GAS TURBINE COMPONENT AND A GAS TURBINE ENGINE COMPRISING THE COMPONENT
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United States of America Patent
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Issued Date -
Nov 24, 2011
app pub date -
Jun 17, 2008
filing date -
Jun 17, 2008
priority date (Note) -
Abandoned
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Abstract
A gas turbine component includes an element having a relatively weak region with regard to stress loads in operation, the component including at least one elongated stiffening structure which extends on at least one side of the weak region, and the elongated stiffening structure is connected to the element in a load-transmitting manner and adapted to form a load path in its extension direction.
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