航空機用窓枠

Abstract

The frame (1) includes at least one outer flange (2) attached to the window opening edge of the aircraft fuselage, and at least one inner flange (3) and a vertical flange (4) which support a window piece e.g. glass panel. The frame is made from resin reinforced with unidirectionally-arranged fiber bundles. An independent claim is also included for a window frame manufacturing method.

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Patent Citations (4)

    Publication numberPublication dateAssigneeTitle
    JP-2005153680-AJune 16, 2005Shikibo Ltd, シキボウ株式会社Dry preform for window frame made of frp used for aircraft
    US-2003168775-A1September 11, 2003Ulrich Eberth, Paul JoernMethod and apparatus for manufacturing a fiber reinforced synthetic composite structural element using fiber textile preforms
    WO-2004016844-A1February 26, 2004Shikibo Ltd.繊維強化複合材料用プリフォーム前駆体、繊維強化複合材料用プリフォームおよびその製造方法
    WO-8301237-A1April 14, 1983Whitener, Philip, CharlesComposite structures window belt and method of making

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