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Flexible Joints - Test Bench

Table of Contents


This report is also available as a pdf.


In this document, we present a test-bench that has been developed in order to measure the bending stiffness of flexible joints.

It is structured as follow:

1 Flexible Joints

The flexible joints that are going to be measured in this document have been design to be used with a Nano-Hexapod (Figure 1).

nano_hexapod.png

Figure 1: CAD view of the Nano-Hexapod containing the flexible joints

Ideally, these flexible joints would behave as perfect ball joints, that is to say:

  • no bending and torsional stiffnesses
  • infinite shear and axial stiffnesses
  • un-limited bending and torsional stroke
  • no friction, no backlash

The real characteristics of the flexible joints will influence the dynamics of the Nano-Hexapod. Using a multi-body dynamical model of the nano-hexapod, the specifications in term of stiffness and stroke of the flexible joints have been determined and summarized in Table 1.

Table 1: Specifications for the flexible joints and estimated characteristics from the Finite Element Model
  Specification FEM
Axial Stiffness > 100 [N/um] 94
Shear Stiffness > 1 [N/um] 13
Bending Stiffness < 100 [Nm/rad] 5
Torsion Stiffness < 500 [Nm/rad] 260
Bending Stroke > 1 [mrad] 24.5
Torsion Stroke > 5 [urad]  

Then, the classical geometry of a flexible ball joint shown in Figure 2 has been optimized in order to meet the requirements. This has been done using a Finite Element Software and the obtained joint’s characteristics are summarized in Table 1.

flexible_joint_fem_geometry.png

Figure 2: Flexible part of the Joint used for FEM - CAD view

The obtained geometry are defined in the drawings of the flexible joints. The material is a special kind of stainless steel called “F16PH”.

The flexible joints can be seen on Figure 3.

IMG_20210302_173619.jpg

Figure 3: 15 of the 16 flexible joints

2 Dimensional Measurements

2.1 Measurement Bench

The axis corresponding to the flexible joints are defined in Figure 4.

flexible_joint_axis.png

Figure 4: Define axis for the flexible joints

The dimensions of the flexible part in the Y-Z plane will contribute to the X-bending stiffness. Similarly, the dimensions of the flexible part in the X-Z plane will contribute to the Y-bending stiffness.

The setup to measure the dimension of the “Y” flexible beam is shown in Figure 5.

flexible_joint_y_flex_meas_setup.png

Figure 5: Setup to measure the dimension of the flexible beam corresponding to the X-bending stiffness

What we typically observe is shown in Figure 6. It is then possible to estimate to dimension of the flexible beam with an accuracy of \(\approx 5\,\mu m\),

soft_measure_flex_size.jpg

Figure 6: Image used to measure the flexible joint’s dimensions

2.2 Measurement Results

The expected flexible beam thickness is \(250\,\mu m\). However, it is more important that the thickness of all beams are close to each other.

The dimension of the beams are been measured at each end to be able to estimate the mean of the beam thickness.

All the measured dimensions are summarized in Table 2.

Table 2: Measured Dimensions of the flexible beams in \(\mu m\)
  X1 X2 X3 X4
1 223 226 224 214
2 229 231 237 224
3 234 230 239 231
4 233 227 229 232
5 225 212 228 228
6 220 221 224 220
7 206 207 228 226
8 230 224 224 223
9 223 231 228 233
10 228 230 235 231
11 197 207 211 204
12 227 226 225 226
13 215 228 231 220
14 216 224 224 221
15 209 214 220 221
16 213 210 230 229

An histogram of these measured dimensions is shown in Figure 7.

beam_dim_histogram.png

Figure 7: Histogram for the (16x2) measured beams’ thickness

3 Measurement Test Bench - Bending Stiffness

The most important characteristic of the flexible joint that we want to measure is its bending stiffness \(k_{R_x} \approx k_{R_y}\).

To do so, we have to apply a torque \(T_x\) on the flexible joint and measure its angular deflection \(\theta_x\). The stiffness is then

\begin{equation} k_{R_x} = \frac{T_x}{\theta_x} \end{equation}

As it is quite difficult to apply a pure torque, a force will be applied instead. The application point of the force should far enough from the flexible part such that the obtained bending is much larger than the displacement in shear.

