Combustion liner for a gas turbine engine

Details Combustion liner for a gas turbine engine Combustion liner for a gas turbine engine

1985-01-07

1986-11-18

Casaregola, Louis J.

Power plants

Combustion products used as motive fluid

Combustion products generator

60755, F02C 100, F02G 300

Patent

active

046228217

ABSTRACT:
The liner of a combustor for a gas turbine engine is constructed to include a refilmer at the combustion/dilution air holes so as to form a film of cool air along the inner surface of the liner in the combustion, that would otherwise be destroyed by the combustion/dilution air.

REFERENCES:
patent: 2699648 (1955-01-01), Berkey
patent: 3656297 (1972-04-01), Monk
patent: 3899876 (1975-08-01), Williamson
patent: 4132066 (1979-01-01), Austin, Jr. et al.
patent: 4361010 (1982-11-01), Tanrikut et al.
patent: 4380906 (1983-04-01), Dierberger
patent: 4549402 (1985-10-01), Saintsbury et al.

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