Carburetion and combustion system for gas turbine engines

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

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Details

60749, F02C 700

Patent

active

051408201

ABSTRACT:
A carburetion and combustion system is provided in which the carburetor discharges a combustible fuel/air mixture in a rotating swirl from a plurality of nozzles at one end of a cylindrical combustion chamber, and discharges a rotating helical swirl of high-velocity compressor air concentrically surrounding the combustion mixture from a second set of nozzles. The high-velocity air swirl confines the flame propagation away from the combustible chamber walls and provides the walls with an insulating layer against the combustion heat.

REFERENCES:
patent: 3570242 (1971-03-01), Leonardi et al.
patent: 4713938 (1987-12-01), Willis

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