Integral fuel nozzle cover for gas turbine combustor

Details Integral fuel nozzle cover for gas turbine combustor Integral fuel nozzle cover for gas turbine combustor

1988-12-22

1990-06-05

Kashnikow, Andres

Fluid sprinkling, spraying, and diffusing

Combining of separately supplied fluids

At or beyond outlet

239428, 239548, F23L 100, B05B 706

Patent

active

049307037

ABSTRACT:
A nozzle cover for a combustor of a combination fuel gas turbine engine is cast as a one-piece integral part requiring machining only for holes, sealing surfaces and threads. The nozzle cover cross section is generally a portion of an ellipsoid in order to maximize strength for a given amount of material. An interface between the nozzle cover and each of a plurality of combination fuel nozzles employs a single threaded opening accommodating two of a required three nozzles. The third nozzle in each combination fuel nozzle is accommodated in threads formed in a stepped wall in the nozzle cover.

REFERENCES:
patent: 233397 (1880-10-01), Bradley
patent: 622482 (1899-02-01), Jackson
patent: 878461 (1908-02-01), Harris
patent: 1741532 (1929-12-01), Morse
patent: 4797087 (1989-01-01), Gitman

Affiliated with

Also associated with

Rating

Integral fuel nozzle cover for gas turbine combustor does not yet have a rating. At this time, there are no reviews or comments for this patent.

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

Rate now

Comments { 0 }

Profile ID: LFUS-PAI-O-486555