Window assembly for aircraft fuselage

Details Window assembly for aircraft fuselage Window assembly for aircraft fuselage

2007-10-16

2007-10-16

Luu, Teri Pham (Department: 3644)

Aeronautics and astronautics

Aircraft structure

Details

C244S129100, C244S119000, C052S204593, C052S786100, C052S786120, C428S034000

Reexamination Certificate

active

11264899

ABSTRACT:
A window assembly for an aircraft fuselage comprises an exterior transparent panel and an interior transparent panel positioned in an opening of the fuselage. At least one of the transparent panels may be relatively lightweight and the exterior transparent panel may be spaced apart from and in overlying relationship with the interior transparent panel. To ameliorate pressure build up in the spaced apart area, a pressure modulator, such as a vent, may be provided.

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U.S. Appl. No. 11/143,287, Sealed Structural Passenger Window Assembly and Method of Forming Same, Chris H. Balsillie, Donald P. Matheson, Jeffrey P. Sandys and Shawn M. Pare, 33 pages, filed Jun. 2, 2005.
Pending U.S. Appl. No. 10/262,361, filed Oct. 28, 2005, inventor Jeffrey H. Wood, 69 pages.

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