Airflow testing method and system for multiple cavity blades and vanes

摘要

A system for airflow testing a turbine engine component (12) having multiple cavities (22, 24, 26) has a test fixture (10) with a module for supporting a turbine engine component (12) to be tested and a sliding element (46) for sequentially allowing a pressurized fluid to flow through each of the multiple cavities (22, 24, 26) in the turbine engine component (12). A method for performing the airflow testing is also described.