The Smart Stick adaptive structure/Smart Stick adaptyvi konstrukcija.
Pilkauskas, K. ; Gaidys, R. ; Lira, C. 等
1. Introduction
Nowadays we observe the development of modern technologies in
different fields such as industrial manufacture, transport, services,
house facilities, public security, space exploration which stimulate the
generation of new conceptual ideas in many fields of engineering. The
field which becomes the basic for different mentioned areas is
mechatronics. The characteristic (basic) components of mechatronic
systems are: actuators, sensors, control systems, interfaces and
materials [1-3]. At present in industrial robotic applications the
oleo-hydraulic pump system mechanisms is mainly actuated by
electromagnetic servo drives. The tendency to use more electro hydraulic
motors is observed as well. However such conventional concept represents
a major bottleneck towards high precision, light weight, flexible and
adaptive component development. The conventional scheme consists of
motors, gears, sensors and numerous connectors. Such architecture makes
the system complicated and expensive to manufacture. An entire new
approach to the robot design, using new types of advanced materials, new
actuators, bioinspired or biomimetic structures seems to be the more
promising way to obtain a reliable mechatronic system.
Efforts to build precision mechanisms based on elastically deformed
frames, elastically hinged structures with the features of mechanical
advantages (displacement amplification) results in promising structures
for precision engineering [4]. Their integration with micro fluidic
systems or basically micro fluidic actuation, as well as active material
actuated systems seems to be perspective way for micro mechatronic
systems development [5, 6].
With the aim to obtain adaptive structures with the distributed
compliance numerous research attempts are made to develop actuators the
functioning features of which mimics biological muscles. Mainly they can
be classified into two major groups: actuators based on fluidic
principles of operation and actuators based on electro-active polymers.
[FIGURE 1 OMITTED]
One of the first well known results in the development of actuators
based on fluidic principle is the McKibben Artificial Muscle [7] which
contracts like a real muscle developing axial force when pressure is
supplied. Its application for robot arm and leg articulation is reported
in [8]. The novel type of actuator which consists of two rigid links
joined by rotational hinge and inflatable ball placed between them can
be used for an ultra light anthropomorphic hand development. The
application of fluidic actuator is reported as well in variable
structure fabric--the fabric which can change shape or mechanical
parameters (stiffness) when actuated [9, 10]. The current research aims
to investigate the interaction process of a mini pipe and rigid U-shaped
link which serves as a structural unit (or brick) for constructing the
adaptive structure "Smart Stick" both at the stage of mini
pipe insertion and the operation stage when the mini pipe is inflated
using external pressure source.
2. Mechanical design of the module
Mechanical part of the structure under investigation consists of a
number of periodically arranged in longitudinal direction U-shaped
structural elements (Fig. 1) manufactured of high elasticity material
(e.g. alloyed steel).
The two basic arrangements with the functioning of both of them
based on the same operational principle are developed for the
investigation (Fig. 2, a, b). The first embodiment employs U-shaped
member (link) considered as absolutely rigid body which is rigidly fixed
on a foil considered as elastic element in a series manner. A single
tube inserted in between the members (links) acts as a fluidic actuator
which when inflated expands causing angular displacement of one element
with respect to another. Total motion (displacement) of the whole
"Smart Stick" is the resultant (sum) of angular displacements
of all the structural units (U-shaped spacer--tube--U-shaped spacer).
The second embodiment employs U-shaped member the side parts of which
are relatively thick and the bottom part relatively thin what implies an
assumption the side parts to be treated as rigid and the bottom part as
elastic. The fluidic actuator in the form of mini tube inserted in
between the side parts of U shape when inflated expands causing angular
displacement of one side of the U shape with respect to another. The
U-shaped links attached rigidly one to another by their sides form the
mechanical structure of "Smart Stick". The resultant
displacement (movement) is the sum of angular displacements of all the
U-shaped members forming the stick.
