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Because of their good properties, the γ‐TiAl based alloys are promising to replace the twice as dense yet established nickel‐based alloys e.g. in turbine blades and especially low pressure turbine blades in aircraft engines. The serial production of such parts made of the γ‐TiAl based alloys requires the development of a stable processing route. However, during forging, the starting material's properties...
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