Determination of regularities of treatment of disks in a fluidized bed of abbrazive

1Kachan, OYa., 1Ulanov, SO
1National University «Zaporizhzhia polytechnic», Zaporizhzhia, Ukraine
Space Sci. & Technol. 2023, 29 ;(6):062-067
https://doi.org/10.15407/knit2023.06.062
Publication Language: Ukrainian
Abstract: 
In this work, the main regularities of processing disks in a fluidized bed of abrasive are established. The research was carried out on the «АПС-600A» installation when processing disks in a fluidized bed of abrasive.
           When processing discs, abrasive grains of groups 24A, 63C, and a mixture of abrasive grains 24A63+24A20 (50 %+50 %) were used. The grain size of the abrasive grains varied in the range № 20 … № 80. The processed disks were made of such alloys as VT3-1, VT-9, EI698-VD, steel 45 HRC 38...45, and aluminum alloy D1T.
            The peripheral speed of the parts is  m/s. The maximum air consumption is 2000 Nm3/h. The pressure of the air that liquefies the abrasive in the air-falling chamber is 5...6 kPa. The disk was immersed in a liquefied layer of abrasive to a depth of (0.2...1.2) Rd of the radius of the disk.
              The regularities of the dependence of the removal of various materials from the machined surface of the disks on the speed of the part, the grain size, and the brand of the abrasive grain have been established.
The dependence of abrasive grain wear on the speed of the part and on its position along the height of the abrasive layer was experimentally established, which allowed for assigning rational modes of processing discs in a fluidized layer of abrasive.
              The main regularities of the processing of disks in a fluidized bed of abrasive have been established, and the influence of the main parameters of the processing process on the productivity and stability of the abrasive grain has been determined.
               The main regularities of the process of processing discs in a fluidized bed of abrasive have been established experimentally, which allows for determining the main parameters, technological conditions, and modes of the finishing operation of parts manufacturing.
Keywords: abrasive grain wear, air, disk, fluidized layer of abrasive, parameters, performance, processing modes, regularity
References: 

1. Agishev B. M. (1977). Application of surface plastic deformation methods to increase the fatigue strength of aircraft GTE compressor disks. Probl. Strength, № 3, 114-119.
https://doi.org/10.1007/BF01532499

2. Gonchar N. V., Yatsenko V. K., Pavlenko D. V. (2004). Endurance of the rim part of compressor disks made of heat-resistant alloy EI698-VD at operating temperatures. Bull. Engine Engineering, № 3, 20-23.

3. Kartashev B. N., Rodichenko A. E. (1976). Vibroprocessing of GTE disks. Aviation industry, № 3, 23-25.
https://doi.org/10.1108/eb041229

4. Kachan A. Ya., Ulanov S. A. (2018). Hardening treatment of rotor parts of the GTE axial compressor. Proc. Dnipro State Technical University (Technical Sciences). Thematic issue: Machines and plastic deformation of metal. Kamianske: DSTU, 307 p.

5. Kachan A. Ya., Ulanov S. A. (2019). Improving the durability of compressor disks made of titanium alloys by processing in a fluidized layer of abrasive. New materials and technologies in metallurgy and machine-building, № 2, 31-37.
https://doi.org/10.15588/1607-6885-2019-2-5

6. Petukhov A. N. (1983). Fatigue resistance of compressor disks. Probl. strength. № 4, 84-87.
https://doi.org/10.1007/BF01522437

7. Sakhno A. G. (1993). Optimization of the regime of ultrasonic hardening of the rim part of the compressor disks. Aviation industry, № 2, 12-13.

8. Yatsenko V. K. (1990). Evaluation of the fatigue strength of the intergroove protrusions of the compressor disks. Aviation industry, № 11, 24-26.

9. Kachan A., Ulanov S., Berezovsky E. (2015). Echnological support of the gas-turbine engine parts bearing capacity by plastic deformation. Metallurgical and Mining Industry, № 11, 183-187.

10. Mattingly J. D., Heiser W. H., Pratt D. T. (2002). Aircraft Engine Design (Second Ed.). Reston, Amer. Inst. Aeronautics and Astronautics, 687 p.
https://doi.org/10.2514/4.861444