Fluid pump for an aircraft turbomachine, lubrication circuit and aircraft turbomachine
AssigneeSafran Aero Boosters SA
InventorQuentin BORLON
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AssigneeSafran Aero Boosters SA
InventorQuentin BORLON
Estimating the term…
A fluid pump for an aircraft turbomachine includes a ring through which a duct passes along a central axis, a rotor driven in rotation with respect to the ring along a main axis offset relative to the central axis. Cavities between the ring and the rotor have volumes that vary according to the angular position of the rotor with respect to the ring. The pump further includes an inlet space for admitting the fluid into the cavities and a discharge space for discharging the fluid from the cavities, the pressure in the discharge space being higher than the pressure in the inlet space. A groove pressurizes the cavities in the discharge space when the rotor rotates.
A fluid pump for an aircraft turbomachine, comprising:
A lubrication circuit for lubricating an aircraft turbomachine, comprising at least one pump, the pump comprising:
An aircraft turbomachine, comprising a lubrication circuit having at least one pump, the pump comprising:
Dependencies are inferred from the claim text.