The working principle of the bench is schematically shown in Figure 8. One part of the flexible joint is fixed. On the mobile part, a force \(F_x\) is applied which is equivalent to a torque applied on the flexible joint center. The induced rotation is measured with a displacement sensor \(d_x\).

test_bench_principle.png

Figure 8: Test Bench - working principle

This test-bench will be used to have a first approximation of the bending stiffnesss and stroke of the flexible joints. Another test-bench, better engineered will be used to measure the flexible joint’s characteristics with better accuracy.

3.1 Flexible joint Geometry

The flexible joint used for the Nano-Hexapod is shown in Figure 9. Its bending stiffness is foreseen to be \(k_{R_y}\approx 5\,\frac{Nm}{rad}\) and its stroke \(\theta_{y,\text{max}}\approx 25\,mrad\).

flexible_joint_geometry.png

Figure 9: Geometry of the flexible joint

The height between the flexible point (center of the joint) and the point where external forces are applied is \(h = 20\,mm\).

Let’s define the parameters on Matlab.

kRx = 5; % Bending Stiffness [Nm/rad]
Rxmax = 25e-3; % Bending Stroke [rad]
h = 20e-3; % Height [m]

3.2 Required external applied force

The bending \(\theta_y\) of the flexible joint due to the force \(F_x\) is:

\begin{equation} \theta_y = \frac{M_y}{k_{R_y}} = \frac{F_x h}{k_{R_y}} \end{equation}

Therefore, the applied force to test the full range of the flexible joint is:

\begin{equation} F_{x,\text{max}} = \frac{k_{R_y} \theta_{y,\text{max}}}{h} \end{equation}
Fxmax = kRx*Rxmax/h; % Force to induce maximum stroke [N]

And we obtain:

\begin{equation} F_{x,max} = 6.2\, [N] \end{equation}

The measurement range of the force sensor should then be higher than \(6.2\,N\).

3.3 Required actuator stroke and sensors range

The flexible joint is designed to allow a bending motion of \(\pm 25\,mrad\). The corresponding stroke at the location of the force sensor is: \[ d_{x,\text{max}} = h \tan(R_{x,\text{max}}) \]

dxmax = h*tan(Rxmax);
\begin{equation} d_{max} = 0.5\, [mm] \end{equation}

In order to test the full range of the flexible joint, the stroke of the translation stage used to move the force sensor should be higher than \(0.5\,mm\). Similarly, the measurement range of the displacement sensor should also be higher than \(0.5\,mm\).

3.4 Test Bench

A CAD view of the measurement bench is shown in Figure 10.

Here are the different elements used in this bench:

Both the measured force and displacement are acquired at the same time using a Speedgoat machine.

test_bench_flex_overview.png

Figure 10: Schematic of the test bench to measure the bending stiffness of the flexible joints

A side view of the bench with the important quantities are shown in Figure 11.

test_bench_flex_side.png

Figure 11: Schematic of the test bench to measure the bending stiffness of the flexible joints

4 Error budget

Many things can impact the accuracy of the measured bending stiffness such as:

  • Errors in the force and displacement measurement
  • Shear effects
  • Deflection of the Force sensor
  • Errors in the geometry of the bench

In this section, we wish to estimate the attainable accuracy with the current bench, and identified the limiting factors.

4.1 Finite Element Model

From the Finite Element Model, the stiffness and stroke of the flexible joint have been computed and summarized in Tables 3 and 4.

Table 3: Axial/Shear characteristics
  Stiffness [N/um] Max Force [N] Stroke [um]
Axial 94 469 5
Shear 13 242 19
Table 4: Bending/Torsion characteristics
  Stiffness [Nm/rad] Max Torque [Nmm] Stroke [mrad]
Bending 5 118 24
Torsional 260 1508 6

4.2 Setup

The setup is schematically represented in Figure 12.

The force is applied on top of the flexible joint with a distance \(h\) with the joint’s center. The displacement of the flexible joint is also measured at the same height.

