A cargo system (100, 520) is provided. The cargo system may comprise a floor panel (112), a cargo sled configured to move across the floor panel (112), and a cargo restraint (200, 202, 500, 722) configured to translate relative to the floor panel (112). The cargo restraint may comprise a longitudinal restraint rod (302, 503) configured to protrude from the floor panel (112) in a deployed position. The cargo restraint may also comprise a restraint surface (300A, 501) disposed on the longitudinal restraint rod. The cargo restraint may enable the cargo sled to pass over the restraint surface in a stowed position. An electromechanical actuator (702) may be mechanically coupled to the longitudinal restraint rod and configured to deploy and stow the cargo restraint.
CONFORMAL ACTUATOR OPERATED AIRCRAFT CARGO RESTRAINT MECHANISM
KONFORMER AKTUATORBETÄTIGTER LUFTFRACHTZURÜCKHALTUNGSMECHANISMUS
MÉCANISME DE RETENUE DE CHARGEMENT D'AÉRONEF MANOEUVRÉ PAR ACTIONNEUR CONFORME
2019-05-08
Patent
Electronic Resource
English
IPC: | B60P Fahrzeuge zum Transport von Lasten oder zum Befördern, Tragen oder Aufnehmen besonderer Lasten oder Gegenstände , VEHICLES ADAPTED FOR LOAD TRANSPORTATION OR TO TRANSPORT, TO CARRY, OR TO COMPRISE SPECIAL LOADS OR OBJECTS / B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
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