Global Patent Index - EP 0939275 A3

EP 0939275 A3 19990929 -

Publication

EP 0939275 A3 19990929

Application

EP 98310791 A 19981230

Priority

US 89797 A 19971230

Abstract (en)

[origin: EP0939275A2] A fuel nozzle/guide assembly for a gas turbine engine for reducing NOx emissions has a central axial inflow swirler (32) and either three concentric radial inflow swirlers (34, 62, 88) or, alternatively, two concentric radial inflow swirlers (34, 62) and a concentric array of air passages (74), for rapid uniform fuel-air mixing downstream from the fuel injector. <IMAGE>

IPC 1-7

F23C 7/00; F23C 5/02; F23D 11/10; F23R 3/10; F23R 3/28

IPC 8 full level

F02C 7/232 (2006.01); F23C 7/00 (2006.01); F23C 7/02 (2006.01); F23D 11/10 (2006.01); F23R 3/14 (2006.01); F23R 3/58 (2006.01)

CPC (source: EP)

F23C 7/004 (2013.01); F23C 7/02 (2013.01); F23D 11/107 (2013.01); F23R 3/14 (2013.01); F23C 2900/03004 (2013.01); F23C 2900/06043 (2013.01); F23C 2900/07001 (2013.01); F23D 2206/10 (2013.01); F23D 2900/11101 (2013.01)

Citation (search report)

Designated contracting state (EPC)

AT BE CH CY DE DK ES FI FR GB GR IE IT LI LU MC NL PT SE

DOCDB simple family (publication)

EP 0939275 A2 19990901; EP 0939275 A3 19990929; JP H11257664 A 19990921

DOCDB simple family (application)

EP 98310791 A 19981230; JP 37287198 A 19981228