Verbrennungstufungssystem

Details

Veröffentlichungs-Nr.

EP3070408

Aktenzeichen

EP16158876

Anmeldetag

7. März 2016

Veröffentlichung

6. Juni 2018

Erteilung

6. Juni 2018

Rechtsraum

EP

IPC

F23R3/34F23K5/06F23K5/14F02C7/228F02C7/232

Abstract

A combustion staging system (30) is provided for fuel injectors of a multi-stage combustor of a gas turbine engine. The system has a splitting unit (35) which receives a metered fuel flow and controllably splits the metered fuel flow into out-going pilot and mains fuel flows to perform pilot-only and pilot-and-mains staging control of the combustor. The system further has pilot (31, 32) and mains fuel (33) manifolds which respectively receive the pilot and mains fuel flows. The system further has a plurality of parallel mains flow scheduling valves (40) which distribute the mains fuel flow from the mains manifold to mains discharge orifices of respective injectors of the combustor. The mains flow scheduling valves also pass the pilot fuel flow to pilot discharge orifices of the respective injectors. Each mains flow scheduling valve has a chamber containing a movable piston, the chamber to a pilot side of the piston being in fluid communication with the pilot fuel manifold and the chamber to a mains side of the piston being in fluid communication with the mains fuel manifold. The piston is biased towards a closed pilot-only position which prevents flow out of the mains side of the chamber to the mains discharge orifice of the respective injector. The piston is movable under an increase in pressure in the mains fuel manifold to an open pilot-and-mains position which allows flow out of the mains side of the chamber to the mains discharge orifice of the respective injector.

Anmelder

Firmen

Rolls-Royce PLC
Rolls-Royce Controls and Data Services Limited

Land

🇬🇧 Großbritannien

Fachgebiete