TURBINE NOZZLE COMPLIANT JOINTS AND ADDITIVE METHODS OF MANUFACTURING THE SAME

A turbine nozzle 231 formed of a superalloy, and including: an annular end-wall 222 including a pocket 315, the pocket 315 defining an inner surface within the annular end-wall; a vane 223, the vane including an airfoil portion 323 and a boss portion 321 , the vane extending from the pocket 315 such...

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Bibliographische Detailangaben
Hauptverfasser: BIERY, Shannon, MADER, Morgan, STIMPSON, Curtis, MORRIS, Mark
Format: Patent
Sprache:eng ; fre ; ger
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