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Turning Dynamics

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Machining Dynamics
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Abstract

Chapter 3 describes regenerative chatter in turning. To predict turning behavior, both analytical and numerical analyses are presented. The analytical, frequency domain stability lobe diagram is derived that describes the limiting stable chip width as a function of spindle speed. A time domain simulation is detailed that determines the dynamic cutting force and tool displacement in turning by numerical integration. The simulation is then used to identify stable and unstable cutting conditions. Finally, the specific application of modulated tool path turning and the effect of process damping on turning stability at low speeds are presented.

Make everything as simple as possible, but not simpler.

—Albert Einstein

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Notes

  1. 1.

    We represent \( \overrightarrow{y}(t) \) and \( \overrightarrow{y}\left(t-\tau \right) \) as vectors because they have both a magnitude and phase relative to the force, Fn. The force and both displacement vectors are displayed in Fig. 3.10.

    Fig. 3.10
    figure 10

    Vector representation of unit normal force and tool deflections (current and previous revolutions) for limit of stability

  2. 2.

    In other words, the ratio of the chatter frequency to forcing frequency cannot be expressed as a ratio of whole numbers.

  3. 3.

    T. Schmitz recognizes the significant contributions of R. Copenhaver and M. Rubeo to the experimental setup.

  4. 4.

    T. Schmitz recognizes the significant contributions of C. Tyler to this section.

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Exercises

Exercises

  1. 1.

    For the turning schematic shown in Fig. 3.69, complete parts (a) through (f). For the single degree of freedom dynamics, the mass is 2 kg, the damping ratio is 0.05, and the stiffness is 2 × 107 N/m. The u direction is oriented at an angle, α, of 35 deg relative to the surface normal, y. The force model parameters are Ks = 1500 N/mm2 and β = 70 deg.

    1. (a)

      Calculate the directional orientation factor. Using this value, compute and plot the real and imaginary parts (in m/N) of the oriented frequency response function versus frequency (in Hz).

    2. (b)

      Determine the minimum value of the real part of the oriented frequency response function and the corresponding chatter frequency. Calculate blim,crit.

    3. (c)

      Determine the spindle speed (in rpm) corresponding to the stability peak defined by the intersection of the N = 0 and N = 1 stability lobes.

    4. (d)

      Find the spindle speed (in rpm) corresponding to the minimum stability limit for the N = 0 lobe.

    5. (e)

      Determine the spindle speed (in rpm) corresponding to the stability peak defined by the intersection of the N = 3 and N = 4 stability lobes.

    6. (f)

      Plot the first four stability lobes (N = 0 to 3) for this system. Use blim units of mm and spindle speed units of rpm.

  2. 2.

    Using the turning schematic shown in Fig. 3.70, complete parts (a) through (d). For the u1 direction, the mass is 10 kg, the damping is 170 N s/m, and the stiffness is 7 × 106 N/m. The u1 direction is oriented at an angle, α1, of 60 deg relative to the surface normal, y. For the u2 direction, the mass is 12 kg, the damping is 1700 N s/m, and the stiffness is 5 × 107 N/m. The u2 direction is oriented at an angle, α2, of 30 deg relative to the y direction. The force model parameters are Ks = 2000 N/mm2 and β = 60 deg.

    1. (a)

      Compute the directional orientation factors, μ1 and μ2. Plot the real and imaginary parts (in m/N) of the oriented frequency response function versus frequency (in Hz).

    2. (b)

      Determine the minimum value of the real part of the oriented frequency response function and the corresponding chatter frequency. Calculate blim,crit.

    3. (c)

      Find the spindle speed (in rpm) corresponding to the minimum stability limit for the N = 2 lobe.

    4. (d)

      Plot the first five stability lobes (N = 0 to 4) for this system. Use blim units of mm and spindle speed units of rpm.

  3. 3.

    Considering the turning model shown in Fig. 3.71, determine the critical stability limit if Ks = 750 N/mm2. For both lumped parameter degrees of freedom, the mass is 1 kg, the stiffness is 7 × 106 N/m, and the damping is 200 N s/m.

  4. 4.

    Complete time domain simulations for the turning model described in Exercise 2. Evaluate the following points for stable or unstable behavior. Use a mean chip thickness (feed per revolution) of 0.15 mm and carry out your simulations for 25 revolutions.

    Ω (rpm)

    b (mm)

    2150

    0.1

    2150

    0.5

    2500

    0.1

    2500

    0.5

    2930

    0.1

    2930

    0.5

    3750

    0.1

    3750

    0.5

    4600

    0.1

    4600

    0.5

    Superimpose your results on the stability lobe diagram from Exercise 2, part (d). Use a circle for stable operating points and an “x” for unstable points.

  5. 5.

    For the facing (turning) operation shown in Fig. 3.72, identify all items on the picture:

    • The direction the spindle rotates

    • The chip width, b

    • The tangential, Ft, and normal, Fn, direction cutting force components that act on the insert/holder

    • The resultant cutting force, F

    • The force angle, β

    • The surface normal direction (for chip thickness variations)

  6. 6.

    For the SDOF turning model shown in Fig. 3.73 with the following parameters, complete parts (a) through (c).

    • k = 2 × 106 N/m

    • m = 2 kg

    • c = 120 N s/m

    • α = 20 deg

    • β = 60 deg

    • Ks = 750 N/mm2 (aluminum alloy)

    • hm = 0.2 mm/rev

    1. (a)

      Compute blim,crit (in mm).

    2. (b)

      Compute the best spindle speed (in rpm) for the N = 3 stability lobe.

    3. (c)

      Compute the approximate chatter frequency (in Hz) at the worst speed for the N = 4 stability lobe.

Fig. 3.69
figure 69

Turning model with flexible tool

Fig. 3.70
figure 70

Turning model with a single degree of freedom in both the u1 and u2 directions

Fig. 3.71
figure 71

Two degree of freedom turning model

Fig. 3.72
figure 72

Facing operation schematic

Fig. 3.73
figure 73

Turning model with a single degree of freedom in the u direction

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Schmitz, T.L., Smith, K.S. (2019). Turning Dynamics. In: Machining Dynamics. Springer, Cham. https://doi.org/10.1007/978-3-319-93707-6_3

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  • DOI: https://doi.org/10.1007/978-3-319-93707-6_3

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