A refueling boom is provided for use in an aerial refueling system. The refueling boom may include a boom section configured to extend from a tanker aircraft. A pressure limiting valve may be provided downstream of the boom section. A boom nozzle may be provided downstream of, or integral with, the pressure limiting valve.
AERIAL REFUELING BOOM WITH PRESSURE LIMITING VALVE
2015-10-08
Patent
Electronic Resource
English
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |