Conformal actuator operated aircraft cargo restraint mechanism
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United States of America Patent
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Apr 10, 2018
Issued Date -
N/A
app pub date -
Oct 15, 2015
filing date -
Oct 15, 2015
priority date (Note) -
In Force
status (Latency Note)
Importance
Abstract
A cargo system is provided. The cargo system may comprise a floor panel, a cargo sled configured to move across the floor panel, and a cargo restraint configured to translate relative to the floor panel. The cargo restraint may comprise a longitudinal restraint rod configured to protrude from the floor panel in a deployed position. The cargo restraint may also comprise a restraint surface 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 may be mechanically coupled to the longitudinal restraint rod and configured to deploy and stow the cargo restraint.
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