AUTOMATIC EJECTION SEAT PERFORMANCE AND ACCOMODATION OPTIMIZATION BASED ON CONNECTOR

A system (300) for automatic optimization of an ejection system (200) for an aircraft includes the ejection system having a plurality of adjustable settings and having a plurality of components (204,206,208,210). The system further includes a connector (212;218;224;230) configured to connect to a co...

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Bibliographische Detailangaben
Hauptverfasser:	STRIBRNY, Casey, CARSON, Kassidy L, BHARUCHA, Nicholas, MCCUMBER, Ronald John, HOLSTINE, Steve, MASTROLIA, Bradley, HAMPTON, John
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 SEATS SPECIALLY ADAPTED FOR VEHICLES TRANSPORTING VEHICLE PASSENGER ACCOMMODATION NOT OTHERWISE PROVIDEDFOR VEHICLES IN GENERAL
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Beschreibung
Zusammenfassung:	A system (300) for automatic optimization of an ejection system (200) for an aircraft includes the ejection system having a plurality of adjustable settings and having a plurality of components (204,206,208,210). The system further includes a connector (212;218;224;230) configured to connect to a component of the plurality of components and having a connector portion that includes information corresponding to a user of the ejection system. The system further includes a controller (302) coupled to the ejection system and configured to adjust at least one of the plurality of the adjustable settings of the ejection system based on the information corresponding to the user of the ejection system.