Patent ID: 11964779
Assignee: SAFRAN AIRCRAFT ENGINES
Field: Engines, pumps, turbines (Mechanical engineering)
Classification: CPC B  F  G | IPC B  F  G

Claim 0:
1. An oil tank filling device for filling an oil tank of an aircraft engine, comprising:
a supply duct leading to the oil tank of the aircraft engine and supplied with oil by another tank disposed in an aircraft at a distance from the aircraft engine,
a pump placed on the supply duct, and
a filling processing module, connected to a probe of an oil level in the oil tank and giving height indications of said oil level,
wherein the supply duct comprises a filling shut-off valve located between the pump and the oil tank, the oil tank filling device comprises a device for closing the filling shut-off valve, independent of the probe and the filling processing module, sensitive to oil rising to an optimum fill level of the oil tank, and
wherein the filling processing module comprises a tank overfill indicator and a tank nominal fill indicator, said tank overfill indicator and said tank nominal fill indicator being controlled when the oil reaches an overfill level above the optimum fill level and a nominal fill level below the optimum fill level, respectively, and the optimum fill level is distant from the nominal fill level and the overfill level by differences in level both corresponding to a measurement uncertainty ascribed to the probe.