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The vibration behavior of impeller blades in the five-axis CNC flank milling process

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Abstract

Today, in most cases, impellers of centrifugal compressors are produced by flank milling on five-axis CNC milling machines. The complex three-dimensional geometry of the very thin blades consists of ruled surfaces. The flank milling process allows a fast production of the impellers and the surface of the blades is of high quality. The limited strength of the very thin blades and also the thin outer radial part of the disk lead to a high sensitivity to static and especially dynamic forces that are caused by the instationary flow in the impeller. The dynamic forces of rotating stall and surge are the most dangerous excitations of the bladed disk. Coupled vibrations may occur and damage the impeller. The highest static load is caused by the centrifugal forces. Therefore, most of the high-loaded impellers are manufactured from aluminum alloy or titanium because of the low density of this light metals and the relatively high strength. Most of the interests and the investigations in the last years are paid to the vibration behavior and the dynamic loads of the impeller during operation. But sometimes, the highest stress may occur during the production process and damage the impeller or weaken the strength and so cause later problems. Especially, excitations from the dynamic forces during the flank milling process have to be taken under consideration. The vibration behavior of the impeller is very complex and is affected by the vibration behavior of the cutter and the milling machine. In this paper, the change of the vibration behavior of centrifugal compressor impeller blades during the manufacturing process is investigated. During the finishing of the thin blades, the blade thickness is continuously changing and also the strength and the corresponding eigenfrequencies of the blade. The dynamic forces acting on the blades are caused by the cutter, the milling machine, and the cutting process. The quantity of the forces and the frequency of the excitation are determined by the rotational speed of the cutter, the feed, the number of edges, and the chip thickness. The results described in this paper give useful information about the change of the vibration behavior of the centrifugal impeller blades during the flank milling process and possible interaction with the cutter and the machine.

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References

  1. Hasemann H, Weser G, Hagelstein D, Rautenberg M (1997) Investigation of the solidity and the blade vibration behaviour of unshrouded centrifugal compressor impellers with different aerodynamic design. ASME-Paper 97-GT 233, 42nd International Gas Turbine and Aeroengine Congress and Exhibition of the ASME, Orlando, FL, USA, 2–5 June

  2. Change T, Wysk RA, Wang H (1998) Computer-aided manufacturing, 2nd edn. Prentice Hall, Upper Saddle River

    Google Scholar 

  3. Hasemann H, Hagelstein D, Rautenberg M (1998) Coupled vibration of unshrouded centrifugal compressor impellers, part 1: experimental investigation. ISROMAC-7, 7th International Symposium on Transport Phenomena and Dynamics of Rotating Machinery, Honolulu, Hawaii, USA, 22–26 February, volume C, pp 1295–1305

  4. Hagelstein D, Hasemann H, Rautenberg M (1998) Coupled vibration of unshrouded centrifugal compressor impellers, part 2: computation of vibration behavior. ISROMAC-7, 7th International Symposium on Transport Phenomena and Dynamics of Rotating Machinery, Honolulu, Hawaii, USA, 22–26 February, volume C, pp 1306–1317

  5. Hasemann H, Oberröhrmann A, Hagelstein D, Rautenberg M (1995) Investigation of the solidity and the blade vibration behaviour of radial compressor impellers due to a significant reduction of the hyperbolic undercut in the flankmilling process. Yokohama International Gas Turbine Congress, Yokohama, Japan, 22–27 October

  6. Rautenberg M, Engeda A, Wittekindt W (1989) Mathematical formulation of blade surfaces in turbomachinery. Part I: theoretical surface formulations. ASME-Paper No. 89-GT-160, 34th ASME International Gas Turbine and Aeroengine Congress and Exposition, Toronto, Ontario, Canada, 4–8 June

  7. Rautenberg M, Engeda A, Wittekindt W (1989) Mathematical formulation of blade surfaces in turbomachinery. Part II: practical examples of determined surfaces. ASME-Paper No. 89-GT-161, 34th ASME International Gas Turbine and Aeroengine Congress and Exposition, Toronto, Ontario, Canada, 4–8 June

  8. Budak E (2000) Improving productivity and part quality in milling of titanium based impellers by chatter suppression and force control. CIRP Ann 49(1):31–35

    Article  Google Scholar 

  9. Larue A, Altintas Y (2005) Simulation of flank milling processes. Int J Mach Tools Manuf 45(2005):549–559

    Article  Google Scholar 

  10. Peigne G, Paris H, Brissaud D, Gouskov A (2004) Impact of the cutting dynamics of small radial immersion milling operations on machined surface roughness. Int J Mach Tools Manuf 44(2004):1133–1142

    Article  Google Scholar 

  11. Ramamurit V, Subramani DA, Sridhara K (1995) Free vibration analysis of a turbocharger centrifugal compressor impeller. Mech Mach Theory 30(1995):619–628

    Article  Google Scholar 

  12. Al-Zubaidy SN (1995) A proposed design package for centrifugal impellers. Comput Struct 55(1995):347–356

    Article  Google Scholar 

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Correspondence to Kawin Sonthipermpoon.

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Sonthipermpoon, K., Bohez, E., Hasemann, H. et al. The vibration behavior of impeller blades in the five-axis CNC flank milling process. Int J Adv Manuf Technol 46, 1171–1177 (2010). https://doi.org/10.1007/s00170-009-2182-9

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  • DOI: https://doi.org/10.1007/s00170-009-2182-9

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