Turbinenmotorbrennkammer mit einem Ersten Kraftstoffinjektor und einem Zweiten Kraftstoffinjektor

Details

Veröffentlichungs-Nr.

EP4745462

Anmeldetag

11. November 2025

Veröffentlichung

20. Mai 2026

Rechtsraum

EP

Abstract

A turbine engine (10) includes a compression section (12), a combustion section (14), and a turbine section (16) in serial flow arrangement. The combustion section (14) has a combustor (30) including a combustor liner (40) at least partially defining a combustion chamber (74) exhausting at a combustion chamber outlet (76), with the combustor liner (40) having an inner liner (42) and an outer liner (44). A liquid fuel injector (70) is configured to inject a first mixture comprised of liquid fuel and air or atomized liquid fuel and air to the combustion chamber (74) and a gaseous fuel injector (72) is configured to inject a second mixture comprised of gaseous fuel and air or atomized fuel and air to the combustion chamber (74).

Anmelder

Firma

General Electric Company

Land

🇺🇸 USA