Afterburner structure with self-excited sweeping oscillating fuel injection nozzles
AssigneeAero Engine Academy of China
InventorsShiqi Wang, Quan Wen, Xiao Han
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AssigneeAero Engine Academy of China
InventorsShiqi Wang, Quan Wen, Xiao Han
Estimating the term…
The present disclosure relates to an afterburner structure with fuel injection nozzles. In the condition of a stable inlet flow, the present disclosure forms a sweeping oscillating jet with a certain frequency at the outlet under an alternate feedback action of a feedback channel and the fluid's Coanda effect, so that the spatial uniformity of the fuel injection is improved; Therefore, without increasing the structural complexity of current afterburner of the turbo-engine and the combustion chamber of the subsonic combustion ramjet, the atomization performance and the uniformity of the oil-gas mixture in the afterburner/combustion chamber of the ramjet can be greatly improved, the combustion efficiency and combustion instability of the engine can be improved and meanwhile the length of the afterburner and the combustion chamber of the subsonic combustion ramjet is shortened.
An afterburner structure with fuel injection nozzles, which comprises a casing, a central fairing cone located in the casing, a number of airfoil struts connecting the central fairing cone and the inner wall of the casing, the airfoil struts are evenly arranged around the central fairing cone;
Dependencies are inferred from the claim text.