Heat shielding for a turbine combustor

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

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Details

60752, 60756, F23R 300, F02C 100

Patent

active

059748052

ABSTRACT:
A combustor for a gas turbine engine has a fuel nozzle located in the upstream end thereof and is positioned within a cylinder coaxial with said nozzle. The cylinder comprises at its downstream end an annular flange extending from the cylinder in a generally radial direction. The flange has a plurality of cooling air apertures radially extending therethrough so as to direct cooling air along the face of an adjacent heatshield.

REFERENCES:
patent: 2907171 (1959-10-01), Lysholm
patent: 3656297 (1972-04-01), Monk
patent: 4766722 (1988-08-01), Bayle-Laboure et al.
patent: 4870818 (1989-10-01), Suliga
patent: 4914918 (1990-04-01), Sullivan
patent: 4999996 (1991-03-01), Duchene et al.
patent: 5419115 (1995-05-01), Butler et al.
patent: 5581999 (1996-12-01), Johnson

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