The invention discloses a dismounting device for double shaft sleeves of a civil aircraft oil
combustion part. The dismounting device comprises a fixing support, a jacking device and two sets of pullers; the fixing support is provided with a top plate and a bottom plate, and the top plate is provided with a lifting mechanism; the jacking device comprises a panel, the middle of the panel is provided with a
threaded rod through hole matched with the lower end of a
threaded rod, through holes symmetrically formed in the two sides of the
threaded rod through hole, and two lifting bolts are assembled in the through holes, wherein the
diameter of the bolt heads of the lifting bolts is larger than that of the through holes for the lifting bolts; each puller comprises a circular
pipe and a jacking rod, wherein a threaded hole serves as an inner hole formed in the upper end of the circular
pipe, the
pipe wall of the lower end of the circular pipe is evenly provided with a plurality of axial long gaps, a tapered opening serves as a hole opening of an inner hole formed in the lower end of the circular pipe, a rolling ball of which the
diameter is larger than that of the small end of the tapered opening is assembled in the tapered opening, the lower end of the jacking rod penetrates into the inner hole of the circular pipe to abut against the rolling ball, the upper end of the jacking rod is provided with an outer threaded in a lathing mode, the outer thread is matched with the threaded hole formed in the upper end of the circular pipe, the topmost end of the jacking rod is provided with an axial threaded hole which is in thread fit with the corresponding lifting bolt, and the outer surface of the jacking rod is provided with knurls convenient for hand screwing. According to the dismounting device, the double shaft sleeves of the civil aircraft oil
combustion part can be dismounted on the condition that a shell is not collided and scraped and shell and shaft sleeve damage is not caused.