COOLED HOT GAS PATH COMPONENTS INCLUDING A PLURALITY OF NOZZLES AND VENTURIES

Hot gas path (HGP) components (100, 200) for turbine systems (10) are disclosed. The HGP component (100, 200) may include a body (110, 210) including a forward end (120, 220), an aft end (122, 222), and an inner portion (132, 232) positioned adjacent a hot gas flow path for the turbine system (10)....

Ausführliche Beschreibung

Gespeichert in:

Bibliographische Detailangaben
1. Verfasser:	WIDENER, Stanley Kevin
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	ADDITIVE MANUFACTURING TECHNOLOGY ADDITIVE MANUFACTURING, i.e. MANUFACTURING OFTHREE-DIMENSIONAL [3-D] OBJECTS BY ADDITIVE DEPOSITION, ADDITIVEAGGLOMERATION OR ADDITIVE LAYERING, e.g. BY 3-D PRINTING,STEREOLITHOGRAPHY OR SELECTIVE LASER SINTERING BLASTING ENGINE PLANTS IN GENERAL HEATING LIGHTING MACHINES OR ENGINES IN GENERAL MECHANICAL ENGINEERING NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES PERFORMING OPERATIONS STEAM ENGINES TRANSPORTING WEAPONS
Online-Zugang:	Volltext bestellen
Tags:	Tag hinzufügen Keine Tags, Fügen Sie den ersten Tag hinzu!

Beschreibung
Zusammenfassung:	Hot gas path (HGP) components (100, 200) for turbine systems (10) are disclosed. The HGP component (100, 200) may include a body (110, 210) including a forward end (120, 220), an aft end (122, 222), and an inner portion (132, 232) positioned adjacent a hot gas flow path for the turbine system (10). The body (110, 210) may also include an outer portion (134, 234) formed radially opposite the inner portion (132, 232), and a plurality of nozzles (146, 246) extending through the outer portion (134, 234). Additionally, body (110, 210) may include an intermediate portion (136, 236) formed between the inner portion (132, 232) and the outer portion (134, 234), and a plurality of venturi (148, 248) extending through the intermediate portion (136, 236). The plurality of venturi (148, 248) may be in fluid communication with the plurality of nozzles (146, 246).