Aircraft windows and associated methods for installation

Aircraft windows and associated methods for installation

Aircraft windows (120) and associated methods for installation. The windows can be installed in a passenger cabin (161) 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 sid...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: GIUNTOLI, DOMENIC S, CONDON, JOSEPH P, RITTS, MICHAEL A, BLADT, RALPH, WARREN, RYON CHRISTOPHER, FRAKER, RICHARD, QUAN, WILLIAM, MIKULENCAK, PAUL
Format: Patent
Sprache:eng ; fre ; ger
Schlagworte:
AEROPLANES
AIRCRAFT
AVIATION
COSMONAUTICS
HELICOPTERS
PERFORMING OPERATIONS
TRANSPORTING
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Beschreibung
Zusammenfassung:Aircraft windows (120) and associated methods for installation. The windows can be installed in a passenger cabin (161) 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 (121) of the window (120) aligned with none of the major axis of the aircraft. Alternatively, the window (120) 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.