Turbinensystem mit einem Übergangskanal

Details

Veröffentlichungs-Nr.

EP2578808

Aktenzeichen

EP12186896

Anmeldetag

1. Oktober 2012

Veröffentlichung

12. Juni 2019

Erteilung

12. Juni 2019

Rechtsraum

EP

IPC

F01D9/02

Abstract

A turbine system is disclosed. The turbine system (10) includes a transition duct (50) having an inlet (52), an outlet (54), and a passage (56) extending between the inlet (52) and the outlet (54) and defining a longitudinal axis (90), a radial axis (94), and a tangential axis (92). The outlet (54) of the transition duct (50) is offset from the inlet (52) along the longitudinal axis (90) and the tangential axis (92). The turbine system further includes a turbine section (16) connected to the transition duct (50). The turbine section includes a plurality of shroud blocks at least partially defining a hot gas path, a plurality of buckets at least partially disposed in the hot gas path, and a plurality of nozzles at least partially disposed in the hot gas path. At least one of a shroud block, a bucket, or a nozzle includes means for withstanding high temperatures.

Anmelder

Firma

General Electric Company

Land

🇺🇸 USA

Fachgebiete