An external hook system for a rotary-wing aircraft includes a lower frame interface which accommodates longitudinal and lateral loads and an upper frame interface. A tension member is mountable between the lower frame interface and the upper frame interface to transfer tension loads between the lower frame interface and the upper frame interface.
EXTERNAL CARGO HOOK SYSTEM FOR ROTARY-WING AIRCRAFT
EXTERNES LASTENHAKENSYSTEM FÜR DREHFLÜGELFLUGZEUG
SYSTÈME DE CROCHET DÉLESTEUR DE FRET EXTERNE POUR AÉRONEF À VOILURE TOURNANTE
27.05.2020
Patent
Elektronische Ressource
Englisch
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