The invention discloses a rotary
detonation combustion chamber which comprises a gas and
oil supply assembly, an injection
assembly and a
combustion chamber body. Wherein an annular channel is formed in the
combustion chamber body, and the
gas supply and
oil supply assembly communicates with the
gas supply system, can form high-speed
airflow to enter the annular channel and communicates with the
energy supply system and the injection assembly through the
gas supply and
oil supply system, so that fuel can enter the injection assembly through the gas supply and oil supply assembly; the high-speed
airflow and the fuel
jet flow can collide in the annular channel to be subjected to secondary atomization to form a combustible mixture, the
combustion chamber body is provided with an igniter used for detonating the combustible mixture so as to form rotating
detonation waves, and through the combustion mode of rotating
detonation, the combustion efficiency is improved. By means of the self-pressurization structure,
airflow expands and accelerates at the downstream of detonation
waves and is exhausted from the
tail of the
combustion chamber in a high-temperature
fuel gas mode, the heat efficiency of combustion can be improved through the self-pressurization characteristic of the self-pressurization structure, emission of pollutants such as
NOx is reduced, and the self-pressurization structure is more compact.