Upload
rogo-catalin
View
214
Download
0
Embed Size (px)
Citation preview
7/29/2019 Hybrid layer
1/11
Robotics and Computer-Integrated Manufacturing 22 (2006) 113123
Hybrid adaptive layer manufacturing: An Intelligent art of direct
metal rapid tooling process
Sreenathbabu Akula, K.P. Karunakaran
Mechanical Engineering Department, Indian Institute of Technology, Bombay, India
Received 21 June 2004; received in revised form 2 February 2005; accepted 11 February 2005
Abstract
A direct metal rapid tool making process, hybrid-layered manufacturing (HLM), was developed for building metallic dies and
molds. This unique methodology has a numerical controlled system that integrates the TransPulse Synergic Metal Inert Gas (MIG)/
Metal Active Gas (MAG) welding process for near-net layer deposition and Computer Numerical Control (CNC) milling process for
net shaping. A customized software program was made to calculate the required adaptive slice thickness for the deposition of the
filler metal with welding process as successive layers from the lowest to the topmost layer direction and to generate the required NC
codes for machining from the top to the bottom layer direction of the deposited metallic layers for attaining the required contour
profile shape. To implement this proposed process, a low-cost three-axis manipulator was fabricated with stepper motor divers in
open-loop control and integrated with the weld machine. Adequate isolation to protect the motion control electronics from welding
spike was incorporated. Synchronization of this two-step processing of each layer, yielding near-net deposition with welding process
and near-net shaping with CNC milling operation offers a new accelerator way of building metal tools and dies.
r 2005 Elsevier Ltd. All rights reserved.
Keywords: Rapid tooling (RT); Welding; CNC machining; Slicing; Molds and dies
1. Introduction
Building pre-production models of a product to test
various aspects of the aesthetic, ergonomic, functioning
and design are known as prototypes. With the concept
of globalization, the multinational corporations in the
open market system, the competition among the
industries has become very acute. The demand for
shorter development time, and reduced product life
cycle resulted in the emergence of a new paradigm calledTime Compression Techniques (TCT) or Rapid Proto-
typing (RP) [1,2].
The main process stages involved in fabricating
prototypes are common to most RP systems that are
currently available or under development, but the
mechanisms by which the individual layers are created
obviously depend on the particular system. A new
approach known as Direct RP through which a
prototype of the parent material can be generated has
emerged [3,4]. Some use laser welding whereas a
majority of them use Metal Inert Gas (MIG) welding.
In Laser Generating and High-Speed Milling process
developed at Fraunhofer Institute for Production
Technology (FhG-IPT), Germany, the raw material
used is binder-coated metallic powder, which whenpassed through the nozzle is melted by a laser beam
resulting in the deposition of the near-net layer. The
layer is then milled to net-shape. As this process makes
use of uniform slicing of 0th-order edge approximation,
it is not rapid enough [5].
Shape Deposition Manufacturing (SDM) process
developed at Carnegie Mellon University, US, uses an
additive process to deposit the rough material and a
machining process to get the desired accuracy. However,
ARTICLE IN PRESS
www.elsevier.com/locate/rcim
0736-5845/$ - see front matterr 2005 Elsevier Ltd. All rights reserved.
doi:10.1016/j.rcim.2005.02.006
Corresponding author.
E-mail addresses: [email protected] (S. Akula),
[email protected] (K.P. Karunakaran).
http://www.elsevier.com/locate/rcimhttp://www.elsevier.com/locate/rcim7/29/2019 Hybrid layer
2/11
instead of sintering by a laser beam, they use a
deposition process called micro-casting, which is in
between metal spraying and welding processes. It uses 5-
axis machining that enables to make the profiles [6].
3D Welding process developed at the University of
Nottingham also uses an MIG welding process to build
metallic prototypes [7]. Using a 0.8 mm diameter wire,they report a building speed of 6500 mm/min, the bead
size being 4.5 mm wide and 1.4 mm thick. Although the
building speed of this process is very attractive, the poor
accuracy of 0.5 mm limits its applications. Similar
research is going on at several universities abroad
although they are not far away from commercialization.
Some of them are Southern Methodist University, US
[8]; Cranfield University, UK, Loughborough Univer-
sity, UK; Fraunhofer Institutes in Germany; Korean
Institute of Science & Technology (KIST) [9], University
of Kentucky, Lexington, US [10], and University of
Michigan, US. Each has its unique features and they
differ from one another in various ways. Similarly, they
differ in the type of slicing used, method of support
structure, application areas, etc. At the Indian Institute
of Technology, Bombay, it was proposed to develop a
hybrid-layered manufacturing (HLM) process with a
numerical controlled system that integrates the Pulse
synergic MIG/Metal Active Gas (MAG) process and
Computer Numerical Control (CNC) milling process to
build tools and dies [11].
