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composite panel for a front pilot collimator (hud) with an electrically conductive coating and an anti-reflective coating

机译:用于前导准直器(hud)的复合板,具有导电涂层和抗反射涂层

摘要

the present invention relates to a composite panel (10) for a front pilot collimator (hud) with an upper edge (o), a lower edge (u) and a hud region (b), comprising at least one outer panel (1) and an inner panel (2), which are joined together by means of a thermoplastic intermediate layer (3) and an electrically conductive transparent coating (20) on the surface (iii) of the inner panel (2) facing the intermediate layer (3) or inside the intermediate layer (3), where the intermediate layer (3) is formed by at least one layer (3a) of thermoplastic material, which is arranged between the electrically conductive coating (20) and the panel outer (1), where the thickness of the layer (3a) of the thermoplastic material is variable with the wedge angle (a) along its vertical course between the lower edge (u) and the upper edge (o) at least in hud region (b), and where an anti-reflective coating (30) is applied to the surface (iv) of the inner panel (2) facing away from the middle layer (3).
机译:本发明涉及一种用于前飞行员准直仪(hud)的复合板(10),其具有上边缘(o),下边缘(u)和hud区域(b),包括至少一个外板(1)内板(2)和内板(2),它们借助于热塑性中间层(3)和内板(2)面对中间层(3)的表面(iii)上的透明导电涂层(20)连接在一起)或中间层(3)的内部,其中中间层(3)由至少一层热塑性材料(3a)形成,该热塑性材料层(3a)布置在导电涂层(20)和面板外层(1)之间,其中热塑性材料层(3a)的厚度至少在平视区域(b)中沿着下边缘(u)和上边缘(o)之间的垂直方向随楔角(a)变化,并且其中抗反射涂层(30)被施加到内面板(2)的背离中间层(3)的表面(iv)上。

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