Engine (50; 54; 55; 56), comprising: a field (2); and a runner (1) which is facing the field (2) and is arranged to be movable relative to the field (2), wherein the rotor (1) comprises a core back (11), several teeth (12) and several coils (13), wherein the several teeth (12) each extend from the core back (11) to the field (2) and are arranged in a direction of travel of the rotor (1) with respect to the field (2), wherein the several coils (13) are attached to the several teeth (12), wherein the multiple teeth (12) comprise at least one first tooth and at least one second tooth, wherein each of the at least one first tooth is a tooth to which only one coil of a
single phase of the coils (13) is attached, wherein each of the at least one second tooth is a tooth to which coils of multiple phases of the coils (13) are attached, wherein the multiple coils (13) are each arranged such that they do not extend beyond a slot formed by adjacent teeth, wherein
C sections (10) are arranged in the direction of travel, wherein the section (10) comprises N / C teeth (12), where N is the number of teeth (12) of the runner (1), wherein C is a greatest common divisor of N and the number of
magnetic poles of the field (2), the
magnetic poles being located in a region facing the N teeth (12), and where the number of second teeth per section of the
C sections (10) is one.