In an embodiment, the present invention provides an aircraft fuel pump assembly including: a pump; a canister to enclose the pump and mount the pump within an aircraft fuel tank; and a discrete electronics unit mounted remotely to the pump. In another embodiment, the present invention provides a manhole cover for an aircraft, comprising an integral mounting for an electronics unit.
ТОПЛИВНЫЙ НАСОС ЛЕТАТЕЛЬНОГО АППАРАТА
2019-05-22
Patent
Elektronische Ressource
Russisch
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
Europäisches Patentamt | 2017
Europäisches Patentamt | 2017