An aircraft cargo system includes a ball panel assembly having a ball panel and a first enclosure assembly. The ball panel defines a first cutout. The first enclosure assembly is at least partially disposed within the first cutout and is movable between an open position and a closed position. The first enclosure assembly includes a first enclosure defining a first opening that receives a first ball transfer unit.
Modular standard configuration ballpanel
28.08.2018
Patent
Elektronische Ressource
Englisch
Configuration Management Standard
SAE | 2019
Configuration Management Standard
SAE | 2011
Integrated Modular Engine Configuration Options
NTIS | 1993
|