Combustor for a gas turbine engine

Details Combustor for a gas turbine engine Combustor for a gas turbine engine

1984-09-17

1985-10-29

Casaregola, Louis J.

Power plants

Combustion products used as motive fluid

Combustion products generator

60759, 60760, F02C 722

Patent

active

045494029

ABSTRACT:
A combustor for a gas turbine is provided, the combustor including a reverse flow type combustion chamber defined by an inner cylindrical wall and an outer wall concentric with the inner wall and connected at one end by an annular dome. The outer wall has three successive sections with the first section being cylindrical and of a predetermined diameter, the second outer wall section being of frusto-conical shape, and the third wall section being of cylindrical shape but of reduced diameter compared to the first section. Injectors are provided in the angled wall of the second outer wall section, and openings are provided annular with the injectors to allow compressor delivered air to enter directly into the combustion chamber surrounding the injector, the injector being directed towards the primary zone.

REFERENCES:
patent: 2780061 (1957-02-01), Clarke et al.
patent: 2956404 (1960-10-01), Kassner et al.
patent: 2974487 (1961-03-01), Stokes et al.
patent: 3633361 (1972-01-01), Vanves
patent: 3691766 (1972-09-01), Champion
patent: 3844116 (1974-09-01), Matto

Affiliated with

Also associated with

Rating

Combustor for a gas turbine engine does not yet have a rating. At this time, there are no reviews or comments for this patent.

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

Rate now

Comments { 0 }

Profile ID: LFUS-PAI-O-723393