Turbinentriebwerk und Brennstoffdüsenanordnung dafür

Details

Veröffentlichungs-Nr.

EP4722597

Anmeldetag

18. September 2025

Veröffentlichung

8. April 2026

Rechtsraum

EP

IPC

F23R3/28, F23R3/50

Abstract

A turbine engine (10), comprising a compressor section (12), a combustion section (14), and a turbine section (16) in a serial flow arrangement, with the combustion section (14) further comprising a combustor liner (40) at least partially defining a combustion chamber (50), and a gaseous fuel nozzle assembly (48). The gaseous fuel nozzle assembly (48) comprises a set of mixing tubes (100), a set of fuel jets (114) and an air passage (120), the air passage (120) including a set of air passage outlets (126), with each air passage outlet of the set of air passage outlets (126) tangentially, fluidly coupled to a corresponding mixing tube air inlet (106).

Anmelder

Firma

General Electric Company

Land

🇺🇸 USA

Fachgebiete