Abstract: A rotation angle detection sensor system for a rotational body is provided, which has a reduced sensitivity against an interfering magnetic field and an interfering electric field. The rotation angle detection sensor system comprises an encoder structure that is attached to the rotational body of a machine and is movable along with this rotational body. A stationary sensor assembly is positioned opposite to this encoder structure and supplies at least one sensor signal for determining the angle position. The sensor assembly includes a first inductive element, the inductance of which is dependent on the angle position of the encoder structure.

Abstract: A rotation angle detection sensor system for a rotational body is provided, which has a reduced sensitivity against an interfering magnetic field and an interfering electric field. The rotation angle detection sensor system comprises an encoder structure that is attached to the rotational body of a machine and is movable along with this rotational body. A stationary sensor assembly is positioned opposite to this encoder structure and supplies at least one sensor signal for determining the angle position. The sensor assembly includes a first inductive element, the inductance of which is dependent on the angle position of the encoder structure.

Abstract: The vibration absorbers have mounts for radial fastening of the vibration absorber to an inside surface of a wheel rim to be used on rails. A plurality of mounts are uniformly distributed over the circumference of the inside surface and are each coupleable to the wheel rim in an acoustically good conducting manner against a surface that matches the radius of curvature of the inside surface. On each mount at least one vibration absorber consisting of a sequence, running in the radial direction, of metal and plastic plates can be coupled in an acoustically effective manner by means of a coupling surface. The vibration absorbers and mount are releasably connected with one another and have a coupling surface that is always the same and is independent of the radius of curvature of the inside surface of the wheel rim.

Abstract: A flying body, such as a missile, is strapped to a carrier vehicle, such as an aircraft, by a strapping or locking mechanism mounted in a housing which also includes components for suspending and launching the flying body from launching rails forming part of the housing connected to the carrier aircraft. The strapping is accomplished with two strapping bridges which are pressed down onto the respective suspension block elements resting on the launching rail. The pressing down force is applied by a toggle lever arrangement, one of which is provided for each strapping bridge. The toggle lever arrangement cooperates with a respective spring arrangement which keeps the corresponding toggle levers in a strapping position until the spring arrangement is released through release pawls operated with a reverse magnet. A retaining mechanism which is effective between the release of the strapping mechanism and the actual launching after ignition of the propulsion system of the flying body, is made ready for launching.