A cargo restraint system (50) may comprise a restraint (102; 104; 106) and an actuator shaft (150) configured to rotate the restraint (102; 104; 106) between a raised position and a stowed position. The restraint (102; 104; 106) may include a head (120) configured to rotate about an axis (A-A') and a plunger (170) configured to translate between an engaged state and a disengaged state. When the plunger (170) is in the engaged state, the head (120) is rotationally coupled to the actuator shaft (150). When the plunger (170) is in the disengaged state, the head (120) can rotate independently of the actuator shaft (150).
CARGO RESTRAINT SYSTEM WITH INDIVIDUALLY RETRACTABLE RESTRAINTS
FRACHTRÜCKHALTESYSTEM MIT EINZELN EINZIEHBAREN RÜCKHALTEVORRICHTUNGEN
SYSTÈME DE RETENUE DE CARGAISON AVEC DISPOSITIFS DE RETENUE RÉTRACTABLES INDIVIDUELLEMENT
2025-01-15
Patent
Electronic Resource
English
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
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