Supersonic combustion engine and method of combustion initiation

Power plants – Reaction motor – Method of operation

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Details

602701, 60204, 602031, F02K 708

Patent

active

052236510

ABSTRACT:
A supersonic combustion air breathing jet engine and method of igniting fuel. The engine has means for providing a spatially controlled combustion distribution of fuel with an ignitor that provides a volumetrically diffuse discharge of energy to initiate a controlled relatively rapid combustion of fuel in a combustion zone such that combustion distribution in relatively high speed gas flows through the combustion zone can be initiated and controlled without dependence upon a flame holder or relatively high local static gas temperature in the combustion zone.

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