50 KiB
Flexible Joints - Test Bench
- Introduction
- Dimensional Measurements
- Measurement Test Bench - Bending Stiffness
- Error budget
- First Measurements
- Bending Stiffness Measurement
- Conclusion
- Bibliography
This report is also available as a pdf.
Introduction ignore
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 ref:tab:test_joints_specs.
Specification | FEM | |
---|---|---|
Axial Stiffness | $> 100\,N/\mu m$ | 94 |
Shear Stiffness | $> 1\,N/\mu m$ | 13 |
Bending Stiffness | $< 100\,Nm/\text{rad}$ | 5 |
Torsion Stiffness | $< 500\,Nm/\text{rad}$ | 260 |
Bending Stroke | $> 1\,\text{mrad}$ | 24.5 |
Torsion Stroke | $> 5\,\mu\text{rad}$ |
Then, the classical geometry of a flexible ball joint shown in Figure ref:fig:test_joints_fem_geometry 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 ref:tab:test_joints_specs.
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 ref:fig:test_joints_received.
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:
- Section ref:sec:test_joints_flex_dim_meas: each flexible joint is measured using a profile projector
- Section ref:sec:test_joints_test_bench_desc: the stiffness measurement bench is presented
- Section ref:sec:test_joints_error_budget: an error budget is performed in order to estimate the accuracy of the measured stiffness
- Section ref:sec:test_joints_first_measurements: first measurements are performed
- Section ref:sec:test_joints_bending_stiffness_meas: the bending stiffness of the flexible joints are measured
Sections | Matlab File |
---|---|
Section ref:sec:test_joints | test_joints_1_.m |
Dimensional Measurements
<<sec:test_joints_flex_dim_meas>>
Measurement Bench
The axis corresponding to the flexible joints are defined in Figure ref:fig:test_joints_axis.
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 "X" flexible beam is shown in Figure ref:fig:test_joints_y_flex_meas_setup.
What we typically observe is shown in Figure ref:fig:test_joints_soft_measure_size. It is then possible to estimate to dimension of the flexible beam with an accuracy of $\approx 5\,\mu m$,
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 ref:tab:test_joints_flex_dim.
Y1 | Y2 | X1 | X2 | |
---|---|---|---|---|
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 ref:fig:test_joints_size_hist.
Bad flexible joints
Measurement Test Bench - Bending Stiffness
<<sec:test_joints_test_bench_desc>>
Introduction ignore
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 ref:fig:test_joints_bench_working_principle. 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 $d_x$.
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.
Flexible joint Geometry
The flexible joint used for the Nano-Hexapod is shown in Figure ref:fig:test_joints_bend_geometry. Its bending stiffness is foreseen to be $k_{R_y}\approx 5\,\frac{Nm}{rad}$ and its stroke $\theta_{y,\text{max}}\approx 25\,mrad$.
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]
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 $6.2\,N$.
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 $0.5\,mm$.
Test Bench
A CAD view of the measurement bench is shown in Figure ref:fig:test_joints_bench_overview.
Here are the different elements used in this bench:
- Translation Stage: V-408
- Load Cells: FC2231-0000-0010-L
- Encoder: Renishaw Resolute 1nm
Both the measured force and displacement are acquired at the same time using a Speedgoat machine.
A side view of the bench with the important quantities are shown in Figure ref:fig:test_joints_bench_side.
Error budget
<<sec:test_joints_error_budget>>
Introduction ignore
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.
Finite Element Model
From the Finite Element Model, the stiffness and stroke of the flexible joint have been computed and summarized in Tables ref:tab:test_joints_axial_shear_prop and ref:tab:test_joints_bending_torsion_prop.
Stiffness [N/um] | Max Force [N] | Stroke [um] | |
---|---|---|---|
Axial | 94 | 469 | 5 |
Shear | 13 | 242 | 19 |
Stiffness [Nm/rad] | Max Torque [Nmm] | Stroke [mrad] | |
---|---|---|---|
Bending | 5 | 118 | 24 |
Torsional | 260 | 1508 | 6 |
Setup
The setup is schematically represented in Figure ref:fig:test_joints_bench_side_bis.
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]
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}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 $h$
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%.
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 %
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 %
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 %
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.
First Measurements
<<sec:test_joints_first_measurements>>
Introduction ignore
- Encoder: Renishaw Resolute 1nm
Force Sensor Calibration
Load Cells:
There are both specified to have $\pm 1 \%$ of non-linearity over the full range.