2. Proposed process
2.1. Hybrid-layered manufacturing
In order to manufacture tools more accurately and
rapidly, a direct rapid tooling process should have the
following characteristics:
sintering or melting of the hard material directly;
two-step processing of each layer, the first step yields
the near-net layer deposition/formation and the
second step machines the layer to the required
accuracy;
efficient Slicing technique;
elimination/minimization of staircase effect;
high rate of material deposition;
ability to build support structures.
Considering these essential features for the direct
rapid tooling process, it was proposed to develop a
unique methodology for building metallic dies and
molds by employing a numerical controlled system that
integrates the TransPulse Synergic MIG/MAG welding
process for near-net layer deposition and CNC milling
process for net shaping. The TransPulse Synergic MIG/
MAG provides the controlled heat and mass transfer
with precise depth of bead penetration and the CNC
machining enhances both the surface quality and
dimensional accuracy with great manufacturing
agility.
To implement this process, a programmable logic
controller (PLC)-based low-cost three-axis manipulator
was fabricated with stepper motor diver in open-loopcontrol. The tool head of the manipulator will hold the
welding torch and milling cutter. At any time either
milling or welding will take place, and for that the
welding gun can be moved up and down with a
pneumatic operated piston. The NC codes M08 and
M09 are used to invoke the switching functions of the
pneumatic piston to move up and down, respectively.
Further, the NC codes M03 and M04 are made to
control the on/off of the welding torch during the metal
deposition. The parameters related to welding processes
such as the speed of the welding filler wire, diameter of
filler wire, type of filler material, voltage, current, gap
between the electrodes, shielding gas, built style, etc. are
to be fine-tuned and frozen after performing
the experiments. While a majority of the welding
parameters will be controlled externally, the necessary
functions to integrate the welding process with the
machine motion will be carried out by user defined G
and M codes.
The framework of this research also consists of a
customized software program that uses the zeroth-order
edge approximation uniform [12] and adaptive slicing
strategy [13] to calculate each slice thickness to be
deposited with the required metal as successive layers
from the lowest to the topmost layer with the weldingprocess. Further, it generates the required CNC code for
machining from the top to the bottom layer direction of
the deposited metallic layers to attain the required
contour profile shape with user-specified accuracy.
The process does not pose any restriction or loss of
accuracy on the prototype as its size grows. Since the
size of the part is limited only by the traverse available
on the CNC machine, a larger CNC machine can be
used to produce large tools. In this context, it is
interesting to note that the die halves used in injection
molding, pressure die casting, sheet metal forming, etc.
will be free of reentrant features overhanging features
since they need to open and close in operation.
Therefore, building such dies in the proposed process
will not require support structures. Furthermore, since
the fatigue loading they suffer in operation is consider-
ably less, these tools will serve the purpose even without
any homogenization operation such as Hot Isostatic
Pressing (HIP) process [14]. The tools produced using
this process may be inferior to their conventional
counterparts in composition and tool life but these will
generate the final products as accurately as any other
tool. This HLM process can be retrofitted to any CNC
machining center [15] (Fig. 1).
ARTICLE IN PRESS
S. Akula, K.P. Karunakaran / Robotics and Computer-Integrated Manufacturing 22 (2006) 113123114
7/29/2019 Hybrid layer
3/11
3. Methodology
Preliminary work in the area of 3D welding has
shown that complex shapes can be formed, but the
results are not perfect. The shape and dimensions
of the weld bead are very important in the use of 3D
welding as an RP system, since these will determine the
limits to the wall thickness, which may be produced
and will also influence the quality of the surface
finish. Although MIG/MAG welding cannot produce
the required accuracy, it is economical, safe, portable
and easy to maintain. Since only near-net layer is
being deposited in a hybrid process, low accuracy is
acceptable [16].
The developed HLM process will have the following
three stages:
i. building the near-net shape of the tool;
ii. heat treatment for stress relieving and strengthening;
iii. machining the near-net shape of the tool to final
dimensions.
3.1. Building the near-net shape of the tool
The metal deposition is done using a pulse Synergic
MIG/ MAG welding machine. The steps of the
deposition process are as follows:
Step one: Generate the tool path required to build
uniform/adaptive layers of zeroth-order edge approx-
imation from the bottom to the top:
The tool path consists of the paths for the welding gun
and the face mill and the required switching functions
M08 and M09. The clad zone for each layer will be
larger than the bottom contours of the layer by a
machining allowance. This allowance is from 0.5 to
2.0 mm. The switching functions are required for
change over between welding and face milling,
activating the welding operation and change over in
tool offset. The zeroth-order edge uniform slices of the
die of a connecting rod (Fig. 2) are shown in Fig. 3.
