Thermodynamic Analysis of a Mechatronic                               Pneumatically-Driven Spherical Joint

                                        Henry M. Paynter & Joseph M. Juarez

 

Abstract—Jointed-member robotic devices (Arthrobots) can benefit from pneumatic Tug-&-Twist technology. In particular, two crossed Twistor-Pairs provide a flexural spherical joint in the form of a Twistor-gimbal-drive. Previous papers have shown that the performance characteristics of both Tuggers and Twistors may be derived from a unique appropriate enthalpy function. This paper develops the Twistor enthalpy, H(P,a ), based upon independent volume and torque measurements, which fully accounts for pressure-dependent Twistor stretch and Coulomb torque. This function then provides a model for computer-control of the final spherical joint.

Index Terms—pneumatics, Arthrobots, Twistor, powered spherical joint 

 

  1. Introduction
  2. Configurations of robots wherein all degrees-of-freedom are joint rotations has meant that torque motors could be used at each and every axis [4]; such devices have been designated Arthrobots [1], [2], [5], and [6]. A Twistor is a Pneumo-elastic device that is an inflatable actuator having an axially elongated, flexible, hollow, thin-walled elastic cylindrical shell defining a fluid chamber, Figure 1, [2], [3], [5], [6], [7], and [16].


    Two Twistor actuators can be pre-twisted to form the jointed device shown in Figure 2, where the Twistor-pair forms the flextural joint and the bi-directional pneumatic actuator. Controllably varying the fluid pressure of each Twistor rotates the member as indicated in Figure 2.

    Two such crossed Twistor-pairs can then provide a fully-active flexural spherical joint, with open-loop proportional control. Such a gimbal-drive is shown in Figure 3.

    This paper derives the characteristics of a Twistor-pair by first measuring both volumes and torques under isobaric conditions at various angles and then obtaining the consistent enthalpy function by integration of the data.
     
     

  3. THERMODYNAMIC PERFORMANCE CHARACTERISTICS


    An approach based directly upon the First Law of Thermodynamics recognizes the near-reversible conversion of fluid available energy into mechanical energy. Such methods have proved useful for Tugger and Twistor design [1] and [16] but, can also provide rational characteristics for computer-control.

    This approach begins with the First Law statement:

    dE = P× dV – T× da (1)

    where Energy E = E (V,a)

    This represents a constraint between Pressure, P; Volume, V; Torque, T; and Twist Angle, a. However, here we are interested in the situation where P and a are proper Input variables with V and T being the corresponding Output variables [6], [8], [9], [10], [11], and [12]. To create these conditions, we must perform a Legendre transformation upon Energy to form a complementary energy or generalized Enthalpy, H [13], [14], and [15].

    The requisite Legendre transformation may be performed as follows.

    Given E(V,a), the function H(P,a) is found directly from the thermodynamic relation:

    H(P,a) = E – P× V

    Differentiation yields, dH = -V× dP – T× da


      From this last relation we then obtain the two Outputs:

    Volume, V(P,a) = -H(P,a) / P

    Torque, T(P,a) = -H(P,a) / a

    These results suggest that the active transduction torque may be estimated by direct integration of the volume changes with pressure.
     
     

  4. EXPERIMENTAL VOLUMETRIC RESULTS


    Volume data was collected on a single Twistor actuator. A Twistor in the untwisted position is said to be at zero degrees. The data collected resulted in volumetric measurements taken at 50, 60, 70, and 80 degrees of Twist Angle; and at varied pressures of 35, 50, 60, and 70 psi. Measurements were also made at 80 psi but, at this point the actuator began to balloon excessively. This was anticipated in the design, where increasing the shell wall thickness would support additional pressure but would detract from low-pressure response. Table 1. shows the measured volumes.
    P / a 50 60 70 80
    35 .0458 .0409 .0323 .0256
    50 .0622 .0561 .0464 .0354
    60 .072 .0629 .0519 .0452
    70 .0805 .0720 .0622 .0543
    80 .1239 .1086 .0867 .0763

    Table 1. Column 1 represents Pressure settings in pounds per square inch, Row 1 represents Twist Angle settings in degrees, and the interior points represent the measured Volumes in cubic inches.

