METHOD AND APPARATUS FOR MAKING A POLYMERIC AIRCRAFT WINDOW PANEL

A mold for casting a polymeric aircraft window panel includes a first mold half (12) having a first mold surface (24), and a second mold half (14) having a second mold surface (50). The first mold surface (24) and/or the second mold surface (50) have a shape conforming to a final shape for the major...

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Hauptverfasser:	MCCARTHY DENNIS P, GOODWIN GEORGE B, SHEARER JOHN D M
Format:	Patent
Sprache:	chi ; eng
Schlagworte:	AEROPLANES AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING AIRCRAFT AVIATION COSMONAUTICS HELICOPTERS PERFORMING OPERATIONS SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDEDFOR SHAPING OR JOINING OF PLASTICS TRANSPORTING WORKING OF PLASTICS WORKING OF SUBSTANCES IN A PLASTIC STATE, IN GENERAL
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Zusammenfassung:	A mold for casting a polymeric aircraft window panel includes a first mold half (12) having a first mold surface (24), and a second mold half (14) having a second mold surface (50). The first mold surface (24) and/or the second mold surface (50) have a shape conforming to a final shape for the major surfaces of the aircraft window panel. The first mold half (12) and/or the second mold half (14) can be formed of rolled, hydroformed, or stamped metal. The first (24) and/ or the second mold surface (50) can include a pattered region (78), The first mold half (12) can comprise a first flange (26)having a peripheral edge (214), and the second mold half (14) a second flange (52) having a peripheral edge (216) or the mold (10, 66) including a shaped gasket (200) located between the peripheral edge (214) of the first mold half (12) and the peripheral edge (214) of the second mold half (14). 浇铸聚合物的飞行器窗板的模具包括具有第模具表面(24)的第模具半部分(12)，以及具有第二模具表面(50)的第二模具半部分(14)。该第模具表面(24)和/或该第二模具表面(50)具有形状依从飞行器窗板的主表面的最终形状。该第模具半部分(12)和/或该第二