Abstract: A method and device for the heat treatment of a profile, in particular an extruded profile for aircraft. The profile may be formed by one or more different, in particular curable, aluminium alloys. The method provides that at least two regions of a profile are subjected to a different heat treatment. The device includes a first chamber that encloses a first region of a profile and a second chamber that encloses a second region of the profile, wherein different temperatures can be set in the first and second chambers. The profile has at least two regions that each have different material properties and are formed by differential heat treatment.

Abstract: A method and device for the heat treatment of a profile, in particular an extruded profile for aircraft. The profile may be formed by one or more different, in particular curable, aluminium alloys. The method provides that at least two regions of a profile are subjected to a different heat treatment. The device includes a first chamber that encloses a first region of a profile and a second chamber that encloses a second region of the profile, wherein different temperatures can be set in the first and second chambers. The profile has at least two regions that each have different material properties and are formed by differential heat treatment.

Abstract: A method is provided for forming complex structures from aluminum alloys, particularly from naturally hard AlMg alloys, naturally hard AlMgSc alloys and/or age-hardenable AlMgLi alloys. The method, in a simple manner by means of as few process steps as possible, forms complex structures from the alloys such that they almost assume their final shape without any significant spring-back. Simultaneously, the loss of material is to be kept as low as possible. This is achieved by means of the following steps: elastic forming of a component to be formed into a defined contour under the effect of external force; and heating-up of the elastically formed component to a temperature higher than the temperature required for a creep formation and relaxation of stresses of the alloy, so that the component is formed while retaining the contour.

Abstract: The present invention relates to a method of forming complex structures from aluminum alloys, particularly from naturally hard AlMg alloys, naturally hard AlMgSc alloys and/or age-hardenable AlMgLi alloys. It is an object of the invention to provide such a method by means of which, in a simple manner, that is, by means of as few process steps as possible, complex structures can be formed from the alloys according to the invention such that they almost assume their final shape without any significant spring-back. Simultaneously, the loss of material is to be kept as low as possible.

Abstract: A drawing mold has a contoured mold surface receiving a metal sheet thereon. A tensile drawing machine applies a drawing tension to the sheet edges to deform the sheet onto the mold. Heated pressurized air supplied through air holes in the mold surface forms an air cushion between the sheet and the mold, to heat and support the sheet without friction. A forming method includes: a pre-stressing phase of pre-stressing and pre-bending the sheet at room temperature and atmospheric pressure; a heating phase of heating the sheet with the pressurized air at an elevated temperature and intermediate elevated pressure; a forming phase of maintaining the temperature and increasing the pressure to support the sheet on the air cushion, and drawing the sheet with the tensile drawing machine; and a cooling phase of cooling the sheet without further deformation, with the air at the intermediate pressure and cooled to room temperature.

Abstract: A drawing mold has a contoured mold surface receiving a metal sheet thereon. A tensile drawing machine applies a drawing tension to the sheet edges to deform the sheet onto the mold. Heated pressurized air supplied through air holes in the mold surface forms an air cushion between the sheet and the mold, to heat and support the sheet without friction. A forming method includes: a pre-stressing phase of pre-stressing and pre-bending the sheet at room temperature and atmospheric pressure; a heating phase of heating the sheet with the pressurized air at an elevated temperature and intermediate elevated pressure; a forming phase of maintaining the temperature and increasing the pressure to support the sheet on the air cushion, and drawing the sheet with the tensile drawing machine; and a cooling phase of cooling the sheet without further deformation, with the air at the intermediate pressure and cooled to room temperature.