The patent application relates to an improved helicopter seat with improved crash characteristics and includes four crash attenuating struts for seat support during normal use and adjusting means to move the seat into positions so that the majority of pilots may fly the helicopter in comfort.
An Improved Armored Helicopter Seat
1973
14 pages
Report
Keine Angabe
Englisch
LIGHTWEIGHT INTEGRALLY ARMORED HELICOPTER FLOOR
British Library Conference Proceedings | 2013
|Armored Structural Helicopter Fuselage Study
NTIS | 1973
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