The invention relates to the technical field of
scramjet engines, solves the technical problems that a
scramjet engine wide-area structure is high in
combustion difficulty and
flame stabilization difficulty, and particularly relates to a
hydrogen peroxide catalytic decomposition gas atomization injection concave cavity integration module and an injection
flame stabilization enhancement method.
Liquid hydrogen peroxide is decomposed into high-temperature
oxygen and
water vapor by adopting a
catalytic decomposition module, then the high-temperature
oxygen and the
water vapor are mixed with
kerosene in a
decomposition gas pipeline to form
kerosene which is aerated and atomized by the high-temperature
oxygen and the
water vapor, the
kerosene is transversely sprayed at the upstream of a concave cavity through a gas atomization kerosene spraying hole, and gas atomization kerosene transverse
jet flow is formed in a supersonic
combustion chamber; therefore, the
combustion efficiency is improved. The oxygen-enriched
jet flow for enhancing the combustion performance is formed in the supersonic
combustion chamber, the ignition performance of liquid kerosene can be improved, meanwhile, the atomization particle size can be reduced, the
jet flow penetration depth can be increased, the
fuel gas mixing efficiency can be improved, and the supersonic combustion
flame stabilizing range of the liquid kerosene can be widened.