This invention relates to the field of
testing equipment technology and provides an airtightness testing device, including an airtightness
detector, an air intake
assembly, and an elastic sealing plug. The air intake
assembly includes a hollow air intake
pipe and a support base. One end of the air intake
pipe is fixedly connected to the support base, and the other end is provided with an
external interface for connecting an external airtightness
detector. The support base has a through-hole for connecting the air intake
pipe and a cavity. The sealing plug includes an arcuate portion adapted to a narrow
throat, a first limiting portion, and a second limiting portion. The sealing plug has a through-hole for the air intake pipe to pass through. The through-hole is located on the inner wall of the first limiting portion, which is recessed inward to form an
abutment groove for restricting the movement of the support base. In this invention, the airtightness testing device has a simple structure, is quick to install and disassemble, ensures the reliability of liquid-fueled
rocket engine quality, effectively improves the efficiency of liquid-fueled
rocket assembly and testing, and shortens the preparation time before
rocket launch.