Coated high temperature combustor liner

Details Coated high temperature combustor liner Coated high temperature combustor liner

1983-12-21

1987-04-07

Croyle, Carlton R.

Power plants

Combustion products used as motive fluid

Combustion products generator

60757, F02C 100, F02G 300

Patent

active

046550445

ABSTRACT:
Each panel of the louver liner of the combustor of a gas turbine engine is coated with a ceramic composition on the surface adjacent the combustion zone with a tapered end at the lip of the cooling air film generating mechanism. A second taper may be incorporated at the back side of the lip of the next adjacent cooling air film generating mechanism.

REFERENCES:
patent: 2937595 (1960-05-01), Margulis et al.
patent: 3101592 (1963-08-01), Robertson et al.
patent: 3918255 (1975-11-01), Holden
patent: 3956886 (1976-05-01), Sedgwick
patent: 3982850 (1976-09-01), Jenkinson
patent: 3995422 (1976-12-01), Stamm
patent: 4077205 (1978-03-01), Pane et al.
patent: 4255495 (1981-03-01), Levine et al.
patent: 4259842 (1981-04-01), Koshoffer
patent: 4380906 (1983-04-01), Dierberger
patent: 4485630 (1984-12-01), Kenworthy

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