Purpose. Increasing fatigue life of GTE compressor disks made of titanium alloys by discs treatment in the fluidized abrasive bed.Investigation methods and equipment. The investigations were carried out using LPC stage I discs of ВТ3-1 alloy and HPC stages IV and V discs made of ВТ-9 titanium alloy of Д-36 aircraft engine.In the process of discs manufacture the following manufacturing methods were used: ultrasonic hardening and treatment in the fluidized abrasive bed.The ultrasonic hardening was carried out using Motor Sich serial installation and the fluidized abrasive bed treatment – using the АПС-600А installation.The discs were tested before and after the treatment on a special electrohydraulic test bench with a multi-axis loading system using a fixture reproducing radial and circumferential stresses at the base of an inter-slot projection.The testing was carried out at specimens temperature of 390 °С and 430 °С.For measuring the length of cracks and the time of their occurrence in the slots, the discs were inspected by ЛЮМ-1-ОВ method ant using the МПБ-2 microscope and КМ-8 cathetometer.Obtained results. It has been established that for LPC stage I discs made of ВТ3-1 alloy the increased fillet radius combined with subsequent treatment in the fluidized abrasive bed increases fatigue life of the discs by 6 times before crack occurrence, and increases durability of the disc with a crack by 5.5 times.Durability of a disc is within 41 % to 77.8 % of their total fatigue life .Treatment of the compressor dics made of ВТ-9 titanium alloy in the fluidized abrasive bed creates residual compression strain up to 300 MPa in the surface layer.Testing of the LPC stage 1 discs showed that frequency and shape of the discs effect both fatigue life prior to a crack occurrence and durability prior to discs destruction within the entire investigated loading frequency range of 0.01 Hz to 1.0 Hz.Testing of HPC stages IV and V discs of ВТ-9 titanium alloy showed that temperature variation within 390 °С to 430 °С did not contribute significantly to the fatigue life change. Introduction of endurance into the loading cycle has a considerable effect on the low-endurance fatigue of the compressor discs.Increase of the soak time up to 60 seconds under the same loading conditions decreased fatigue life of the full-scale specimens by 10 times.Scientific novelty. It was demonstrated that treatment of the compressor disks made of titanium alloys in the fluidized abrasive bed increases their cyclic life by 5 to 6 times in comparison with their treatment in accordance with serial technology.Practical effect. A process sheet was proposed and the modes of compressor discs treatment in the fluidized abrasive layer were developed that provide increase of the fatigue life by 5 to 6 times as compared with a serial technology.