Aeronautics and astronautics – Aircraft structure – Details
Reexamination Certificate
2006-04-18
2006-04-18
Barefoot, Galen (Department: 3644)
Aeronautics and astronautics
Aircraft structure
Details
Reexamination Certificate
active
07028950
ABSTRACT:
A substantially strong, lightweight load bearing window for use in a mobile platform, for example, an aircraft. The window includes a rim portion having a carbon reinforced resin structure and a transparent portion having a fiberglass reinforced resin structure. A plurality of holes are formed in the rim portion for enabling a plurality of connectors 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 of an aircraft, the transparent portion is adapted to be flush with the skin of the aircraft. The connectors fix the window to the skin of the aircraft. The window effectively forms a strong, structurally integral portion of the skin.
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McKee Scot
Salmon James J.
Barefoot Galen
Harness & Dickey & Pierce P.L.C.
The Boeing Company
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