Abstract: A mold assembly for producing a casting core for a cooling jacket of an electric motor has an external mold and an internal mold enclosed by the external mold. The external mold forms an outer wall and the internal mold an inner wall of the core molding cavity fillable with a core material and having a cylindrical shape. The internal mold has two first mold shells and two second mold shells. The two first mold shells and the two second mold shells jointly form the inner wall of the core molding cavity. The second mold shells are arranged between the first mold shells. A first demolding mechanism is arranged between the first mold shells and enables movement of the first mold shells toward one another. A second demolding mechanism is arranged between the second mold shells and enables movement of the second mold shells toward one another.

Abstract: A mould assembly for producing a casting core for a cooling jacket of an electric motor has an external mould and an internal mould enclosed by the external mould. The external mould forms an outer wall and the internal mould an inner wall of the core moulding cavity fillable with a core material and having a cylindrical shape. The internal mould has two first mould shells and two second mould shells. The two first mould shells and the two second mould shells jointly form the inner wall of the core moulding cavity. The second mould shells are arranged between the first mould shells. A first demoulding mechanism is arranged between the first mould shells and enables movement of the first mould shells toward one another. A second demoulding mechanism is arranged between the second mould shells and enables movement of the second mould shells toward one another.

Abstract: Structural element for an aircraft, especially an aircraft door, in a single-piece, integral cast embodiment consisting of an aluminum or magnesium alloy.

Abstract: Structural element for an aircraft, especially an aircraft door, in a single-piece, integral cast embodiment consisting of an aluminum or magnesium alloy.

Abstract: Aluminum alloy containing a fraction of uniformly distributed particles, preferably silicon particles, of less than 20% by weight, so as to increase the wear resistance, prior to processing or machining under hot conditions, and process for producing wear-resistant objects from such an aluminum alloy.

Abstract: A device for electronic collection of dust which includes an electrostatic separator and a high voltage transformer which, in conjunction with a pulse generator, supplies a pulse voltage to the separator. The output voltage of the pulse generator is superimposed on the output voltage of the transformer to cause the voltage at the electrostatic separator to exceed the spark over limit, once each cycle of the transformer output.