUNAGA Stiffness and/or strength optimization of laminated composites
Eschke et al. Shearing Stability of Rectangular Sandwich Plates With a Soft Core of Any Thickness