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 |