WINDOW ELEMENT FOR INSERTION IN A WINDOW CUTOUT IN AN OUTER SKIN OF AN AIRCRAFT

WINDOW ELEMENT FOR INSERTION IN A WINDOW CUTOUT IN AN OUTER SKIN OF AN AIRCRAFT

The invention relates to a window element for insertion in a window cutout in an outer skin of an aircraft, with a window frame for accommodating a window package and a press-on frame. The window frame can be attached to the inside of the outer skin in the region of the window cutout, in particular...

Ausführliche Beschreibung

Gespeichert in:
Bibliographische Detailangaben
1. Verfasser: KRAHN, STEFAN
Format: Patent
Sprache:eng ; fre
Schlagworte:
AEROPLANES
AIRCRAFT
AVIATION
COSMONAUTICS
HELICOPTERS
PERFORMING OPERATIONS
TRANSPORTING
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Beschreibung
Zusammenfassung:The invention relates to a window element for insertion in a window cutout in an outer skin of an aircraft, with a window frame for accommodating a window package and a press-on frame. The window frame can be attached to the inside of the outer skin in the region of the window cutout, in particular it can be riveted to the external skin, wherein for attaching the press-on frame, a plurality of press-on frame fittings are connected to the window frame and to the outer skin, in particular is riveted to the window frame and to the outer skin, and the window frame comprises an essentially L-shaped or rectangular cross-sectional geometric shape. The window element facilitates the installation of the window element by reducing the number of fasteners required to connect the press-on frame fittings with the window frame and the outer skin.