Turbinenmotor mit einem Brennabschnitt

Details

Veröffentlichungs-Nr.

EP4711596

Anmeldetag

13. August 2025

Veröffentlichung

18. März 2026

Rechtsraum

EP

Abstract

A turbine engine (100) has a compression section, a combustion section (102), a turbine section in serial flow arrangement and defining a working airflow (Fw) path (182). The combustion section (102) has a circumferential casing (104), a combustor (106), and a fuel nozzle (130). The circumferential casing (104) defines an interior (108). The turbine engine (100) includes a deswirler assembly (134). The deswirler assembly (134) couples the working airflow (Fw) path (182) of the compression section to the interior (108). The turbine engine (100) includes a fuel supply system (140).

Anmelder

Firma

General Electric Company

Land

🇺🇸 USA