Composite aircraft window frame

Details Composite aircraft window frame Composite aircraft window frame

B - Operations, Transporting

64

C

B64C 1/14 (2006.01) B29D 12/00 (2006.01)

Patent

CA 2675206

An aircraft window frame (18) includes a laminated outer rim (22) and inner sash (24) having a central aperture (26) for receiving a window pane (20). The sash (24) is transversely offset from the rim (22) and they include different layers (1-7) between the opposite inboard and outboard sides (28,20) of the frame (18).

L'invention concerne un encadrement de hublot pour avion (18). Ledit encadrement comprend un rebord externe stratifié (22) et un châssis interne (24) ayant une ouverture centrale (26) pour recevoir une glace de hublot (20). Le châssis (24) est transversalement décalé par rapport au rebord (22) et ils comprennent des couches différentes (1 à 7) entre les côtés opposés, intérieur et extérieur, (28, 20) de l'encadrement (18).

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