A UAV capture system is disclosed. In the illustrative embodiment, the UAV capture system is coupled to the deck of a sea-faring vessel. The UAV capture system includes a single arresting line that is supported by a stanchion. In the illustrative embodiment, the stanchion is disposed on a rotatable boom.

 
Web www.patentalert.com

> Engine inlet air particle separator with active flow control

~ 00348