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: The invention relates to a crucible induction furnace for producing cast parts consisting of aluminum and magnesium alloys, especially particle-reinforced alloys. According to the invention, the material being melted is directly, inductively heated and stirred in an electrically non-conductive, refractory lining or crucible.

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: The invention provides a metal alloy made from a metal matrix with added nucleating particles which causes uniform formation of bubbles and a homogenous foam structure. The invention also provides a method for producing metal foamed bodies including the following steps: producing a homogeneous mixture of at least one metal powder forming a metal matrix, a powder made of or made with nucleating particles causing uniform formation of bubbles and a homogenous foam structure, and at least one gas-generating gasifying agent powder; introducing the mixture into a mold or compacting the mixture under pressure, e.g., by cold or hot isostatic pressing, followed by hot forming, e.g., by extrusion or rolling, and optional further processing, e.g., by cold forming and/or machining; foaming by heating to a temperature above the temperature of decomposition of the gasifying agent, preferably inside the temperature range of the melting point of the metal used; and subsequent cooling of the body thus foamed.