MODULAR INDEXING FOR AIRCRAFT INTERIOR

MODULAR INDEXING FOR AIRCRAFT INTERIOR

An assembly for an aircraft cabin of an aircraft, the aircraft having a fuselage with a plurality of external windows arranged at a pitch. The assembly having a window cone panel with an internal window, top and bottom edges defining a panel height, and side edges defining a panel width. First and s...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: KNOWLES, BYRON, KAMIN, JOHN, Y
Format: Patent
Sprache:eng ; fre ; ger
Schlagworte:
AEROPLANES
AIRCRAFT
AVIATION
COSMONAUTICS
HELICOPTERS
PERFORMING OPERATIONS
TRANSPORTING
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Beschreibung
Zusammenfassung:An assembly for an aircraft cabin of an aircraft, the aircraft having a fuselage with a plurality of external windows arranged at a pitch. The assembly having a window cone panel with an internal window, top and bottom edges defining a panel height, and side edges defining a panel width. First and second terminator components are disposed on either side of the window cone panel such that the first terminator component is on one side of the window cone panel and the second terminator component is on the other side of the window cone panel. A splice component is disposed on either side of the window cone panel between the window cone panel and one of the first and second terminator components. The splice component includes an index for adjusting an overall width of the assembly to align the internal window opening with the external window pitch.