NOZZLE WITH SLASH FACE(S) WITH SWEPT SURFACES WITH JOINING LINE ALIGNED WITH STIFFENING MEMBER

A nozzle (24, 224) for a turbine system (10) is disclosed. The nozzle (24, 224) includes an airfoil (40), an inner sidewall (42, 242), and an outer sidewall (44, 244). The inner sidewall (42, 242) and outer sidewall (44, 244) each includes a peripheral edge (70, 80, 270, 280) defining a pressure sid...

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Bibliographische Detailangaben
1. Verfasser:	KITTLESON, Jacob John
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 nozzle (24, 224) for a turbine system (10) is disclosed. The nozzle (24, 224) includes an airfoil (40), an inner sidewall (42, 242), and an outer sidewall (44, 244). The inner sidewall (42, 242) and outer sidewall (44, 244) each includes a peripheral edge (70, 80, 270, 280) defining a pressure side slash face (72, 82, 272, 282), a suction side slash face (74, 84, 274, 284), a leading edge face (76, 86, 276, 286), and a trailing edge face (78, 88, 278, 288). At least one of the inner sidewall (42, 242) pressure side slash face (72, 82, 272, 282), the inner sidewall (42, 242) suction side slash face (74, 84, 274, 284), the outer sidewall (44, 244) pressure side slash face (72, 82, 272, 282), or the outer sidewall (44, 244) suction side slash face (74, 84, 274, 284) includes a first swept surface (100) extending at a first angle (102) relative to an axis of the turbine system (10) and a second swept surface (104) extending at a second angle (106) relative to an axis of the turbine system (10). The first and second swept surfaces (100, 104) meet at a joining line (110) that is circumferentially aligned with the stiffening member (90).