Wasserstofffähiger Kraftstoffinjektor

Details

Veröffentlichungs-Nr.

EP4756291

Anmeldetag

16. September 2025

Veröffentlichung

10. Juni 2026

Rechtsraum

EP

IPC

F23R3/28, F23R3/34

Abstract

A fuel injector (200) for a gas turbine combustor (17) is provided. The fuel injector (200) includes an annular main body (300) extending from a first end (301) to a second end (302). The annular main body (300) defines a centerline axis (303) extending from the first end (301) to the second end (302), and at least a portion of a fuel circuit (320) extends along the centerline axis (303). A first plurality of fluid inlets (345) is disposed about the fuel circuit (320), and a second plurality of fluid inlets (350) is disposed about the first plurality of fluid inlets (345). The fuel circuit (320) includes a fuel inlet (324) and a fuel outlet (330) in fluid communication with the fuel inlet (324). An exterior surface of the fuel outlet (330) forms a fuel outlet angle (500) relative to the centerline axis (303).

Anmelder

Firma

GE Vernova Technology GmbH

Land

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