A combination adaptive energy absorption and emergency flotation device for positioning beneath a plurality of seat pans of a seat assembly in an aircraft seating application. The device includes a plurality of fluidly coupled inflatable elastic bladders (112a-c), at least one constrictor valve (128) fluidly coupling at least two adjacent ones of the plurality of inflatable elastic bladders allowing fluid flow therethrough in response to predetermined pressure on the device from the plurality of seat pans, and a fluid supply source (124) fluidly coupled to the plurality of inflatable elastic bladders for outputting a positive flow of fluid to the plurality of inflatable elastic bladders, wherein the adaptive energy absorption device is detached from the plurality of seat pans to allow removal from beneath the plurality of seat pans for use as an emergency flotation device.
COMBINATION ENERGY IMPACT ATTENUATION, VIBRATION MITIGATION AND FLOTATION DEVICE FOR AIRCRAFT SEATING APPLICATIONS
KOMBINIERTE ENERGIEAUFPRALLDÄMPFUNGS-, VIBRATIONSDÄMPFUNGS- UND SCHWIMMVORRICHTUNG FÜR FLUGZEUGSITZANWENDUNGEN
DISPOSITIF COMBINÉ D'ATTÉNUATION DES IMPACTS ÉNERGÉTIQUES; D'ATTÉNUATION DES VIBRATIONS ET DE FLOTTAISON POUR LES APPLICATIONS DE SIÈGES D'AÉRONEFS
2022-10-26
Patent
Elektronische Ressource
Englisch
Europäisches Patentamt | 2023
|Europäisches Patentamt | 2022
|Energy attenuation system for aircraft seating
Emerald Group Publishing | 1998
Engineering Index Backfile | 1960
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