The invention discloses a high-pressure spray
optical diagnosis experiment
system using pulse excitation
back pressure oscillation, and belongs to the field of atomization characteristic evaluation of oscillation spray of a liquid
rocket engine. The
system comprises a hyperbaric chamber
system, a pulse excitation system and a test and
optical diagnosis system. The hyperbaric cabin system comprises a cabin body and a
quartz glass observation window. The cabin body is provided with a multi-path gas /
liquid interface, a cable cabin penetrating interface, a
pressure sensor interface and a pulse gun interface. Safety gas is introduced into the high-pressure cabin through the
gas cylinder and the pressure reducing valve, and the specified
back pressure is achieved in the cabin within the pressure bearing range so as to simulate different engine pressure environments. According to the invention, wide-frequency-domain and large-amplitude transient pressure oscillation is excited in a high
back pressure environment, a pressure pulse disturbance scene under
high pressure is simulated, a spraying experiment of an
injector is carried out, and dynamic changes and influence rules of
injection pressure drop, an atomization taper angle, liquid film breakage, a liquid film edge stability state, liquid film suction and separation and the like are analyzed; and
engineering tests and
product optimization of various types of inspirators are facilitated.