GAS TURBINE ENGINE AIRFLOW MEMBER, CORRESPONDING TURBOMACHINE COMPONENT AND MANUFACTURING METHOD

摘要

A gas turbine engine airflow member including a blade core portion, a shroud tip portion extending from the blade core portion, and an airfoil portion formed exteriorly to the blade core portion, where the blade core portion and the shroud tip portion are constructed as a first unitary structure and the airfoil portion is constructed as a second structure. A method of forming a gas turbine engine component is also disclosed.