Turbine blade comprising a cooled platform

摘要

The present subject matter discloses a turbine component (10) including a platform (14) and an airfoil (12) extending radially upward from the platform (14). A plurality of curved cooling passages (56) may be defined in the platform (14). Each of the curved cooling passages (56) may have at least one end disposed at an exterior surface of the platform (14). Additionally, each of the cooling passages (56) may be configured to direct a cooling medium through the platform (14).