The height between the joint’s center and the force application point is:

h = 25e-3; % Height [m]

test_bench_flex_side.png

Figure 12: Schematic of the test bench to measure the bending stiffness of the flexible joints

4.3 Effect of Bending

The torque applied is:

\begin{equation} M_y = F_x \cdot h \end{equation}

The flexible joint is experiencing a rotation \(\theta_y\) due to the torque \(M_y\):

\begin{equation} \theta_y = \frac{M_y}{k_{R_y}} = \frac{F_x \cdot h}{k_{R_y}} \end{equation}

This rotation is then measured by the displacement sensor. The measured displacement is:

\begin{equation} D_b = h \tan(\theta_y) = h \tan\left( \frac{F_x \cdot h}{k_{R_y}} \right) \label{eq:bending_stiffness_formula} \end{equation}

4.4 Computation of the bending stiffness

From equation \eqref{eq:bending_stiffness_formula}, we can compute the bending stiffness:

\begin{equation} k_{R_y} = \frac{F_x \cdot h}{\tan^{-1}\left( \frac{D_b}{h} \right)} \end{equation}

For small displacement, we have

\begin{equation} \boxed{k_{R_y} \approx h^2 \frac{F_x}{d_x}} \end{equation}

And therefore, to precisely measure \(k_{R_y}\), we need to:

  • precisely measure the motion \(d_x\)
  • precisely measure the applied force \(F_x\)
  • precisely now the height of the force application point \(h\)

4.5 Estimation error due to force and displacement sensors accuracy

The maximum error on the measured displacement with the encoder is 40 nm. This quite negligible compared to the measurement range of 0.5 mm.

The accuracy of the force sensor is around 1% and therefore, we should expect to have an accuracy on the measured stiffness of at most 1%.

4.6 Estimation error due to Shear

The effect of Shear on the measured displacement is simply:

\begin{equation} D_s = \frac{F_x}{k_s} \end{equation}

The measured displacement will be the effect of shear + effect of bending

\begin{equation} d_x = D_b + D_s = h \tan\left( \frac{F_x \cdot h}{k_{R_y}} \right) + \frac{F_x}{k_s} \approx F_x \left( \frac{h^2}{k_{R_y}} + \frac{1}{k_s} \right) \end{equation}

The estimated bending stiffness \(k_{\text{est}}\) will then be:

\begin{equation} k_{\text{est}} = h^2 \frac{F_x}{d_x} \approx k_{R_y} \frac{1}{1 + \frac{k_{R_y}}{k_s h^2}} \end{equation}
The measurement error due to Shear is 0.1 %

4.7 Estimation error due to force sensor compression

The measured displacement is not done directly at the joint’s location. The force sensor compression will then induce an error on the joint’s stiffness.

The force sensor stiffness \(k_F\) is estimated to be around:

kF = 50/0.05e-3; % [N/m]
k_F = 1.0e+06 [N/m]

The measured displacement will be the sum of the displacement induced by the bending and by the compression of the force sensor:

\begin{equation} d_x = D_b + \frac{F_x}{k_F} = h \tan\left( \frac{F_x \cdot h}{k_{R_y}} \right) + \frac{F_x}{k_F} \approx F_x \left( \frac{h^2}{k_{R_y}} + \frac{1}{k_F} \right) \end{equation}

The estimated bending stiffness \(k_{\text{est}}\) will then be:

\begin{equation} k_{\text{est}} = h^2 \frac{F_x}{d_x} \approx k_{R_y} \frac{1}{1 + \frac{k_{R_y}}{k_F h^2}} \end{equation}
The measurement error due to height estimation errors is 0.8 %

4.8 Estimation error due to height estimation error

Let’s consider an error in the estimation of the height from the application of the force to the joint’s center:

\begin{equation} h_{\text{est}} = h (1 + \epsilon) \end{equation}

The computed bending stiffness will be:

\begin{equation} k_\text{est} \approx h_{\text{est}}^2 \frac{F_x}{d_x} \end{equation}

And the stiffness estimation error is:

\begin{equation} \frac{k_{\text{est}}}{k_{R_y}} = (1 + \epsilon)^2 \end{equation}
h_err = 0.2e-3; % Height estimation error [m]
The measurement error due to height estimation errors of 0.2 [mm] is 1.6 %

4.9 Conclusion

Based on the above analysis, we should expect no better than few percent of accuracy using the current test-bench. This is well enough for a first estimation of the bending stiffness of the flexible joints.

