A tanker aircraft capacity extension system shaped to fit within an aircraft cargo area may include a first portable fuel container having a first outlet port adapted to connect to an integral fuel system of the aircraft, and a first inlet port; and a second portable fuel container having a second outlet port adapted to connect to the first inlet port and a second inlet port adapted to connect to a third fuel container; when the second outlet port is connected to the first inlet port and the first outlet port is connected to the integral fuel system of the aircraft, fuel flows from the second fuel container, through the outlet port to the first inlet port into the interior of the first container, and out from the first outlet port of the first container.
Tanker aircraft capacity extension system and method
2018-01-23
Patent
Elektronische Ressource
Englisch
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
Engineering Index Backfile | 1945