This invention relates to a high-temperature, high-pressure micro-
combustion device and method for single-particle fuel. The invention comprises a heat-insulating cavity between the
combustion chamber body, the heat-insulating shell, and the heat-insulating top plate, sealed with an
optical glass window on both sides of the
combustion chamber in the middle of the
combustion chamber body. An air inlet and an air outlet for the
combustion chamber are located within the
combustion chamber body. A glass
gasket is nested in the middle of the combustion chamber body, and a micro-combustion plate is placed on the glass
gasket. A ring-shaped cast
copper heating plate surrounds the combustion chamber on the outer side opposite the glass
gasket. A high-speed camera, a high-
magnification objective lens, and a
background light source are located outside the
optical glass window. A
laser emitted from a
laser enters the high-temperature, high-pressure combustion chamber perpendicularly. This invention can more efficiently and easily meet the requirements of high-temperature, high-pressure micro-combustion experiments under a
microscope. It is simple to manufacture, highly stable, heat-insulating, and can flexibly address imaging problems in
microparticle ignition and combustion experiments, effectively conducting interference-free testing of single-particle micro-combustion under high-temperature, high-pressure conditions.