Two stage (premixed/diffusion) gas only secondary fuel nozzle

Power plants – Combustion products used as motive fluid – Combustion products generator

Patent

Rate now

  [ 0.00 ] – not rated yet Voters 0   Comments 0

Details

60746, F23R 334

Patent

active

051992655

ABSTRACT:
A secondary nozzle for a gas turbine includes an elongated, tubular nozzle body having an inlet end and an outlet end; a tubular core assembly having an outer diameter less than an interior diameter of the tubular nozzle body to thereby define a diffusion fuel passage between the core assembly and the tubular nozzle body extending to the outlet end, and a premix fuel passage through the core assembly extending to a pilot orifice at the outlet end; an air passage located along at least a portion of the tubular nozzle body and located radially between the diffusion and premix fuel passages; and, a plurality of gas injectors extending radially out of the elongated tubular nozzle body from the premix fuel passage.

REFERENCES:
patent: 2955420 (1960-10-01), Schirmer
patent: 2999359 (1961-09-01), Murray
patent: 3048014 (1962-08-01), Schmidt
patent: 3946553 (1976-03-01), Roberts et al.
patent: 3958416 (1976-05-01), Hammond, Jr. et al.
patent: 3973395 (1976-08-01), Markowski et al.
patent: 4112676 (1978-09-01), DeCorso
patent: 4173118 (1979-11-01), Kawaguchi
patent: 4193260 (1980-03-01), Carlisle et al.
patent: 4262482 (1981-04-01), Roffe et al.
patent: 4292801 (1981-10-01), Wilkes et al.
patent: 4389848 (1983-06-01), Markowski et al.
patent: 4420929 (1983-12-01), Jorgensen et al.
patent: 4498288 (1985-02-01), Vogt
patent: 4589260 (1986-05-01), Krockow
patent: 4603548 (1986-08-01), Ishibashi et al.
patent: 4683715 (1987-08-01), Iizuka et al.
patent: 4698963 (1987-10-01), Taylor
patent: 4716719 (1988-01-01), Takahashi et al.
patent: 4787208 (1988-11-01), DeCorso
patent: 4805411 (1989-02-01), Hellat et al.
patent: 4944149 (1990-07-01), Kuwata
patent: 4949538 (1990-08-01), Iasillo et al.
patent: 4967561 (1990-11-01), Bruhwiler et al.
patent: 4974415 (1990-12-01), Shekleton et al.
patent: 4982570 (1991-01-01), Waslo et al.
patent: 4984429 (1991-01-01), Waslo et al.
patent: 5030871 (1991-07-01), Shah et al.
patent: 5054280 (1991-10-01), Ishibashi et al.
patent: 5081843 (1992-01-01), Ishibashi et al.
"Gas Turbine Combustion and Emissions", Gas Turbine Reference Library, Dr. L. B. Davis, Jr., GE Company (no date).
"General Electric Gas Turbine Multiple-Combustion System", Gas Turbine Reference Library, Edward J. Walsh, GE Company, 1984.
"Dry Low NOx Combustion System for Utility Gas Turbine", AMSE, R. M. Washam, GE Company, 1983.
"Development of a Dry Low NOx Combustor", AMSE, Davis & Washam, GE Company, Jun. 1989.

LandOfFree

Say what you really think

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

Rating

Two stage (premixed/diffusion) gas only secondary fuel nozzle does not yet have a rating. At this time, there are no reviews or comments for this patent.

If you have personal experience with Two stage (premixed/diffusion) gas only secondary fuel nozzle, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Two stage (premixed/diffusion) gas only secondary fuel nozzle will most certainly appreciate the feedback.

Rate now

     

Profile ID: LFUS-PAI-O-528362

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