The invention discloses a pulse
detonation combustion chamber outlet
gas pressure pulsation attenuation device. The device comprises an air inlet
pipe, a cylindrical pressure stabilizing cavity, conical flow guide structures, perforated spoilers, a pressure stabilizing cavity extension section and an
exhaust pipe, the air inlet
pipe and the
exhaust pipe are arranged on the two sides of the pressure stabilizing cavity respectively, and the conical flow guide structures are arranged in the pressure stabilizing cavity in a
bilateral symmetry mode; the perforated
spoiler is perpendicular to the conical flow guide structure and extends upwards from the maximum section of the conical flow guide structure until the perforated
spoiler is flush with the inner side wall face of the pressure stabilizing cavity and the inner side wall face of the pressure stabilizing cavity extending section, a plurality of through holes are formed in the perforated
spoiler to form a gas flowing channel, and the perforated spoiler extends outwards to be connected with the pressure stabilizing cavity extending section through a
flange. The advantages of the pressure stabilizing cavity, the flow guide structure and the perforated spoiler are organically fused, the pressure pulsation amplitude of gas at an outlet of the pulse
detonation combustion chamber can be effectively reduced, the stability and uniformity of gas at an inlet of a
turbine are improved, and then the utilization efficiency of the
turbine for unsteady-state energy of the gas is improved.