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We have been providing secure, reliable, virus-free web access to the internet since 1998.Structure and strength of workpieces that undergo complex geometrical and material changes during processing are of increasing interest in recent years. This is seen, for example, in the case of turbine blades, where an increase in the operating temperature for the gas turbine leads to a rise in the thermal and mechanical loads on the turbine blade. Particularly exposed to this thermal and mechanical load are the inside and the outside walls of the turbine blade. One possibility for reducing the thermal and mechanical loads of turbine blades is to reduce the temperature and the mechanical loading of the base material of the turbine blade. One approach to this is to produce turbine blades whose walls are formed of a material which can better withstand thermal and mechanical loads. Also, a problem with the cooling systems that are frequently used with turbine blades is that they frequently achieve their cooling effect only over a very short region of the interior of the wall of the turbine blade.
A turbine blade is usually composed of a root part and a blade part, which are connected via hinged joints. It is, moreover, customary to provide an undercut for the support of the root part at its underside. With a view to improving the strength and the stiffness of the blade part, it is known to refine, in a so-called elongation zone, an inner wall of the blade part, which inner wall is located opposite the root part. The elongation zone is produced by impressing the blade part and the root part with pressure and heat during a heat treatment of the blade part and root part, and deformation of the material of the blade part and the root part takes place in an area which is to be refined. This deformation produces a longitudinal elongation, which is usually arranged transverse to the axis of the blade part. With the aid of this production process, the blade wall can be formed in such a way that it
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