Combustors and gas turbine engines employing same

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

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Details

60743, 60744, 60750, F02C 722, F23R 320

Patent

active

044780451

ABSTRACT:
Combustors [22] which employ such features as rotary cup fuel atomizers and the latter in conjuction with CIVIC combustion to enhance flame performance, to produce efficient combustion over a wide operating range, and to eliminate the problems typically encountered in liquid fueled combustors, especially as they are scaled down in size. A porous or perforate barrier [180] can be used to keep large fuel drops from reaching the combustion zone [124] of the combustor. Also, an air buffer system can be employed to keep fuel from backing up to the bearings [32] by which the rotary cup [98] of the atomizer is rotatably supported, and a fuel supply line [56] with a strategically located orifice [176] can be provided to effect an interaction between fuel discharged therefrom and the buffer air. This keeps the film of fuel formed on the atomizer cup [98] from being disrupted and also keeps the buffer air from penetrating to an inner hot gas recirculation zone [130] in the combustor. The foregoing are undesirable as they cause flame instability and the generation of smoke.

REFERENCES:
patent: 2214568 (1940-09-01), Thomas
patent: 2374569 (1945-04-01), Tramontini
patent: 2416389 (1947-02-01), Heppner et al.
patent: 3287904 (1966-11-01), Warren et al.
patent: 3840328 (1974-10-01), Ashton
patent: 3919988 (1975-11-01), Bun
patent: 3933133 (1976-01-01), Shekleton
patent: 4045159 (1977-08-01), Nishi et al.
patent: 4054028 (1977-10-01), Kawaguchi
patent: 4204485 (1980-05-01), Perepolkin

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