Fuel trim system for a multiple chamber gas turbine...

Details Fuel trim system for a multiple chamber gas turbine... Fuel trim system for a multiple chamber gas turbine...

F - Mech Eng,Light,Heat,Weapons

02

C

F02C 9/20 (2006.01) F02C 7/228 (2006.01) F02C 9/28 (2006.01) F02C 9/32 (2006.01) F02C 9/34 (2006.01) F23R 3/34 (2006.01)

Patent

CA 2103429

A fuel trimming unit has bean adapted to each combustion chamber in a multi-chamber combustor of an industrial gas turbine. The fuel trim unit matches the combustion air flows into each combustion chamber. This adjusts the fuel-air mixture to account for air floss variations into the individual combustion ruction zones of each combustion chamber. Because of the fuel trim unit, a uniform fuel-air mixture is provided to each combustion chamber in a gas turbine. The foal trim unit is adjusted using sensor inputs of the fuel flow rata to each combustion chamber, the dynamic pressure in each combustion chamber, and the turbine exhaust temperature.

Affiliated with

Also associated with

Rating

Fuel trim system for a multiple chamber gas turbine... does not yet have a rating. At this time, there are no reviews or comments for this patent.

If you have personal experience with Fuel trim system for a multiple chamber gas turbine..., we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Fuel trim system for a multiple chamber gas turbine... will most certainly appreciate the feedback.

Rate now

Comments { 0 }

Profile ID: LFCA-PAI-O-2060288