Combustion chamber and process utilizing a premix chamber of a p

Power plants – Combustion products used as motive fluid

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60 3965, 60 3969, 60 3971, 60 3974R, 431352, 239145, F02C 722

Patent

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039370070

ABSTRACT:
Combustion chamber apparatus and process for use in gas turbine engines including a premix chamber bounded by porous ceramic material and a combustion chamber immediately adjacent a porous ceramic diaphragm which bounds the premix chamber. In this premix chamber, partial vaporization of the fuel, without combustion, takes place so as to improve combustion efficiency and shorten the length of the flame tube or combustion chamber needed for complete efficient combustion of the fuel. Primary air is introduced into the premix chamber, which passes with the fuel into the flame tube or combustion chamber, for futher mixture with secondary and tertiary air.

REFERENCES:
patent: 3187799 (1965-06-01), Nesbitt
patent: 3368604 (1968-02-01), Mutchler
patent: 3810732 (1974-05-01), Koch

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