The application relates to a double-channel rotating
detonation combustion chamber structure with an inlet total pressure adjusting function, which comprises a Tesla valve arranged at the inlet of the rotating
detonation combustion chamber, the Tesla valve comprises a shell and a flow channel, the inlet end and the outlet end of the flow channel are respectively provided with pressure adjusting structures, the radial outer side of the flow channel is provided with an injection channel, the injection channel comprises an air outlet channel and a pressurizing channel communicated with the air outlet channel, and the side, away from the pressurizing channel, of the air outlet channel is provided with an opening and closing
assembly for opening or closing the air outlet channel, the opening and closing
assembly comprises a supporting plate, a plurality of opening and closing
doors and a self-locking driving part, and the self-locking driving part is used for synchronously driving the plurality of opening and closing
doors to be close to or away from the outlet side of the air outlet channel. The application has the effects that when the rotating
detonation combustion chamber is in an air thin belt, the air intake of the air
inlet channel is automatically enhanced, the rotating detonation
combustion chamber preferentially intakes the air in the air
inlet channel, the air supply of the
combustion chamber is ensured, and the adaptability and stability of the
combustion chamber in different environments are improved.