NO914011L - NON-GRAPHITE-CONTAINING, ANT ignition-resistant structures - Google Patents

NON-GRAPHITE-CONTAINING, ANT ignition-resistant structures

Info

Publication number
NO914011L
NO914011L NO91914011A NO914011A NO914011L NO 914011 L NO914011 L NO 914011L NO 91914011 A NO91914011 A NO 91914011A NO 914011 A NO914011 A NO 914011A NO 914011 L NO914011 L NO 914011L
Authority
NO
Norway
Prior art keywords
linear
opposite side
ant
ignition
graphite
Prior art date
Application number
NO91914011A
Other languages
Norwegian (no)
Other versions
NO914011D0 (en
Inventor
Jr Francis P Mccullough
R Vernon Snelgrove
David M Hall
Original Assignee
Dow Chemical 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 US07/479,828 external-priority patent/US5024877A/en
Application filed by Dow Chemical Co filed Critical Dow Chemical Co
Publication of NO914011D0 publication Critical patent/NO914011D0/en
Publication of NO914011L publication Critical patent/NO914011L/en

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Landscapes

  • Laminated Bodies (AREA)

Abstract

En struktur (20) som er særlig egnet for anvendelse som fly-innerpanel og omfattende minst én polymermatrise (24) innbefattende 20 - 50 vekt-% ikke-lineære, karbonholdige fibre og 50 - 80 vekt-% organosilikonpolymer. Strukturen er dannet ved varme- og trykkoverf«ring. På en sideflate av strukturen kan det festes en polyraerfilm (22) fortrinnsvis en polyesterfilm. Filmen kan med fordel være utstyrt med en dekorativ innpregning (21). På den motsatte side av matrisen (24) kan det anbringes et forsterknings-strymateriale (25).Et lag av ulligneride dun (26) av ikke-lineære og/eller lineære, karbonholdige fibre kan anordnes på den motsatte side av strymaterialet (25) ved ønske om varme- og lydisolasjon. Den motsatte side av dunet (26) kan med fordel være belagt med en film eller sjikt (28) av et metall- eller polymermateriale e.l.A structure (20) which is particularly suitable for use as an aircraft inner panel and comprising at least one polymer matrix (24) comprising 20-50% by weight of non-linear carbonaceous fibers and 50-80% by weight of organosilicone polymer. The structure is formed by heat and pressure transfer. A polyester film (22), preferably a polyester film, can be attached to a side surface of the structure. The film may advantageously be provided with a decorative embossing (21). On the opposite side of the matrix (24) a reinforcing spreading material (25) can be arranged. A layer of non-linear down (26) of non-linear and / or linear, carbonaceous fibers can be arranged on the opposite side of the spreading material (25). if desired for heat and sound insulation. The opposite side of the down (26) may advantageously be coated with a film or layer (28) of a metal or polymeric material or the like.

NO91914011A 1989-04-14 1991-10-11 NON-GRAPHITE-CONTAINING, ANT ignition-resistant structures NO914011L (en)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US33791289A 1989-04-14 1989-04-14
US07/479,828 US5024877A (en) 1989-04-14 1990-02-14 Fire resistant materials
PCT/US1990/001582 WO1990012686A1 (en) 1989-04-14 1990-03-20 Nongraphitic ignition resistant structures

Publications (2)

Publication Number Publication Date
NO914011D0 NO914011D0 (en) 1991-10-11
NO914011L true NO914011L (en) 1991-12-11

Family

ID=27376407

Family Applications (1)

Application Number Title Priority Date Filing Date
NO91914011A NO914011L (en) 1989-04-14 1991-10-11 NON-GRAPHITE-CONTAINING, ANT ignition-resistant structures

Country Status (1)

Country Link
NO (1) NO914011L (en)

Also Published As

Publication number Publication date
NO914011D0 (en) 1991-10-11

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