Gasturbinenbrennkammer

Details

Veröffentlichungs-Nr.

EP3141817

Aktenzeichen

EP16187715

Anmeldetag

7. September 2016

Veröffentlichung

4. Dezember 2019

Erteilung

4. Dezember 2019

Rechtsraum

EP

IPC

F23R3/10F23R3/12F23R3/28

Abstract

A gas turbine combustor (2) includes: an inner casing (10); an outer casing (11); an annular flow path (48) disposed between the inner casing (10) and the outer casing (11); a fuel header (40); a plurality of fuel nozzles (91) supported concentrically on the fuel header (40); an air hole plate (32) having a plurality of air holes (33) associated with the respective fuel nozzles (91); a guide (37) having a wall portion (37A) and a bent portion (37B); and an outer peripheral flow path (94) defined between the outer peripheral surface of the air hole plate (32) and the inner casing (10).

Anmelder

Firma

Mitsubishi Hitachi Power Systems, Ltd.

Land

🇯🇵 Japan

Fachgebiete