Ejection seat and rail assemblies for aircraft evacuation systems

An ejection system comprising an ejection seat (figure 1, 14) and a plurality of sliders (figure 1, 12) coupled to the ejection seat. A rail assembly 130 comprises a first rail 150, defining a first channel, and a first rail insert 152, defining a first rail insert channel, where the first rail inse...

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Bibliographische Detailangaben
Hauptverfasser:	Casey Andrew Stribrny, John Hampton, Jackson Fulcher, Nicholas Kersi Charles Bharucha, Steve Holstine
Format:	Patent
Sprache:	eng
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 SEATS SPECIALLY ADAPTED FOR VEHICLES TRANSPORTING VEHICLE PASSENGER ACCOMMODATION NOT OTHERWISE PROVIDEDFOR VEHICLES IN GENERAL
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Beschreibung
Zusammenfassung:	An ejection system comprising an ejection seat (figure 1, 14) and a plurality of sliders (figure 1, 12) coupled to the ejection seat. A rail assembly 130 comprises a first rail 150, defining a first channel, and a first rail insert 152, defining a first rail insert channel, where the first rail insert channel is adapted to receive the sliders. Also disclosed is an ejection system comprising a plurality of sliders or rollers, where the rail comprises a first friction reducing coating formed over an interior surface of the rail