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Affects of Cutting Parameters (Chatter Theory) Dynamics of  High Performance/ High Speed  Machining
SECTION OBJECTIVES ,[object Object],[object Object],[object Object],[object Object],[object Object]
The Cutting Force ,[object Object],[object Object],[object Object],[object Object],[object Object],[object Object]
Mechanical and Thermal Properties of Selected Work piece Materials Column Heads represent the following: UTS, ultimate tensile strength, N/mm 2 (Mpa) K s , specific force, N/mm 2 k, thermal conductivity, N/(sec °C)  =k/(  c), thermal diffusivity, mm 2 /sec T m , melting temperature, °C (  c), specific heat per volume, N/(mm 2   °C) T s , shear plane temperature, °C
Metal Removal Rate MRR = b*a*f f = n*m*c b = axial depth of cut  n = spindle speed a = radial depth of cut  m = number of teeth (width of cut)  c = chip load f = feed or feed rate v =   *d*n v = cutting speed d = cutting diameter 1) From the point of view of cutting speed  v  and chip load  c  the limit is dictated by tool life and breakage and potential increase of MRR depends mainly on improving tool materials. 2) From the point of view of the depth of cut  b  and number of teeth  m  cutting simultaneously the limit is caused by chatter and improvement of MRR is possible by higher dynamic stiffness of the machine tool as formulated by the condition of limit of stability.  This condition is the primary reason for the dimensions and shapes of the machine tool structural components.
Simplified Formulations
Definitions: ,[object Object],[object Object],[object Object],[object Object],[object Object],[object Object]
Stable  Chatter
High-Speed Benefits ,[object Object],[object Object],[object Object]
Basis for Analysis: The Stability Chart Process Damping Region Full Stability Chart
Chatter Mechanism ,[object Object],[object Object],[object Object],[object Object]
Regeneration of Waviness
Cutting Force and Chip Thickness ,[object Object],[object Object],[object Object],[object Object],[object Object]
Derivation of Limit of Stability
  Where k is stiffness,    is damping ratio,       is orientation factor, and K s  is specific force. This is a design criterion. The actual structural systems are more complex,  with several prominent modes.  The criterion is then For a SDOF system:  Limit of Stability Computation “ Oriented” FRF: Limit width of chip:
Limit of Stability Computation (cont.) Where: b lim = limit axial width of cut for no chatter K s = cutting stiffness m = direction orientation factor ->  m =cosb (b=70º, m=0.34) Re[G] = real part of the transfer function. b lim  is smallest (b lim,crit ) when Re[G] is minimum EXAMPLE:  Plunge turning 1035 steel, K s =300,00 lb/in 2 Assume common z=0.04, b=70º and choose a large,  easy to remember  stiffness k=1 Mlb/in. For p times less stiffness b lim,crit =0.8 in/p e.g. if stiffness 10 times less, b lim,crit =0.080 in
Directional Orientation    = cutting force angle f = feed direction F = cutting force n = cutter rotation N = normal of cut u = directional orientation factor X = X-axis Y = Y-axis
Oriented Frequency Response Function (FRF)
Formation of the Stability Lobe Diagram from the Real Part of the FRF Critical limit depth of cut (b cr )
Stability Chart (Lobing Diagram)
Chatter characteristics. ,[object Object],[object Object],[object Object],[object Object],[object Object]
Comparison of stable and unstable cut spectra (frequency content)
Process Damping ,[object Object],[object Object]
General Tendencies ,[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object]

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Chatter Overview

  • 1. Affects of Cutting Parameters (Chatter Theory) Dynamics of High Performance/ High Speed Machining
  • 2.
  • 3.
  • 4. Mechanical and Thermal Properties of Selected Work piece Materials Column Heads represent the following: UTS, ultimate tensile strength, N/mm 2 (Mpa) K s , specific force, N/mm 2 k, thermal conductivity, N/(sec °C)  =k/(  c), thermal diffusivity, mm 2 /sec T m , melting temperature, °C (  c), specific heat per volume, N/(mm 2 °C) T s , shear plane temperature, °C
  • 5. Metal Removal Rate MRR = b*a*f f = n*m*c b = axial depth of cut n = spindle speed a = radial depth of cut m = number of teeth (width of cut) c = chip load f = feed or feed rate v =  *d*n v = cutting speed d = cutting diameter 1) From the point of view of cutting speed v and chip load c the limit is dictated by tool life and breakage and potential increase of MRR depends mainly on improving tool materials. 2) From the point of view of the depth of cut b and number of teeth m cutting simultaneously the limit is caused by chatter and improvement of MRR is possible by higher dynamic stiffness of the machine tool as formulated by the condition of limit of stability. This condition is the primary reason for the dimensions and shapes of the machine tool structural components.
  • 7.
  • 9.
  • 10. Basis for Analysis: The Stability Chart Process Damping Region Full Stability Chart
  • 11.
  • 13.
  • 14. Derivation of Limit of Stability
  • 15. Where k is stiffness,  is damping ratio,  is orientation factor, and K s is specific force. This is a design criterion. The actual structural systems are more complex, with several prominent modes. The criterion is then For a SDOF system: Limit of Stability Computation “ Oriented” FRF: Limit width of chip:
  • 16. Limit of Stability Computation (cont.) Where: b lim = limit axial width of cut for no chatter K s = cutting stiffness m = direction orientation factor -> m =cosb (b=70º, m=0.34) Re[G] = real part of the transfer function. b lim is smallest (b lim,crit ) when Re[G] is minimum EXAMPLE: Plunge turning 1035 steel, K s =300,00 lb/in 2 Assume common z=0.04, b=70º and choose a large, easy to remember stiffness k=1 Mlb/in. For p times less stiffness b lim,crit =0.8 in/p e.g. if stiffness 10 times less, b lim,crit =0.080 in
  • 17. Directional Orientation  = cutting force angle f = feed direction F = cutting force n = cutter rotation N = normal of cut u = directional orientation factor X = X-axis Y = Y-axis
  • 18. Oriented Frequency Response Function (FRF)
  • 19. Formation of the Stability Lobe Diagram from the Real Part of the FRF Critical limit depth of cut (b cr )
  • 21.
  • 22. Comparison of stable and unstable cut spectra (frequency content)
  • 23.
  • 24.