The XFL212R has a spherical interface while the FC2231 has a flat surface. Therefore, we should have a nice point contact when using the two force sensors as shown in Figure ref:fig:test_joints_force_sensor_calib.
The two force sensors are therefore measuring the exact same force, and we can compare the two measurements.
Let's load the measured force of both sensors.
%% Load measurement data
load('calibration_force_sensor.mat', 't', 'F', 'Fc')
We remove any offset such that they are both measuring no force when not in contact.
%% Remove offset
F = F - mean(F( t > 0.5 & t < 1.0));
Fc = Fc - mean(Fc(t > 0.5 & t < 1.0));
Let's select only the first part from the moment they are in contact until the maximum force is reached.
%% Only get the first part until maximum force
F = F( t > 1.55 & t < 4.65);
Fc = Fc(t > 1.55 & t < 4.65);
Then, let's make a linear fit between the two measured forces.
%% Make a line fit
fit_F = polyfit(Fc, F, 1);
The two forces are plotted against each other as well as the linear fit in Figure ref:fig:test_joints_force_sensor_calib_fit.
The measurement error between the two sensors is shown in Figure ref:fig:test_joints_force_sensor_calib_error. It is below 0.1N for the full measurement range.
Force Sensor Stiffness
The objective of this measurement is to estimate the stiffness of the force sensor FC2231-0000-0010-L.
To do so, a very stiff element is fixed in front of the force sensor as shown in Figure ref:fig:test_joints_meas_force_sensor_stiffness.
Then, we apply a force on the stiff element through the force sensor. We measure the deflection of the force sensor using an encoder.
Then, having the force and the deflection, we should be able to estimate the stiffness of the force sensor supposing the stiffness of the other elements are much larger.
From the documentation, the deflection of the sensor at the maximum load (50N) is 0.05mm, the stiffness is therefore foreseen to be around $1\,N/\mu m$.
Let's load the measured force as well as the measured displacement.
%% Load measurement data
load('force_sensor_stiffness_meas.mat', 't', 'F', 'd')
Some pre-processing is applied on the data.
%% Remove offset
F = F - mean(F(t > 0.5 & t < 1.0));
%% Select important part of data
F = F( t > 4.55 & t < 7.24);
d = d( t > 4.55 & t < 7.24); d = d - d(1);
t = t( t > 4.55 & t < 7.24);
The linear fit is performed.
%% Linear fit
fit_k = polyfit(F, d, 1);
The displacement as a function of the force as well as the linear fit are shown in Figure ref:fig:test_joints_force_sensor_stiffness_fit.
And we obtain the following stiffness:
k = 0.76 [N/um]
Bending Stiffness Measurement
<<sec:test_joints_bending_stiffness_meas>>
Introduction
A picture of the bench used to measure the X-bending stiffness of the flexible joints is shown in Figure ref:fig:test_joints_picture_bench_overview. A closer view on flexible joint is shown in Figure ref:fig:test_joints_picture_bench_close and a zoom on the force sensor tip is shown in Figure ref:fig:test_joints_picture_bench_zoom.
The same bench used to measure the Y-bending stiffness of the flexible joint by pivoting the flexible joint by 90 degrees.
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 ref:fig:test_joints_meas_bend_time.
The displacement as a function of the force is then shown in Figure ref:fig:test_joints_meas_F_d.
The bending stiffness can be estimated by computing the slope of the curve in Figure ref:fig:test_joints_meas_F_d. 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 ref:fig:test_joints_meas_F_d_lin_fit.
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:
- Bending Stiffness: 5.5Nm/rad
- Bending Stiffness at stop: 173.6Nm/rad
- Bending Stroke: 18.9mrad
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 ref:tab:test_joints_meas_results_x_dir for the X direction and in Table ref:tab:test_joints_meas_results_y_dir for the Y direction.
$R_{R_x}$ [Nm/rad] | $k_{R_x,s}$ [Nm/rad] | $R_{x,\text{max}}$ [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 |
$R_{R_y}$ [Nm/rad] | $k_{R_y,s}$ [Nm/rad] | $R_{y,\text{may}}$ [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 |
Analysis
The dispersion of the measured bending stiffness is shown in Figure ref:fig:test_joints_bend_stiff_hist and of the bending stroke in Figure ref:fig:test_joints_bend_stroke_hist.
The relation between the measured beam thickness and the measured bending stiffness is shown in Figure ref:fig:test_joints_thickness_stiffness.
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.
Conclusion
<<sec:test_joints_conclusion>>