Abstract: The invention relates to a rotating electrical flux-switching machine, comprising a rotatable tubular rotor (2), an inner first stator (3), and an outer second stator (4) that is concentric and spaced apart relative to the first stator (3), wherein the rotor (2) is arranged concentrically relative to the first and second stator (3, 4) and is arranged between the first and the second stator (3, 4) in such a way that a first air gap (10) is formed between the first stator (3) and the rotor (2), and a second air gap (11) is formed between the second stator (4) and the rotor (2). The invention also relates to an aircraft comprising a rotating electrical machine of this type.

Abstract: The disclosure relates to an electric machine and a hybrid electric vehicle. The electric machine includes at least one first group of superconducting coils arranged to guide a magnetic flow at least along a U-shaped course. The hybrid electric aircraft is, in particular, an aeroplane and has an electric machine of this type.

Abstract: An electrical spool device having at least one coil winding composed of a superconducting strip conductor is specified. The strip conductor includes: a strip-type substrate having two main surfaces; at least one planar superconducting layer applied on a first main surface of the substrate; and at least one outer electrical coupling layer applied on at least one of the main surfaces of the conductor composite thus formed. In this case, the coupling layer brings about an electrical coupling of adjacent turns of the coil winding, wherein the electrical coupling is dimensioned such that the time constant for electrical charging and/or discharging of the coil winding is in the range of 0.02 seconds and 2 hours.

Abstract: The coil winding has an electrical conductor for an electrical machine and includes at least two layers. The electrical conductor, following its longitudinal extension, runs inwardly wound in a first of the at least two layers, and then extends to a second of the at least two layers and runs outwardly wound in the second layer. The electrical machine includes at least one such coil winding. The hybrid electric aircraft is in particular an airplane and includes such an electrical machine and/or at least one such coil winding.

Abstract: The invention relates to a rotating electrical flux-switching machine, comprising a rotatable tubular rotor (2), an inner first stator (3), and an outer second stator (4) that is concentric and spaced apart relative to the first stator (3), wherein the rotor (2) is arranged concentrically relative to the first and second stator (3, 4) and is arranged between the first and the second stator (3, 4) in such a way that a first air gap (10) is formed between the first stator (3) and the rotor (2), and a second air gap (11) is formed between the second stator (4) and the rotor (2). The invention also relates to an aircraft comprising a rotating electrical machine of this type.

Abstract: Various embodiments include a drive system for a vehicle, the system comprising: an internal combustion engine for converting chemical energy stored in a liquid fuel into mechanical energy; a fuel tank for storing fuel for use by the internal combustion engine; and an electric machine having a rotor, a stator, and a cooling system for cooling at least one component of the electric machine using a cooling liquid. The cooling liquid comprises the fuel.

Abstract: The invention relates to an electrical conductor which is made up substantially of one or even several metal conductors which are sheathed by a graphene layer. Particularly in the case of the electrical conductor transporting an alternating current, the current in the conductor is forced radially outwards and therefore flows in the graphene layer. Since graphene has a substantially better conductivity than the materials customary in this application, such as copper for example, relatively low losses are accordingly produced and substantially higher degrees of efficiency can be achieved. The electrical conductor constructed in this way is used in a stator and/or rotor winding of an electrical machine, so that it has a significantly elevated power-to-weight ratio.

Abstract: Various embodiments include a drive system for a vehicle, the system comprising: an internal combustion engine for converting chemical energy stored in a liquid fuel into mechanical energy; a fuel tank for storing fuel for use by the internal combustion engine; and an electric machine having a rotor, a stator, and a cooling system for cooling at least one component of the electric machine using a cooling liquid. The cooling liquid comprises the fuel.

Abstract: The invention relates to a method for driving an air vehicle using a multilevel converter with at least two converter modules. A first operating voltage is applied to at least one of the converter modules in a first operating state, and a second operating voltage which is lower than the first operating voltage is applied to the converter module in a second operating state. The air vehicle is designed to carry out such a method and comprises an electric drive which has at least one multilevel converter with at least two converter modules, each of which is designed and connected so as to be supplied with a first operating voltage in a first operating state and with a second operating voltage which is lower than the first operating voltage in a second operating state. Advantageously, the air vehicle is an airplane, in particular a hybrid electric airplane.

Abstract: The invention relates to an electrical conductor which is made up substantially of one or even several metal conductors which are sheathed by a graphene layer. Particularly in the case of the electrical conductor transporting an alternating current, the current in the conductor is forced radially outwards and therefore flows in the graphene layer. Since graphene has a substantially better conductivity than the materials customary in this application, such as copper for example, relatively low losses are accordingly produced and substantially higher degrees of efficiency can be achieved. The electrical conductor constructed in this way is used in a stator and/or rotor winding of an electrical machine, so that it has a significantly elevated power-to-weight ratio.

Abstract: The disclosure relates to a drive system and to a method for providing kinetic energy for a propulsion device of an aircraft. The drive system is designed as a series hybrid system, which has an electric motor for driving the propulsion device, a generator for providing the electrical energy for the electric motor, and an internal combustion engine for providing the kinetic energy for operating the generator. The generator is designed as a superconducting generator. Hydrogen is used as a coolant for the generator. As soon as the hydrogen in the region surrounding the generator exceeds a specified temperature, the hydrogen is drawn from the generator in the gaseous state and fed to a device, which processes the hydrogen in such a way that energy that may be used in the drive system is provided. The device may be a fuel cell and/or the internal combustion engine designed as a hydrogen turbine, for example.