An aircraft window has an inner window assembly retained on an outer window assembly by a plurality of interlocking clips and receptacles positioned around the perimeter of the window. The interlocking clips and receptacles produce a retention force that compresses a seal against an outer structural the window to seal an internal cavity between the inner and outer window assemblies.
AIRCRAFT WINDOW AND INSTALLATION METHOD
FLUGZEUGFENSTER UND INSTALLATIONSVERFAHREN
FENÊTRE D'AVION ET PROCÉDÉ D'INSTALLATION
2017-11-15
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |
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European Patent Office | 2018
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