Patent ID: 11965462
Assignee: MTU AERO ENGINES AG
Field: Engines, pumps, turbines (Mechanical engineering)
Classification: CPC F  B  Y | IPC B  F

Claim 5:
6. The aircraft according to claim 1, wherein the removal apparatus comprises at least one separation plate arranged in the water removal channel and/or at least one swirl generator arranged in the water removal channel downstream from the separation plate, and/or at least one turbine stage arranged in the water removal channel downstream from the separation plate coupled to a generator, and/or at least one separation pipe arranged in the water removal channel downstream from the turbine stage and/or the swirl generator, and/or at least one electrostatic removal apparatus, and/or at least one heat exchanger with coolant flowing through it in a cooling circuit and/or has an at least partial hydrophilic surface.