Manufacturing method for obtaining high-temperature components for gas turbines and components thus obtained
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United States of America Patent
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Issued Date -
Sep 7, 2006
app pub date -
Dec 10, 2003
filing date -
Dec 18, 2002
priority date (Note) -
Abandoned
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Abstract
A manufacturing method for obtaining high-temperature components (10) for gas turbines, which comprises at least incorporation of an element or insert (14) in a main body (12) of the component (10), this element or insert (14) having mechanical properties able to withstand stresses to which said component (10) is subject in a zone where the said element or insert (14) is arranged; the invention also relates to a high temperature component thus obtained.
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