A cargo restraint system may comprise an inner shaft (154) and a first outer tube (152) coaxially configured to rotate about an axis and a first restraint located about the first outer tube (152) and configured to rotate about the axis. A second outer tube coupled to the inner shaft (154) configured to rotate about the axis and a second restraint (104) located about the second outer tube and configured to rotate about the axis. The first restraint (102) and the second restraint (104) may include a head configured to rotate about the axis and a plunger configured to translate between an engaged state and a disengaged state.
RESTRAINT SYSTEM UTILIZING CO-AXIAL ACTUATION
RÜCKHALTESYSTEM MIT KOAXIALER BETÄTIGUNG
SYSTÈME DE RETENUE UTILISANT UN ACTIONNEMENT COAXIAL
2025-04-09
Patent
Electronic Resource
English
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / 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 |