Step two: Fix a substrate on the table:
This substrate will conform to the mountings on the
press or injection molding machine on which it will be
used. It is recommended to have as thick a substrate as
possible. This will reduce distortion as well as building
time. This is possible because the dies invariably have a
thick bottom, which can become part of the substrate.
Step three: Select the necessary parameters on the
welding system:
The weld parameters of attained well-defined
bead geometry and layer thickness with adequate
ARTICLE IN PRESS
Fig. 1. Developed HLM machine.
Fig. 3. Zeroth-order edge uniform slicing.
Fig. 2. Die of a connecting rod.
S. Akula, K.P. Karunakaran / Robotics and Computer-Integrated Manufacturing 22 (2006) 113123 115
7/29/2019 Hybrid layer
4/11
machining allowance are selected. The weld machine
is operated in pulsed synergic mode.
Step four: Deposit the bottom most layer on the
substrate:
The welding path in any section or layer is of two
types: one is area-filling path (Fig. 4a) and the other is
contouring path (Fig. 4b). First, the deposition takesplace using area-filling paths and this is followed by
contouring. The deposited geometry fully covers the
required layer. However, it will be required to
optimize the path so as to transfer heat uniformly
over the layer. This is essential in view of the large
amount of heat input. Furthermore, arrangement for
preheating the substrate may also be required for
desirable patterns of grain size distribution.
After completion of the metal deposition at the
bottom most layer, the switching functions are
invoked to change over between welding and face
milling process by halting the welding process and
activating the face milling process and vice versa. For
this operation, a pneumatic system is used to swivel
between the welding gun and the milling cutter.
Step five: Face mill the top surface of the layer to
attain the required layer thickness:
The instability of the arc welding process may cause a
malfunction/defect in the middle of the weld bead. To
minimize and correct the deviation in successive
multiple layer deposition, face milling operation is
performed. This process step ensures the vertical Z
accuracy of building metal layer. Furthermore, the
welded surface may have an oxidized layer that
influences the subsequent layer deposited on top of it.
When milling is done, welding happens on a nascent
surface giving good quality of welding. Therefore, it is
required to do face milling after every layer deposition
though techno-economically not feasible for each
deposited layer (Fig. 5).
Repeat the above two steps for the remaining layers
till a casting like rough shape is obtained.
At the end, we will attain the near-net shape of the
required tool on the substrate.
3.2. Heat treatment for stress relieving and strengthening
Depending on the pattern of heat input, the grain
structure may be non-uniform and there could be
considerable amount of internal stresses. To relieve
them, suitable heat treatment is performed by annealing
or normalizing. HIP can densify the component and
improve its mechanical properties and fatigue life.
3.3. Machining the near-net shape of the tool to final
dimensions
All the horizontal surfaces of the tool are finished by
the face mill during the deposition stage and the edges of
the layers are still rough. These edges are machined in
this stage. This is done with the help of an end mill. The
tool paths consist of the paths for milling the edges of
each layer using a ball end mill in scan milling mode
using a maximum of three axes. The type and diameter
of the cutter will be automatically selected for different
regions by analyzing the local geometry [17]. The
approach involves splitting the machining surface into
three groups for the purpose of generating the cutter
path for their automatic machining: (i) a set of
horizontal surfaces, (ii) a set of vertical surfaces and
(iii) the set of remaining surfaces. The first set of surfaces
has already been machined during face milling; the
surfaces may, however, require touchup if spatter falls
on them. The other two sets of surfaces will be machined
using a flat or bull or ball end mill depending on whether
they are connected to the neighboring surface patches
sharply or through fillets [18,19].
ARTICLE IN PRESS
Fig. 4. Area-filling styles: (a) direction-parallel (also known as zigzag),
(b) contour-parallel (also known as spiral).
Fig. 5. Face milling on weld deposition.
S. Akula, K.P. Karunakaran / Robotics and Computer-Integrated Manufacturing 22 (2006) 113123116
7/29/2019 Hybrid layer
5/11
Finally, after completion of all these stages, the
desired metallic tool is attained.
4. HLM software
The HLM process consists of a custom-made soft-ware program that uses the zeroth-order edge approx-
imation slicing strategy of the RP paradigm to calculate
each slice thickness to be deposited with the required
metal as successive layers from the lowest to the topmost
layer with the welding process and it also generates the
required CNC code for machining from the top to the
bottom layer direction of the deposited metallic layers to
attain the required contour profile shape with user-
specified accuracy. Synchronization of the welding
process with work-piece/substrate motion and CNC
milling operation offers a new accelerator way of
building metal parts and tools.
