Ceramic combustion liner

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

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Details

60 3966, 431352, F23D 1502, F02G 300

Patent

active

039344088

ABSTRACT:
A combustion liner for a gas turbine combustion apparatus has a wall of ceramic material. To minimize destructive thermal gradients in the ceramic material due to local cooling by air entering the liner through ports for combustion or dilution air, the walls of these ports are isolated from the entering air by metal bushings inserted through each port, these bushings being retained by a band encircling the liner and connected to the bushings.

REFERENCES:
patent: 2601390 (1952-06-01), Hague
patent: 3545202 (1970-12-01), Batt et al.
patent: 3594109 (1971-07-01), Penny

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