Aircraft windows and associated methods for installation

Details Aircraft windows and associated methods for installation Aircraft windows and associated methods for installation

B - Operations, Transporting

64

C

B64C 1/14 (2006.01) B64C 1/00 (2006.01)

Patent

CA 2414700

Aircraft windows and associated methods for installation. The windows can be installed in a passenger cabin of an aircraft and can include a frame that supports a pane assembly having a viewing area of at least 180 square inches. The viewing area can have a triangular shape, with the sides of the window aligned with none of the major axis of the aircraft. Alternatively, the window can have a longitudinally extended rectangular shape, a diamond shape or an elliptical shape. The window frame can have a divider portion that separates two window apertures, each of which carries a separate pane assembly. Adjacent windows can be closed out with a common bezel.

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