REDUNDANT RAIL AND CARRIAGE ASSEMBLY

A redundant rail and carriage assembly is disclosed. The assembly may include a primary sub-assembly (204) including a primary rail (206) and a primary carriage (208). The assembly may include a secondary sub-assembly (210) including a secondary rail (212) and a secondary carriage (214), the seconda...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser:	JACOB, Twinkle V, DAVID, Lyle T, STEELE, Bradley, SIKORSKI, Joseph, WARWICK, Michael R.G
Format:	Patent
Sprache:	eng ; fre ; ger
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 redundant rail and carriage assembly is disclosed. The assembly may include a primary sub-assembly (204) including a primary rail (206) and a primary carriage (208). The assembly may include a secondary sub-assembly (210) including a secondary rail (212) and a secondary carriage (214), the secondary rail being different than the primary rail, the secondary carriage being different than the secondary carriage. The assembly may be configured to couple to an actuatable door (200) configured to actuate between a stowed door position and a deployed door position via at least one intermediate door position using one of the primary sub-assembly or the secondary sub-assembly, the secondary sub-assembly being configured to actuate the actuatable door via the secondary rail and the secondary carriage if one of the primary rail or the primary carriage of the primary sub-assembly fails.