Directionally Solidified Alloy
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CM 247 LC is a derivative of MAR M 247 composition, primarily designed for directionally solidified (DS) turbine blade and vane applications. The modified alloy is a development of Cannon Muskegon Corporation. Twelve years of successful flight engine DS turbine blade and vane service experience has occurred.
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Beyond the DS experience, fine grained integral wheel casting application has ensued. Besides the advantages the alloy provides to castability and ductility, it also achieves approximately half the MAR M 247 crack growth rate of the similarly fine grain processed MAR M 247 alloy.
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The exceptional castability of CM 247 LC has resulted in its selection for conventionally cast vanes, nozzles and structural turbine components for aero and industrial gas turbines.
Extensive industrial turbine applications for DS blade and vane components have developed in CM247 LC where natural gas is used a fuel.
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