F - Mech Eng,Light,Heat,Weapons – 02 – C
Patent
F - Mech Eng,Light,Heat,Weapons
02
C
F02C 7/22 (2006.01) B05B 7/00 (2006.01) B05B 7/10 (2006.01) F01D 9/06 (2006.01) F02C 1/00 (2006.01) F02G 3/00 (2006.01) F02M 61/18 (2006.01) F23R 3/28 (2006.01)
Patent
CA 2502813
A gas turbine fuel nozzle head includes an outlet passage having a curved annular transitional surface extending smoothly to a substantially radial and annular surface relative to a central axis of the fuel nozzle head, for providing a low cost and compact structure with improved cold start and altitude re-light capabilities.
Sampath Parthasarathy
Zheng Qing-Ping
Norton Rose Canada S.e.n.c.r.l.,s.r.l./llp
Pratt & Whitney Canada Corp.
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