Electrified aircraft and its aerodynamic performance control method

摘要

PROBLEM TO BE SOLVED: To provide an electrified aircraft capable of optimizing the aerodynamic performance of a wing in an emergency such as each flight phase or a gust action without depending on the shape of the wing, and a method for controlling the aerodynamic performance thereof. An electrified aircraft 1 is one or more having a propeller or fan 21 for propulsion arranged so as to contribute to the lift of main wings 11 and 12, and an electric motor 22 for driving the propeller or fan 21. Based on the relationship between the electric propulsion system 20 and the variables related to the operating state of the electric propulsion system 20 and the aerodynamic force generated in the main wings 11 and 12, the total thrust by the electric propulsion system 20 or the aerodynamic force of the main wings 11 and 12 is predetermined. A control unit that adjusts the electric propulsion system 20 so as to be within the value of or a predetermined range is provided. [Selection diagram] Fig. 2