A series of dynamic tests of both operational and prototype H-60 troop seats was performed to determine occupant protection during a crash event. The H-60A/L, UH-60M, prototype Glatz, and prototype Wolf seats were tested at several impact orientations including Combined Vertical, Pure Vertical and Combined Horizontal, and at different acceleration and energy levels using small female and large male manikins. Biodynamic data were compared to injury criteria recommended by the Army Full Spectrum Crashworthiness (FSC) Report (2011). Data were also compared to Eiband and operational mishap data. The testing and data analysis methodology developed during the program can be used to baseline and compare seats within a given aircraft platform or across different aircraft platforms. Combining quantitative injury criteria measures, such as those outlined within the FSC, along with laboratory and operational mishap data, demonstrate that new seats and seat technology can be quickly and inexpensively tested either singly or in a comparative evaluation, independent of aircraft platforms.
Assessment of Cargo Space Seating Performance Applicable to Pave Hawk and Black Hawk Aircraft During Helicopter Mishaps
2012
106 pages
Report
Keine Angabe
Englisch
Aircraft , Aeronautics , Public Health & Industrial Medicine , Job Environment , Aircraft seats , Crashworthiness , Helicopters , Biodynamics , Crash injuries , Crash landings , Instrumentation , Test methods , H-60 aircraft , Occupant protection , Manikins , Quantitative injury criteria measures , Seat technology , Dynamic tests , Fsc(Full spectrum crashworthiness) , Helicopter mishaps
ASSESSMENT OF CARGO SPACE SEATING PERFORMANCE IN PAVE HAWK AND BLACK HAWK AIRCRAFT
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Engineering Index Backfile | 1950
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