Abstract: An actuator for aviation applications, in particular for adjusting rotor blades in a helicopter, may include an electromechanical drive assembly connected to an output drive via a downstream transmission, where the drive assembly is divided into sub-drives that can be operated independently, and where at least two sub-drives are spatially separated from one another in that the transmission is placed between these sub-drives. The transmission may include at least two harmonic gearings coupled to one another by at least one first coupling element, where a first harmonic gearing is located inside a non-rotating first housing, where a second harmonic gearing is located inside a rotating second housing, and where the second housing is connected to the output drive.

Abstract: The invention relates to an apparatus for picking up sound waves with a separating body and at least two microphones arranged on the separating body. A pick-up which is particularly true to nature is achieved in such a way that the separating body consists of a reverberant material and is provided with a substantially wedge-shaped arrangement, with two separating surfaces which are inclined towards one another at an acute angle, and that the microphones are arranged at a low distance from the separating surfaces.