Airflow testing method and system for multiple cavity blades and vanes

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 mu...

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Bibliographische Detailangaben
Hauptverfasser:	Varsell, Richard, Davis, Thomas R, Mironets, Sergey, Pietraszkiewicz, Edward F
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	BLASTING ENGINE PLANTS IN GENERAL HEATING LIGHTING MACHINES OR ENGINES IN GENERAL MECHANICAL ENGINEERING NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES STEAM ENGINES WEAPONS
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Beschreibung
Zusammenfassung:	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.