FIELD: transport.
SUBSTANCE: invention relates to aircraft glazing. Lateral or front glazing comprises first rigid mount with outer side directed toward crew cabin outer section, second rigid mount, third rigid mount with inner side directed toward crew cabin inner section. Second rigid mount is arranged between first and second rigid mounts. Said rigid mounts are made of thermally semi-hardened or chemically hardened glass. Glazing has first "active" system comprising layer and second "active" system arranged between first rigid mount and second rigid mount and consisting of thin heated layers. First rigid mount is located with indent with respect to other two rigid mounts. Glazing incorporates polymer film as adhesive interlayer to hold back broken glazing pieces arranged between first rigid mount and second rigid mount, and/or between second rigid mount and third rigid mount.
EFFECT: higher reliability.
12 cl, 2 dwg
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Authors
Dates
2012-12-27—Published
2007-12-06—Filed