Laminated safety pane for aircraft
First Claim
Patent Images
1. A laminated safety pane for aircraft, comprising:
- a laminate of at least two bonded glass sheets, at least one of which sheets is chemically toughened and which is the glass sheet which faces the interior of the cabin, wherein a surface of said chemically toughened glass sheet is bonded by a plastic material selected from the group consisting of (i) a polyvinyl butyral having a plasticizer content ranging from 30 to 45 parts by weight of plasticizer per 100 parts by weight of polyvinylbutyral resin and (ii) a thermoplastic polyurethanes to an intermediate thermoplastic sheet of a polyvinylbutyral having a plasticizer content less than 30 parts by weight of plasticizer per 100 parts by weight of polyvinylbutyral resin, the surface of said chemically toughened glass sheet facing the interior of the cabin, having been treated with a silane primer, being coated with a layer of a transparent anti-splinter and protective covering of a polyurethane having a thickness of 50 μ
m to 600 μ
m and selected from the group consisting of (i) an aliphatic polyurethane resulting from the polycondensation of a biuret of 1,6-hexamethylene diisocyanate containing from 21 to 24% by weight of NCO radicals, with a branched aliphatic hydroxylated polyether resulting from the condensation of propylene oxide with trimethylolpropane, said polyether containing approximately from 10.5 to 12% by weight of hydroxyl radicals, the NCO/OH ratio expressed by weight ranging from 0.9 to 1.1 and (ii) a polyurethane formed from a reaction mixture comprising an isocyanate component selected from the group consisting of the biurets or the trifunctional isocyanurates of 1,6-hexamethylene diisocyanate, having an NCO radical content of 15 to 25% by weight and a polyol component selected from the group consisting of polyester polyols with a functionality greater than 2 having an OH radical content of 3 to 12% by weight, the reaction mixture having an NCO/OH ratio expressed in equivalents of 0.9 to 1.1, said polyurethane being elastically deformable, and having a modulus of elasticity of less than 2,000 daN/cm2 and an elongation at rupture exceeding 60% with less than 2% plastic deformation.
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Accused Products
Abstract
A laminated safety pane for an aircraft comprises a glass sheet intended to be on the side of the pane facing the interior of the cabin of the aircraft, the glass sheet being coated, on its surface facing the interior of the cabin with a transparent anti-splinter covering and protection film for the glass sheet, of a polyurethane having a high capacity for elastic deformation.
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Citations
4 Claims
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1. A laminated safety pane for aircraft, comprising:
a laminate of at least two bonded glass sheets, at least one of which sheets is chemically toughened and which is the glass sheet which faces the interior of the cabin, wherein a surface of said chemically toughened glass sheet is bonded by a plastic material selected from the group consisting of (i) a polyvinyl butyral having a plasticizer content ranging from 30 to 45 parts by weight of plasticizer per 100 parts by weight of polyvinylbutyral resin and (ii) a thermoplastic polyurethanes to an intermediate thermoplastic sheet of a polyvinylbutyral having a plasticizer content less than 30 parts by weight of plasticizer per 100 parts by weight of polyvinylbutyral resin, the surface of said chemically toughened glass sheet facing the interior of the cabin, having been treated with a silane primer, being coated with a layer of a transparent anti-splinter and protective covering of a polyurethane having a thickness of 50 μ
m to 600 μ
m and selected from the group consisting of (i) an aliphatic polyurethane resulting from the polycondensation of a biuret of 1,6-hexamethylene diisocyanate containing from 21 to 24% by weight of NCO radicals, with a branched aliphatic hydroxylated polyether resulting from the condensation of propylene oxide with trimethylolpropane, said polyether containing approximately from 10.5 to 12% by weight of hydroxyl radicals, the NCO/OH ratio expressed by weight ranging from 0.9 to 1.1 and (ii) a polyurethane formed from a reaction mixture comprising an isocyanate component selected from the group consisting of the biurets or the trifunctional isocyanurates of 1,6-hexamethylene diisocyanate, having an NCO radical content of 15 to 25% by weight and a polyol component selected from the group consisting of polyester polyols with a functionality greater than 2 having an OH radical content of 3 to 12% by weight, the reaction mixture having an NCO/OH ratio expressed in equivalents of 0.9 to 1.1, said polyurethane being elastically deformable, and having a modulus of elasticity of less than 2,000 daN/cm2 and an elongation at rupture exceeding 60% with less than 2% plastic deformation.- View Dependent Claims (2, 3, 4)
Specification
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Current AssigneeSaint-Gobain Vitrage International
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Original AssigneeSaint-Gobain Vitrage International
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InventorsChaussade, Pierre, Heutte, Catherine
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Primary Examiner(s)NAKARANI, DHIRAJLAL S
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Application NumberUS07/927,006Time in Patent Office2,136 DaysField of Search428/332, 428/334, 428/425.5, 428/425.6, 428/437, 428/213, 428/214, 428/215, 428/425.3, 428/428, 428/429, 52/408, 156/106, 156/108, 427/421, 204/192.1US Class Current428/332CPC Class CodesB32B 17/10036 comprising two outer glass ...B32B 17/10045 with at least one intermedi...B32B 17/10137 Chemical strengtheningB32B 17/10293 Edge features, e.g. inserts...B32B 17/10761 containing vinyl acetalB32B 17/1077 containing polyurethaneC03C 2218/31 Pre-treatmentY10T 428/26 Web or sheet containing str...Y10T 428/31594 Next to aldehyde or ketone ...Y10T 428/31598 Next to silicon-containing ...Y10T 428/31601 Quartz or glassY10T 428/31612 As silicone, silane or silo...Y10T 428/3163 Next to acetal of polymeriz...
