The invention belongs to the technical field of aero-engines, and discloses a
turbine casing
impact heat exchange test method and
system, and the method comprises the steps: determining
impact hole parameter research variables, and the structure parameters and number of aperture replacement parts, and adjusting the diameters of
impact holes through the aperture replacement parts; the number and arrangement of the impact holes are adjusted by installing hole
diameter replacement parts and a plurality of plugs on the impact hole plates; the impact target distance is adjusted through different numbers of target distance replacement parts; and performing an impact cooling heat exchange test on each combined
cartridge receiver impact heat exchange test piece to obtain heat exchange coefficients of impact target surfaces of different research variables. The hole
diameter replacement part is arranged to change the hole
diameter and hole arrangement, the target distance replacement part is arranged to change the impact distance, the number of test pieces can be reduced, the
machining cost is reduced, the
machining period is shortened, meanwhile, disassembly and
assembly are easy, disassembly and
assembly time is short, test consistency is guaranteed, effective measurement of the impact heat exchange test temperature is achieved, and therefore the corresponding impact heat
exchange coefficient is obtained.