    This volume data was then fit to an equation that maintains the Maxwell Relations and the differential form of the First Law equation 1, [17], and [18].

    This fitting process for volume employed Microsoft Excel. The resulting linear regression in English units is:

    V(P,a) = 0.041093 + 0.001244× P – 0.031424× a - 0.000319× P

    where Volume, V, is in Cubic-Inches, Pressure, P, is in Pounds per Square Inch, and Twist Angle, a, is in Radians.

    Figure 4. shows the regression fit of the volume data as a function of Twist Angle at the four experimental pressures. V(P,a) is within one standard deviation from the experimental data results in Table 1.

  5. THE PARTIAL ENTHALPY, Hv(P, a).


    From the volume data, V(P,a), alone, it is only possible to obtain a partial enthalpy function through integration in the form

    Hv(P, a) = ò V(P,a)× dP.

     Using the above fit to V(P,a), the integration yields:HV(P,a) = 0.041093× P + 0.001244× P2/2 – 0.031424× P - 0.000319× P2/2,

    so now by differentiation with respect to a there results the active ( or transduced) torque:

    TV(P,a) = - HV / a = 0.031424× P + 0.000319× P2/2.

    However, this volumetric partial enthalpy is unable to provide the pressure-dependent Coulomb torque component, which can be determined from experimental measurements, as described in the next section.
     
     

  6. EXPERIMENTAL TORQUE MEASUREMENTS


    The previous results for the active torque, TV, indicate that a single Twistor behaves like a vane-motor whose cross-section is sensibly pressure dependent. However, if this resultant characteristic is to be applied to the case of the Twistor-pair of Figure 2 or to the Spherical-Joint of Figure 3, one must also take into account the net Coulombian flexural torque variation of both opposed Twistors. Generally this passive elastic torque will also be found to be pressure dependent.

    In principle, if both Volume, V, and Torque, T, were independently varied and measured, they could be considered as Inputs, with Pressure, P, and Twist Angle, a, as respective Outputs. The corresponding potential would then be a generalized Free Energy, F(V, T). In the same way, if P and T were taken as Inputs and V and a as Outputs the appropriate potential is the Free Enthalpy, G(P, T).

    However, upon pressurizing one actuator of a Twistor-pair, the torque was in fact directly measured by a torque-wrench for the very same pressures and angles used for the above volume data. In consequence, one may consider the Measured Torque, T, to be composed of two separate components: the Active Torque, TV, and a pressure-dependent Coulomb Torque, TC, in the fashion:

    T(P, a) = TV(P, a) + TC(P, a).

    Table 2 lists the measured data for T(P, a) while Table 3 lists the results for TC if TV is taken as that determined above from the volume measurements.
    P/a
    50
    60
    70
    80
    70
    8.5
    20
    42.6
    52
    60
    -21
    -8
    7
    22
    50
    -31.4
    -18.6
    -5.4
    9.4
    35
    -48
    -36
    -20.6
    -4.6
    0
    -63.2
    -50
    -33.4
    -19

    Table 2. Column 1 represents Pressure settings in pounds per square inch, Row 1 represents Twist Angle settings in degrees, and the interior points represent the measured Torques in Inch-Ounces.
     
     
     
     
     
     
    P/a
    50
    60
    70
    80
    70
    -39.2
    -27.7
    -5.1
    4.3
    60
    -60.35
    -47.35
    -32.35
    -17.35
    50
    -62.92
    -50.12
    -36.92
    -22.12
    35
    -68.72
    -56.72
    -41.32
    -25.32
    0
    -63.2
    -50
    -33.4
    -19

    Table 3. Column 1 represents Pressure settings in pounds per square inch, Row 1 represents Twist Angle settings in degrees, and the interior points represent the Coulomb Torque in Inch-Ounces.

    Inspection of Table 3 suggests the following model equation for TC(P, a):

    TC(P, a) = a + b× P + c× P3 + d× a

     As before, the regression parameters a, b, c, d, and e were determined using Microsoft Excel. The resulting model equation for T(P, a) then becomes:

    T(P, a) = -135.385 + 0.050784× P + 0.005104× P2/2 + 0.000155× P3 + 83.36536× a.

