Combustion apparatus for gas turbine engines

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

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Details

60 3971, 60 3974R, 431177, 431186, 239432, 239512, 239515, F02C 722

Patent

active

039614751

ABSTRACT:
A combustion chamber for a gas turbine engine which has staged combustion in two toroidal vortices of opposite hand arranged one upstream of the other. A burner delivers air/fuel mixture in a radial direction to support the vortices and the burner has a convergent outlet for the air/fuel mixture.

REFERENCES:
patent: 2999359 (1961-09-01), Murray
patent: 3430443 (1969-03-01), Richardson et al.
patent: 3724207 (1973-04-01), Johnson

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