Brennkammer für einen Gasturbinenmotor

Details

Veröffentlichungs-Nr.

EP4800299

Anmeldetag

6. Februar 2026

Veröffentlichung

2. September 2026

Rechtsraum

EP

IPC

F23R3/00, F23R3/50, F23R3/60

Abstract

A combustor (26, 26a, 26b) for a gas turbine engine (10) includes a dome (56), a cowl (60) connected with the dome (56) via an outer connection (106) and via an inner connection (112), an outer liner (54) having an outer liner first end (102) connected with the outer connection (106) and an outer liner second end (104) arranged downstream of the outer liner first end (102), an inner liner (52) having an inner liner first end (108) connected with the inner connection (112) and an inner liner second end (110) arranged downstream of the inner liner first end (108), and a combustion chamber (62) defined between the outer liner (54) and the inner liner (52). An outer piston ring assembly (114) is connected at a first end (118) to the outer connection (106) and includes a piston ring (122) at a second end (120), and an inner piston ring assembly (124) is connected at a first end (128) to the inner connection (112) and includes a piston ring (132) at a second end (130).

Anmelder

Firma

General Electric Company

Land

🇺🇸 USA

Fachgebiete