Nachwärmanordnung für einen Gasturbinenmotor

Details

Veröffentlichungs-Nr.

EP4764186

Anmeldetag

19. November 2025

Veröffentlichung

24. Juni 2026

Rechtsraum

EP

IPC

F02C7/228, F02K3/10, F23R3/20

Abstract

There is provided a reheat assembly (300A, 300B, 300C) for a gas turbine engine (10). The reheat assembly (300A, 300B, 300C) comprises a jetpipe casing (310), a support duct (340), a plurality of fuel discharge ports (362), and a fuel distribution passageway (342). The jetpipe casing (310) comprises a reheat core section (320) and a reheat bypass section (330). The support duct (340) radially separates the reheat core section (320) and the reheat bypass section (330). Each fuel discharge port (362) is configured to discharge fuel received from the fuel distribution passageway (342). The fuel distribution passageway (342) is defined by an interior channel embedded within the support duct (340).

Anmelder

Firma

Rolls-Royce plc

Land

🇬🇧 Großbritannien