[FIGURE 2 OMITTED]
The application of a single tubular actuator folded in between
rigid side parts of U-shaped members is an effective means for actuating
the "Smart Stick". Nevertheless to seek for the best
performance circular shape of its cross-section is least favourable and
the favourable shape is shown in Fig. 3. Sequentially the tubular
actuator should periodically have the second type cross-sections
(elliptical shape).
[FIGURE 3 OMITTED]
Basically the two main cases have been already analysed for
functioning principles. According the first case the necessary parts of
tubular actuator are initially plastically deformed and in further
modelling an assumption of perfect shape as in Fig. 3 was used [11, 12].
According the second assumption a min pipe of circular cross-section was
used and it was elastically deformed (approaching the shape of Fig. 3)
during assembly process. Two stages were modelled and simulated--elastic
deformation during assembly with no inner pressure and operation stage
when the inner pressure was supplied causing angular displacement of the
structure [13].
In the current research with the aim of interaction process
analysis of the mini tube with rigid element the initially pre-stressed
arrangement was analysed. The angle of expansion due to tube insertion
into the elastic joint and subsequent inflation is obtained and compared
with experimental results.
It is worth mentioning that such arrangement is easy to manufacture
and the application of a single tube for actuation avoiding mechanical
connectors makes the system simple reliable and light weight.
3. Computational model
Performance of the whole "Smart Stick" is predefined by
the behaviour of its single cell--structural unit. For the embodiments
of both cases described earlier the single unit can be represented in
Fig. 2 FEM analysis of the system shown in Fig. 2, a was performed. The
computational model corresponding it is shown in Fig. 4, a. It
represents one rigid spacer (embodiment No. 1) or one rigid side of the
U element (embodiment No. 2) half of the tube and elastic element (foil
or bottom part of U-shaped element) the length of which is half gap
width between the spacers or half U span.
[FIGURE 4 OMITTED]
Mechanical characteristics of the materials of U-shaped element are
given in Table 1.
The following dimensions were used for simulation with the aim of
experimental data benchmark:
--spacer height 2 mm,
--foil thickness 0.1 mm,
--outside diameter of the tube 2.08 mm,
--Tube wall thickness 0.255 mm
[FIGURE 5 OMITTED]
The width of the elastic elements is 50 mm.
Behaviour of the cell--elementary unit was analyzed by FEM using
the software code FEMLAB 3.1. The first simulation phase--the tube
insertion was performed as follows. Assuming that there is no pressure
on the inner tube wall at initial position shown in Fig. 4, a the end
point A was moved vertically downwards deforming the system elements
elastically and allowing the points B of the half tube contour to move
freely in horizontal direction (Fig. 4, b). At the second simulation
phase--system operation pressure on the inner surface of the half tube
was applied further deforming elements of the system (Fig. 4, b) what
resulted in angular position change of the spacer after pressure is
supplied as shown in Fig. 4, c. Resultant displacements of the system
elements for the both simulation phases are shown in Fig. 5.
4. Experimental research
The degree to which the system deforms under various pressures
within the tubing was measured and compared against results from
previous experimentation and finite element analysis. A mechanical pump
was used to maintain the pressure at a constant while the results were
recorded. The deformation of a single joint (i.e. one tube between two
spacers) was recorded as described below. Although the fluidic actuator
is suitable for gas or liquid it was decided to carry out pressure
testing using liquid, as this fluid best suited the available equipment.
As the increase of pressure caused the actuation, thus the particular
working fluid type was irrelevant for characterisation.
4.1. Optical test rig
In order to calculate the angle of rotation of a single elastic
joint the smart stick was fixed so that only one joint was free to
rotate, a mirror was mounted on the front of the spacer. A tube as
described earlier was inserted between the free to rotate spacer and a
fixed spacer, the pressure in this tube was then controlled via a hand
pump that was connected to a pressure sensor. The pressure sensor was
attached to a voltmeter to give voltage changes which could then be
converted into pressure change. The laser was aimed at the mirror and
focused a board covered with graduated paper behind the laser. As the
pressure increased the smart stick joint rotated and the position of the
laser point moved. The positioned was recorded at specific voltages. The
diagram below (Fig. 6, 7) outlines the rig setup.
