Load bearing window

A substantially strong, lightweight load bearing window for use in a mobile platform, for example, an aircraft. The window includes a rim portion (18) having a carbon reinforced resin structure and a transparent portion (20) having a fiberglass reinforced resin structure. A plurality of holes are fo...

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Bibliographische Detailangaben
1. Verfasser:	SALMON JAMES J.,MCKEE SCOT
Format:	Patent
Sprache:	eng
Schlagworte:	AEROPLANES AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING AIRCRAFT AVIATION COSMONAUTICS HELICOPTERS PERFORMING OPERATIONS REMOVABLE EXTERNAL PROTECTIVE COVERINGS SPECIALLY ADAPTED FORVEHICLES SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDEDFOR SHAPING OR JOINING OF PLASTICS TRANSPORTING VEHICLES IN GENERAL WINDOWS, WINDSCREENS, NON-FIXED ROOFS, DOORS, OR SIMILARDEVICES FOR VEHICLES WORKING OF PLASTICS WORKING OF SUBSTANCES IN A PLASTIC STATE, IN GENERAL
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Beschreibung
Zusammenfassung:	A substantially strong, lightweight load bearing window for use in a mobile platform, for example, an aircraft. The window includes a rim portion (18) having a carbon reinforced resin structure and a transparent portion (20) having a fiberglass reinforced resin structure. A plurality of holes are formed in the rim portion for enabling a plurality of connectors (22) to be inserted therethrough. The rim portion has a smaller cross sectional area (i.e., thickness) than the transparent portion such that the rim portion is adapted to fit behind a skin (14) of the aircraft. The connector fix the window to the skin of the aircraft. The window effectively forms a strong, structurally integral portion of the skin.