INTEGRATED STOWAGE BIN ASSEMBLY

A stowage bin assembly includes a bin bucket assembly (12) having a bin bucket which includes at least one sidewall (15), the at least one sidewall (15) including a notch (20) and the at least one sidewall having an interior surface. The stowage bin assembly also includes at least one hinge assembly...

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Bibliographische Detailangaben
Hauptverfasser:	LACONTE, RICHARD J, CHADWELL, DAVID
Format:	Patent
Sprache:	eng ; fre
Schlagworte:	AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION COSMONAUTICS EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS PARACHUTES PERFORMING OPERATIONS TRANSPORTING
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Beschreibung
Zusammenfassung:	A stowage bin assembly includes a bin bucket assembly (12) having a bin bucket which includes at least one sidewall (15), the at least one sidewall (15) including a notch (20) and the at least one sidewall having an interior surface. The stowage bin assembly also includes at least one hinge assembly (14A; 14B). The at least one hinge assembly (14A; 14B) includes a housing (22) which is received in the notch (20), the housing having an interior surface, wherein the interior surface of the housing is substantially flush with the interior surface of the at least one sidewall when the housing of the at least one hinge assembly is received in the notch (20). The stowage bin assembly also includes a stowage bin door (13) pivotably coupled to the bin bucket assembly via the at least one hinge assembly (14A; 14B), the stowage bin door (13) moveable between an open position and a closed position. Related components, assemblies, and devices are also provided. L'invention concerne un compartiment à bagages comprenant un ensemble bac de compartiment (12) ayant un bac de compartiment qui comprend au moins une paroi latérale (15), ladite paroi latérale (15) comprenant une encoche (20) et ladite paroi latérale ayant une surface intérieure. Le compartiment à bagages comprend également au moins un ensemble charnière (14A ; 14B). Ledit ensemble charnière (14A ; 14B) comprend un boîtier (22) qui est inséré dans l'encoche (20), le boîtier ayant une surface intérieure, la surface intérieure du boîtier étant sensiblement alignée avec la surface intérieure de ladite paroi latérale lorsque le boîtier dudit ensemble charnière est inséré dans l'encoche (20). Le compartiment à bagages comprend également une porte de compartiment à bagages (13) couplée de manière pivotante à l'ensemble bac de compartiment par l'intermédiaire dudit ensemble charnière (14A ; 14B), la porte de compartiment à bagages (13) étant mobile entre une position ouverte et une position fermée. L'invention concerne également des composants, ensembles et dispositifs associés.