| 摘要 |
<p>The invention relates to a window element (1) fsr insertion in a window cutout (3) in an outer skin (4) of an aircraft, with a window frame (2, 34, 40) for accommodating a window package (6) and a press-on frame (25, 36). According to the invention the window frame (2, 34, 40) can be attached to the inside (5) of the outer skin (4) in the region of the window cutout (3), in particular can be riveted to the external skin (4), wherein for attaching the press-on frame (25, 36) at least one press-on frame fitting (14) is csnnected to the window frame (2, 34, 40) and to the outer skin (4), in particular is riveted to the window frame (2, 34, 40) and to the outer skin (4), and the window frame (2, 34, 40) comprises an essentially L-shaped or rectangular cross-sectional geometric shape .</p> |
