Invention Grant
US08109712B2 Method of producing a turbine or compressor component, and turbine or compressor component 失效
制造涡轮机或压缩机部件的方法,以及涡轮机或压缩机部件

Method of producing a turbine or compressor component, and turbine or compressor component
Abstract:
Disclosed is a turbine or compressor component with an integrated cooling channel, in particular a turbine blade, and a method for producing the same. The cooling channel of the component is subjected to internal pressure during a pressure impingement phase, the internal pressure being at a level sufficiently high that it causes the at least semiplastic deformation of the wall regions delimiting the cooling channel.
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