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

Claim 0:
1. An aircraft comprising:
a wing, a flight propulsion drive, and an engine pylon retainer, which joins together the wing and the flight propulsion drive,
at least one heat exchanger for cooling the exhaust gas of the fight propulsion drive and/or at least one water removal channel with at least one removal apparatus for separating water from the exhaust gas of the flight propulsion drive, after flowing through the heat exchanger,
a condenser for respectively cooling down exhaust gas of the flight propulsion drive, situated between the heat exchanger and the water removal channel in a bypass duct of the flight propulsion drive, comprising one or more condenser sections arranged concentrically to an axis of rotation of the flight propulsion drive and/or designed as plate and/or crossflow and/or counter-flow heat exchangers, and/or by at least one collection duct enclosing the condenser, for collecting exhaust gas cooled down by the condenser,
wherein the removal apparatus is arranged on, in, the retainer or is connected by the retainer to the wing and/or the flight propulsion drive is fastened on the retainer by at least one flight propulsion drive suspension and the heat exchanger is fastened, independently of the flight propulsion drive suspension, on the retainer by at least one heat exchanger suspension.