Another measurement bench allowing better accuracy will be developed.

5 First Measurements

5.1 Agreement between the probe and the encoder

The measurement setup is made such that the probe measured the translation table displacement. It should then measure the same displacement as the encoder. Using this setup, we should be able to compare the probe and the encoder.

Let’s load the measurements.

load('meas_probe_against_encoder.mat', 't', 'd', 'dp', 'F')

The time domain measured displacement by the probe and by the encoder is shown in Figure 13.

comp_encoder_probe_time.png

Figure 13: Time domain measurement

If we zoom, we see that there is some delay between the encoder and the probe (Figure 14).

comp_encoder_probe_time_zoom.png

Figure 14: Time domain measurement (Zoom)

This delay is estimated using the finddelay command.

The time delay is approximately 15.8 [ms]

The measured mismatch between the encoder and the probe with and without compensating for the time delay are shown in Figure 15.

comp_encoder_probe_mismatch.png

Figure 15: Measurement mismatch, with and without delay compensation

Finally, the displacement of the probe is shown as a function of the displacement of the encoder and a linear fit is made (Figure 16).

comp_encoder_probe_linear_fit.png

Figure 16: Measured displacement by the probe as a function of the measured displacement by the encoder

From the measurement, it is shown that the probe is well calibrated. However, there is some time delay of tens of milliseconds that could induce some measurement errors.

5.2 Measurement of the Millimar 1318 probe stiffness

setup_mahr_stiff_meas_side.jpg

Figure 17: Setup - Side View

setup_mahr_stiff_meas_top.jpg

Figure 18: Setup - Top View

Let’s load the measurement results.

load('meas_stiff_probe.mat', 't', 'd', 'dp', 'F')

The time domain measured force and displacement are shown in Figure 19.

mahr_time_domain.png

Figure 19: Time domain measurements

Now we can estimate the stiffness with a linear fit.

This is very close to the 0.04 [N/mm] written in the Millimar 1318 probe datasheet.

And compare the linear fit with the raw measurement data (Figure 20).

mahr_stiffness_f_d_plot.png

Figure 20: Measured displacement as a function of the measured force. Raw data and linear fit

The Millimar 1318 probe has a stiffness of \(\approx 0.04\,[N/mm]\).

6 Bending Stiffness Measurement

6.1 Introduction

A picture of the bench used to measure the X-bending stiffness of the flexible joints is shown in Figure 21. A closer view on flexible joint is shown in Figure 22 and a zoom on the force sensor tip is shown in Figure 23.

picture_bending_x_meas_side_overview.jpg

Figure 21: Side view of the flexible joint stiffness bench. X-Bending stiffness is measured.

picture_bending_x_meas_side_close.jpg

Figure 22: Zoom on the flexible joint - Side view

picture_bending_x_meas_side_zoom.jpg

Figure 23: Zoom on the tip of the force sensor

The same bench used to measure the Y-bending stiffness of the flexible joint is shown in Figure 24.

picture_bending_y_meas_side_close.jpg

Figure 24: Stiffness measurement bench - Y-d bending measurement

6.2 Analysis of one measurement

In this section is shown how the data are analysis in order to measured:

  • the bending stiffness
  • the bending stroke
  • the stiffness once the mechanical stops are in contact

The height from the flexible joint’s center and the point of application force \(h\) is defined below:

h = 25e-3; % [m]
%% Load Data
load('meas_stiff_flex_1_x.mat', 't', 'F', 'd');

%% Zero the force
F = F - mean(F(t > 0.1 & t < 0.3));

%% Start measurement at t = 0.2 s
d = d(t > 0.2);
F = F(t > 0.2);
t = t(t > 0.2); t = t - t(1);

The obtained time domain measurements are shown in Figure 25.

flex_joint_meas_example_time_domain.png

Figure 25: Typical time domain measurements

The displacement as a function of the force is then shown in Figure 26.

flex_joint_meas_example_F_d.png

Figure 26: Typical measurement of the diplacement as a function of the applied force

The bending stiffness can be estimated by computing the slope of the curve in Figure 26. The bending stroke and the stiffness when touching the mechanical stop can also be estimated from the same figure.

