PROBLEM TO BE SOLVED: To provide a functional film for aircraft windows that is used for imparting an aircraft window structure with functions such as electromagnetic shielding properties, heat shielding properties and thermal insulation properties, and an aircraft window structure employing the same.SOLUTION: A functional film (100) is sequentially provided, on a first main surface of a transparent film base (10), with a functional thin film (20) that is composed of a laminate of metal oxide layers (21, 22) and a metal layer (25), and a transparent protective layer (30) in this order. The transparent protective layer (30) serves as the outermost surface layer of the functional film (100).SELECTED DRAWING: Figure 1
【課題】航空機の窓構造に、電磁波遮蔽性、遮熱性、断熱性等の機能を付与するための航空機窓用機能性フィルム、および当該機能性フィルムを適用した航空機用窓構造体を提供する。【解決手段】機能性フィルム(100)は、透明フィルム基材(10)の第一主面上に、金属酸化物層(21,22)と金属層(25)との積層体からなる機能性薄膜(20)、および透明保護層(30)をこの順に備える。透明保護層(30)は、機能性フィルム(100)の最表面層である。【選択図】図1
FUNCTIONAL FILM FOR AIRCRAFT WINDOWS, AIRCRAFT WINDOW STRUCTURE AND METHOD FOR FUNCTIONALIZING AIRCRAFT WINDOW
航空機窓用機能性フィルム、航空機窓構造体、および航空機窓の機能化方法
2017-03-23
Patent
Electronic Resource
Japanese
European Patent Office | 2017
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