Nachwärmanordnung für einen Gasturbinenmotor

Details

Veröffentlichungs-Nr.

EP4760152

Anmeldetag

12. November 2025

Veröffentlichung

17. Juni 2026

Rechtsraum

EP

IPC

F23R3/20, F02K3/10, F02K3/11

Abstract

The foregoing describes a reheat assembly (300) for a gas turbine engine (100). The reheat assembly (300) comprises: a support duct section (321') comprising a core side (322') for facing a core reheat region (232), and a bypass side for facing a bypass reheat region (231); a support duct (21') comprising a plurality of circumferentially spaced inlets (380), each inlet (380) being configured to communicate the bypass reheat region (231) with the core reheat region (232); a fuel supply system (360) comprising a plurality of bypass fuel injection ports (363), each bypass fuel injection port (363) being associated with an inlet (380) of the plurality of inlets (380); wherein each bypass fuel injection port (363) is configured to discharge fuel into the bypass reheat region (231) for transit through the associated inlet into the core reheat region (232).

Anmelder

Firma

Rolls-Royce plc

Land

🇬🇧 Großbritannien