%% Determine the linear region and region when touching the mechanical stop
% Find when the force sensor touches the flexible joint
i_l_start = find(F > 0.3, 1, 'first');
% Reset the measured diplacement at that point
d = d - d(i_l_start);
% Find then the maximum force is applied
[~, i_s_stop] = max(F);
% Linear region stops ~ when 90% of the stroke is reached
i_l_stop = find(d > 0.9*d(i_s_stop), 1, 'first');
% "Stop" region start ~1N before maximum force is applied
i_s_start = find(F > max(F)-1, 1, 'first');

%% Define variables for the two regions
F_l = F(i_l_start:i_l_stop);
d_l = d(i_l_start:i_l_stop);

F_s = F(i_s_start:i_s_stop);
d_s = d(i_s_start:i_s_stop);
%% Fit the best straight line for the two regions
fit_l = polyfit(F_l, d_l, 1);
fit_s = polyfit(F_s, d_s, 1);

%% Reset displacement based on fit
d = d - fit_l(2);
fit_s(2) = fit_s(2) - fit_l(2);
fit_l(2) = 0;

The raw data as well as the fit corresponding to the two stiffnesses are shown in Figure 27.

flex_joint_meas_example_F_d_lin_fit.png

Figure 27: Typical measurement of the diplacement as a function of the applied force with estimated linear fits

Then, the bending stroke is estimated as crossing point between the two fitted lines:

d_max = fit_l(1)*fit_s(2)/(fit_l(1) - fit_s(1));

The obtained characteristics are summarized in Table 5.

Table 5: Estimated characteristics of the flexible joint number 1 for the X-direction
Bending Stiffness [Nm/rad] 5.5
Bending Stiffness @ stop [Nm/rad] 173.6
Bending Stroke [mrad] 18.9

6.3 Bending stiffness and bending stroke of all the flexible joints

Now, let’s estimate the bending stiffness and stroke for all the flexible joints.

The results are summarized in Table 6 for the X direction and in Table 7 for the Y direction.

Table 6: Measured characteristics of the flexible joints in the X direction
  Bending Stiff X [Nm/rad] Stop Stiff X [Nm/rad] Bending Stroke X [mrad]
1 5.5 173.6 18.9
2 6.1 195.0 17.6
3 6.1 191.3 17.7
4 5.8 136.7 18.3
5 5.7 88.9 22.0
6 5.7 183.9 18.7
7 5.7 157.9 17.9
8 5.8 166.1 17.9
9 5.8 159.5 18.2
10 6.0 143.6 18.1
11 5.0 163.8 17.7
12 6.1 111.9 17.0
13 6.0 142.0 17.4
14 5.8 130.1 17.9
15 5.7 170.7 18.6
16 6.0 148.7 17.5
Table 7: Measured characteristics of the flexible joints in the Y direction
  Bending Stiff Y [Nm/rad] Stop Stiff Y [Nm/rad] Bending Stroke Y [mrad]
1 5.7 323.5 17.9
2 5.9 306.0 17.2
3 6.0 224.4 16.8
4 5.7 247.3 17.8
5 5.8 250.9 13.0
6 5.8 244.5 17.8
7 5.3 214.8 18.1
8 5.8 217.2 17.6
9 5.7 225.0 17.6
10 6.0 254.7 17.3
11 4.9 261.1 18.4
12 5.9 161.5 16.7
13 6.1 227.6 16.8
14 5.9 221.3 17.8
15 5.4 241.5 17.8
16 5.3 291.1 17.7

6.4 Analysis

The dispersion of the measured bending stiffness is shown in Figure 28 and of the bending stroke in Figure 29.

bending_stiffness_histogram.png

Figure 28: Histogram of the measured bending stiffness

bending_stroke_histogram.png

Figure 29: Histogram of the measured bending stroke

The relation between the measured beam thickness and the measured bending stiffness is shown in Figure 30.

flex_thickness_vs_bending_stiff.png

Figure 30: Measured bending stiffness as a function of the estimated flexible beam thickness

6.5 Conclusion

The measured bending stiffness and bending stroke of the flexible joints are very close to the estimated one using a Finite Element Model.

The characteristics of all the flexible joints are also quite close to each other. This should allow us to model them with unique parameters.

Author: Dehaeze Thomas

Created: 2021-03-04 jeu. 17:20