发明名称 CONFORMAL ACTUATOR OPERATED AIRCRAFT CARGO RESTRAINT MECHANISM
摘要 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.
申请公布号 US2017106966(A1) 申请公布日期 2017.04.20
申请号 US201514884557 申请日期 2015.10.15
申请人 Goodrich Corporation 发明人 Himmelmann Richard
分类号 B64C1/22;B64C1/20 主分类号 B64C1/22
代理机构 代理人
主权项 1. A cargo system, comprising: a floor panel; a cargo sled configured to move across the floor panel; a cargo restraint configured to translate relative to the floor panel, the cargo restraint comprising: a longitudinal restraint rod configured to protrude from the floor panel in a deployed position; anda restraint surface disposed on the longitudinal restraint rod, wherein the cargo restraint is configured to enable the cargo sled to pass over the restraint surface in a stowed position; and an electromechanical actuator mechanically coupled to the longitudinal restraint rod, wherein the electromechanical actuator is configured to deploy and stow the cargo restraint.
地址 Charlotte NC US