The invention belongs to the field of
ramjet engines, and particularly relates to a
combustion oscillation restraining structure and method and a
ramjet engine, and the
combustion oscillation restraining structure comprises a
combustion oscillation forward sensing
assembly, a pressure
potential energy flow guiding device and a controller; the combustion oscillation forward sensing
assembly comprises two pressure sensors arranged between an inlet of the
combustion chamber and the
injector; the pressure
potential energy flow guide device comprises a flow guide
pipe and a valve arranged in the flow guide
pipe, an inlet of the flow guide
pipe communicates with the inner wall of the
combustion chamber and is located between the two pressure sensors, and an outlet of the flow guide pipe communicates with the spray pipe; the controller is used for controlling the opening and closing or the opening degree of the valve according to the combustion oscillation condition obtained by the combustion oscillation forward sensing
assembly. According to the combustion oscillation suppression structure, combustion oscillation suppression is conducted on the basis of the internal mechanism of combustion oscillation of the
ramjet, the pressure
potential energy flow guiding device fully utilizes the
pressure difference existing in the reaction flow field to adjust the flow field in a self-adaptive mode, and the
thermodynamic cycle efficiency cannot be reduced.