Combustor liner for gas turbine engine

Power plants – Combustion products used as motive fluid – External-combustion engine type

Patent

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Details

60 3966, F02C 718

Patent

active

041320662

ABSTRACT:
This invention relates to an improvement of the cooling air flow distribution in proximity to the combustion and dilution air holes of a combustor liner fabricated from Finwall.RTM. material for a turbine type power plant.

REFERENCES:
patent: 3064425 (1962-11-01), Hayes
patent: 3545202 (1970-12-01), Batt et al.
patent: 3899876 (1975-08-01), Williamson
patent: 3899882 (1975-08-01), Parker

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