    Where Torque, T, is in Inch-Ounces, Pressure, P, is in Pounds per Square Inch, and Twist Angle, a, is in Radians.

    Figure 5., shows the regression fit for the Torque as a function of Twist Angle at the five experimental pressures.

     

  7. APPLICATION of the RESULTING MODEL EQUATIONS to OPEN-LOOP COMPUTER CONTROL of the SPHERICAL DRIVE


    Of course, 4 pneumatic pressure regulators can directly manipulate the Twistor-Gimbal Drive of Figure 3. However, sophisticated open-loop control of both axes results upon supplying the 4 pressures from 4 electro-pneumatic valves driven from either a solid-state PLC unit or through an interface from a notebook computer. Figure 6., indicates such an arrangement where the PLC on the left is moving the "eyeball" on the right through a simple tracking task. The logic schedule makes use of the model equation above for torque as a function of pressure and angle.

     

  8. CONCLUSION


    This analytical approach is very effective for estimating active torque when only volume data is available for Twistors. It has been shown that the volume equation in the form above satisfies the Maxwell relations and that the intermediate evaluation of the (partial) Enthalpy serves as the means toward calculating active Torque.

    Although it is clear from the above test results that this particular Twistor has only a limited torque capability, nevertheless, simple scaling laws extrapolate volumes and active torques both to larger and smaller sizes. However, particularly for smaller-size Twistors, the Coulomb torques are very design dependent so that accurate total torque characteristics require prototype calibration. However, present experience with several sizes and designs indicates that the form of the model for T(P, a) remains nearly invariant, with only the parameters changing with design and size. For this reason the architecture of control programs for Twistor-pairs and Gimbal-drives can be held fixed.

     

  9. ACKNOWLEDGEMENTS


    A special thanks goes to Mario DiMarco of DM3 Electric Car Racing for use of his experimental facility and for suggesting that we use air over water to facilitate measuring the actuator chamber volumes and to Professor Rudy Wojtecki of Kent State University, Trumbull Campus for his assistance in the pneumatic computer contol of the Gimbal-drive.
     
     

  10. REFERENCES
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  12. Paynter, H. M.,"Low-Cost Pneumatic Arthrobots Powered by TUG-&-TWIST Polymer Actuators," In: Stelson, K. and Oba, F. (eds): Proceedings, Japan-USA Symposium on Flexible Automation, Boston, MA, pp. 107-110.
  13. Paynter, H. M.: All-Elastomer Fluid-Pressure-Actuatable Twistors and Twistor Drive Assemblies, United States Patent 5,090,297, Frbruary 25, 1992.
  14. Asada, H. and Youcef-Toumi, K., Direct-Drive Robots: Theory and Practice, The M.I.T. Press, Cambridge, MA, 1987.
  15. Paynter, H. M. : Method and System employing Double-Acting, Fluid-Driven Twistor-Pairs as Combined Joints and Motors in Arthrobots, United States Patent 4,751,868, June 21, 1988.
  16. Paynter, H. M. : Walking Robots having Double Acting Fluid Driven Twistor Pairs as Combined Joints and Motors and Method of Locomotion, United States Patent 5,040,626, August 20, 1991.
  17. Paynter, H. M. : Fluid-Driven Torsional Operators for Turning Rotary Valves and the Like, United States Patent 4,108,050, August 22, 1978.
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  26. Paynter, H. M., and Juarez, J. M., "Thermodynamic Treatment of Tug-&-Twist Technology Part 2: Thermodynamic Twistor Design," In: Lee K-M. (ed.), 1999 IEEE/ASME International Conference on Advanced Intelligent Mechatronics Proceedings[AIM ’99], September 19-23, 1999, Atlanta, GA, pp. 826-829.
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Figure 3- Twistor Gimbal-Drive with Laser mounted         

Figure 6. Mechatronic "eyeball" manipulated by a Twistor-Gimbal Drive.