FIELD: continuous combustion chambers.
SUBSTANCE: method comprises generating the flow of fuel-air mixture with ignition fuel which is ignited and burnt out in the near-axis vortex, generating the periphery vortex and combustion product discharge in different cross-sections perpendicular to the axis, and generating developed periphery vortex with the use of the compressing deflector. The flow of the fuel-air mixture is generated in the spherical head of the combustion chamber and stabilized with the spreading deflector. The combustion products are burnt out in the corresponding zone of the combustion chamber.
EFFECT: stabilized fuel combustion.
4 dwg
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Authors
Dates
2005-07-20—Published
2004-08-16—Filed