APPARATUS FOR TESTING CREEP OF TURBINE BLADE

An apparatus for testing creep of a turbine blade comprises: a first support portion for supporting one end of a turbine blade; a plurality of elastic members, each having one side end connected to the other surface opposite to one surface of the first support portion, which faces toward the one end of the turbine blade, wherein at least a few of the elastic members have a different elastic modulus; a connection portion connected to the other side end of the elastic member to support the elastic member; a second support portion for supporting the other end of the turbine blade; an actuator for applying tensile force to at least one of the connection portion and the second support portion; and a heating portion disposed adjacent to a surface of the turbine blade so as to apply heat to the surface of the turbine blade.