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.
AIRCRAFT FUEL PUMP
FLUGZEUGKRAFTSTOFFPUMPE
POMPE À CARBURANT D'AÉRONEF
2021-12-29
Patent
Elektronische Ressource
Englisch