[FIGURE 6 OMITTED]
[FIGURE 7 OMITTED]
In order to calculate the rotation the law of rotation was applied
[[theta].sub.i] = [[theta].sub.r] (1)
Where n is perpendicular to the surface, [[theta].sub.i] is the
angle to the normal at which the beam hits the reflective surface and
[[theta].sub.r] is the angle to the normal at which the beam is
reflected.
As a result the angle of rotation can be calculated using the
following equation
[theta] = 1/2 arctan (M/D) (2)
But assuming [theta] is small:
[theta] [approximately equal to] 1/2 (M/D) (3)
To calculating the uncertainty in 6, we require the uncertainty in
D and M and using the relationship in [14].
D = 6300mm [M.sub.max] = 0.445mm [[delta].sub.D] = 2 m
[[delta].sub.M] - 1 m
[MATHEMATICAL EXPRESSION NOT REPRODUCIBLE IN ASCII] (4)
Numerically
[MATHEMATICAL EXPRESSION NOT REPRODUCIBLE IN ASCII] (5)
It was assumed that extended uncertainty [i.sub.[theta]] = [+ or
-]0.125 degrees and uncertainty in direct measure of pressure [i.sub.p]
= [+ or -]0.0025 MPa is suitable for test rig.
4.2. Experimental results
This is not especially useful for data analysis so consequentially
the cycles were averaged, in order to obtain a cycle that could then be
assessed. The following graph shows the averaged cycles for the single
sided ABS spacer (Fig. 8). The uncertainty in pressure was calculated
using [14] as [+ or -]0.002 MPa per reading and the uncertainty in angle
was calculated as 0.25o per measurement. These values were constant
throughout the experiment and are shown on the graph in the form of
error boxes (indicating that the true value lies at some position within
these boundaries). It can be seen form this graph that the loading and
unloading cycles are different, the loading cycle begins at the zero
position however on returning to ambient pressure the there is a
rotational offset.
[FIGURE 8 OMITTED]
5. Results and conclusions
The results of experimental research and simulation were used to
obtain performance characteristics of "Smart Stick". The most
important of them "angular displacement vs. applied pressure"
is shown in Fig. 9
Sufficient agreement of experimental and simulation results proves
the validity of the selected computational model. Sequentially the
presented simulation approach can be applied for the investigation of
structures of different architectures built on the basics of structural
unit (units) the research of which is presented in the paper.
Compliant in its nature foil spacer or U-shaped elements periodic
arrangement actuated by a single tube with no connectors together with
active material pressurization block are the basic elements for
mechatronic modules development which are embeddable into different
structure systems.
[FIGURE 9 OMITTED]
Multimodule realization of "Smart Stick", with
corresponding control unit, is the way to develop multi DOF actuation
structures.
Received May 25, 2009
Accepted August 21, 2009
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K. Pilkauskas *, R. Gaidys **, C. Lira ***
* Kaunas University of Technology, Mickeviciaus 37, 442445 Kaunas,
Lithuania, E-mail: kestutis.pilkauskas@ktu.lt
** Kaunas University of Technology, Studentu 50, 51368 Kaunas,
Lithuania, E-mail: rimvydas.gaidys@ktu.lt
*** University of Bristol, Queen's Building, University Walk,
BS8 1TR Bristol, UK, E-mail: c.lira@bristol.ac.uk
Table 1
Element
Elastic link Fluidic Actuator
Material: AISI 301 Material: Polivynil
E = 193 GPa E = 19.3 MPa
v = 0.33 [micro] = 0.28
p = 7900 kg/[m.sup.3] [rho] = 1010 kg/[m.sup.3]
[[sigma].sub.y] = 352 [[sigma].sub.y] = 17
[10.sup.6] Pa [10.sup.6] Pa