Rolls-royce Deutschland Ltd & Co. Kg

Daniel Merz

Johannes Gabriel Bauer

Andreas Reeh

Yunyang Zhao

Tobias Vermeulen

A bandage for a rotor of an electrical machine that may be used in an electrical drive system of an aircraft is provided. The bandage, which serves to fix permanent magnets to the rotor, includes two rings, which are coaxial circular ring-like components, that are connected together by axial webs. The permanent magnets each have axial grooves on a surface of the respective permanent magnet facing the stator. The bandage is arranged on the rotor such that the permanent magnets lie between the rings, and the axial webs are positioned in the axial grooves. Since a thickness of the axial webs corresponds to a depth of the axial grooves, the magnet surfaces and the surface of the bandage are flush with one another, such that the bandage requires no additional space in an air gap.

Rotor with a bandage arrangement for an electrical machine

A stator pole for a stator of a transverse flux machine is provided. The stator includes a stator winding arranged in a winding space, and the winding space being formed circumferentially in a circumferential direction in relation to an axis of rotation of a rotor. The stator pole has a body element made of a ferromagnetic material, which has at least one pole head which, in the installation position, may be arranged opposite the one rotor, and a magnetic return path region, which may be arranged facing away from the one rotor, wherein a number of the pole heads of the stator pole correspond to a number of the rotors. The stator pole is configured to occupy only a portion of a circumference of the winding space in the circumferential direction, and the magnetic return path region has a curved shape which adjoins the at least one pole head, as a result of which the magnetic return path region is designed to define the winding space in part transversely to the circumferential direction.

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Munich, Germany

Daniel Merz