The invention discloses a reciprocating sealing test device of an
aviation hydraulic
actuator and a
verification method, and belongs to the field of
aviation airborne equipment test and
verification. Comprising an end cover, a nut, an outer cylinder, an inner hexagon screw, a
pipe joint, a limiting block, a partition baffle, a
piston rod, a lining and the like, and all the parts are assembled to form the complete component-level sealing test device. Performing sealing element inspection before and after an experiment on the to-be-tested sealing element, and inspecting the quality of the movable surface of the test device; then the sealing element is assembled on a test device, and installation technology adaptability inspection is carried out; the test device is installed on a
test bench, and sealing characteristic tests including a running-in test, a normal-temperature, high-temperature and low-temperature performance test, a low-pressure static test and a high-pressure static test are carried out; performing environment adaptability tests including low-temperature storage, low-temperature work, high-temperature storage, high-temperature work and temperature shock; sealing life durability tests including normal-temperature, high-temperature and low-temperature motion durability tests are completed; and performing
decomposition inspection after the test is finished.