| 摘要 |
<p>The invention relates to a drive device for an aircraft (100), at least comprising a battery (101) for storing electrical energy, an electric motor (103) for driving a propeller (104), a conducting means (102) for transferring the electrical energy from the battery (101) to the electric motor (103), and a first control means (201) for controlling said electric motor (103). The invention is characterised in that: the battery (101) is a lithium-air battery; the electric motor (103) is a high-temperature superconductor motor; at least one store (105) is provided for a coolant and a cooling system which is connected to said store (105) for cooling said high-temperature superconductor motor (103), the cooling system comprising a second control means (202) for controlling said cooling system; a first means (204) is provided for variably arranging the lithium-air battery (101) and/or a second means (205) is provided for variably arranging the store (105) in the aircraft (100); and a third control means (203) is provided for controlling the first (204) and/or the second (205) means.</p> |
