The invention discloses an axisymmetric adjustable spray
pipe of a rotary
detonation combined engine adapting to spiral
shock wave incoming flow, and relates to the field of combined power engines. The jet
pipe is composed of fins, a jet
pipe shell, an electric push rod, balls, a
graphite ring, a jet pipe outer cover, a jet pipe inner cylinder, a jet pipe inner cone and the like, an adjustable outer
culvert flow channel is formed between the jet pipe outer cover and the jet pipe inner cylinder, and an outer
culvert throat channel is formed in the position, with the minimum axial section area, of the flow channel; an inner
culvert flow channel is formed between the spray pipe inner cylinder and the spray pipe inner cone; and the area of the
throat of the outer culvert is adjusted through the push-pull action of the electric push rod. Under the working mode of the
turbine, air flow is sprayed out through the inner culvert flow channel; and in the
stamping mode, air flow is sprayed out through the outer culvert flow channel. In the
stamping mode, the area of the
throat of the outer culvert is flexibly changed through adjustment of the electric push rod, and the requirements for environment pressure and engine performance at different altitudes are met. The flow matching capacity and expansion pressure ratio adaptability of the engine are improved, and the performance of the rotating and knocking combined engine in the
stamping mode is improved.