Turbine Vane Construction

摘要

A method for forming a component for use in a gas turbine engine, such as a turbine vane construction is provided. The method broadly comprises the steps of: forming a first aerodynamic structure (100) having a first platform (102) with a leading edge (104) and a trailing edge (106), and an edge (112) with an airfoil suction side structure (114); forming a second aerodynamic structure (100) having a second platform (102) with a leading edge (104) and a trailing edge (106), and an first edge (108) with an airfoil pressure side structure (110); and joining the two structures (100) together so that the airfoil suction side structure (114) mates with the airfoil pressure side structure (110) to form an airfoil (120).