Gas turbine fuel nozzle assembly

F - Mech Eng,Light,Heat,Weapons – 23 – R

Patent

Rate now

  [ 0.00 ] – not rated yet Voters 0   Comments 0

Details

F23R 3/28 (2006.01) F02C 3/14 (2006.01) F02C 3/30 (2006.01) F23D 17/00 (2006.01) F23L 7/00 (2006.01) F23R 3/36 (2006.01)

Patent

CA 2104523

ABSTRACT OF THE DISCLOSURE A fuel nozzle assembly is provided having the capability of burning either gaseous or liquid fuel, or both simultaneously, along with steam injection. The nozzle has a nozzle body that is attached to a nozzle cap by inner, outer and middle sleeves. The sleeves form inner and outer concentric annular conduits between themselves for directing the flow of gaseous fuel and steam from the fuel and steam inlet ports to the outlet ports. In addition, the inner sleeve forms a central chamber in which an oil fuel nozzle is disposed. Radial passages in the nozzle body allow cooling air to flow over the oil nozzle and through the oil outlet port, thereby preventing coking at the nozzle tip. The fuel nozzle assembly is originally built, and the nozzle cap is replaced, by sliding the sleeves forward and aft on the assembly so as to gain access to the next innermost sleeve.

LandOfFree

Say what you really think

Search LandOfFree.com for Canadian inventors and patents. Rate them and share your experience with other people.

Rating

Gas turbine fuel nozzle assembly does not yet have a rating. At this time, there are no reviews or comments for this patent.

If you have personal experience with Gas turbine fuel nozzle assembly, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Gas turbine fuel nozzle assembly will most certainly appreciate the feedback.

Rate now

     

Profile ID: LFCA-PAI-O-1443938

  Search
All data on this website is collected from public sources. Our data reflects the most accurate information available at the time of publication.