Three types of NC programs are required in HLM:
i. paths for the layered weld deposition;
ii. paths for face milling each layer;
iii. paths for finish milling.
The first step for generating the welding path is to
slice the stereolithography (STL) file of the Computer
Aided Design (CAD) model into uniform layers of
zeroth-order edge approximation [20,21]. This results in
a set of loops defining each layer. During the near-net
layer generation, more material deposition has to
account for the machining allowance. Therefore, theloops defining each layer must be offset by the
machining allowance [22]. Having offset the loops of
the layer, the welding torch has to move along the
contours of the loops as well as their interior as per the
area-filling program. The area filling could be direction-
parallel or contour-parallel as described earlier. The
surface obtained after weld deposition will be scalloped
and have spatter deposition. In order to maintain Z
accuracy as well as to provide a flat nascent surface for
the next layer deposition, face milling is done. This is
relatively simple and is same for all layers but for the Z
coordinates. Having thus obtained the near-net layer, it
has to go for heat treatment and then finish machining.
For this purpose, a program for the layered machining
of the CAD surfaces has been developed. This finishing
is done within the required scallop tolerance and it can
make use of ball, bull and flat end mills.
The customized software, termed as Hybrid Layered
Manufacturing Software (HLMSoft), was developed to
run under Microsoft Windows platform. The code was
based on using Microsoft Visual C++ language. Micro-
soft Foundation Classes (MFC) were used to develop the
menus, dialog boxes and icons and the graphic outputs
were rendered using OpenGL graphics library. The
output files generated from the software, i.e. the weld
deposition path, face mill cutter path and the coarse
slice-machining paths, are of standard NC format as
shown in Fig. 6. These output files are compatible with
the protocol of the controller card SC03. The controller
card passes on these signals to the Control Box that
amplifies the power of these signals and feeds them to
the drive system.
4.1. Input format
The CAD model in an STL format, which is the de
facto standard for most of the RP processes, acts as the
input format for the software. The STL file consists of
unordered triangular facets, representing the surface of
an object. The tessellated facets are described by a set of
x, y and z coordinates for each of the three vertices andan outward pointing unit normal vector (Fig. 7).
4.2. Sectioning of the STL body with a plane
A verified and correct STL file of the CAD model in
binary format acts as the input file. The first step in this
process includes sectioning the tessellated body at
different vertical heights (z_levels) in relation to the
layer thickness to attain the information about the
number of contour loops, orientation of each loop and
the vertices of each loop [23].
4.3. Coarse slicing
Coarse slicing of the CAD model is the first step for
processing the body. Coarse slicing comprises of
decomposing the complex object into slices of simpler
geometry and then passing them for finer slicing. In a
coarse slicing, the number of loops in the top z_level and
in the bottom z_level will be the same, i.e. for each loop
in the bottom z_level there will be a corresponding loop
at the top level. In this slicing process it is essential to
establish the mapping between the top and the bottom
contours of a coarse slice.
ARTICLE IN PRESS
N0001 G28 Z0
N0020 G28 X0 Y0
N0030 M08 // To move pneumatic piston down
N0040 G10 L2 P1 X40.0 Y60.0 Z-150.0
N0050 G55
N0060 G90 G01 G21 F1000
N0070 G00 X0 Y0
N0120 M03 //To initiate the welding process
: :: :
N0500 M04 //To turn off the welding process
: :
: :
: :
N3990 M09 //To lift the pneumatic piston up
N4000 M30
Fig. 6. Output NC File of HLMSoftware.
S. Akula, K.P. Karunakaran / Robotics and Computer-Integrated Manufacturing 22 (2006) 113123 117
7/29/2019 Hybrid layer
6/11
Further, each coarse slice is divided in accordance to
the user-defined/required uniform slice or adaptive
slice thickness known as Fine Slicing [24]. Fine Slicing
is an iterative process to calculate slice thickness based
on the local curvature of the body. The data attainedthrough the Fine Slices are utilized for the path
generation of the MIG/MAG welding gun and the
face-milling operation.
4.4. Setting the process parameters
Using the dialog box as shown in Fig. 8, the user can
input the required parameters for welding as well as
milling processes. Welding-related parameters to be
input are as follows:
type of area-fill (direction-parallel or contour-paral-
lel);
slice thickness;
bead step over;
welding direction (applicable only to direction-paral-
lel area-fill);
machining allowance;
welding feed rate, i.e. torch speed.
Face-milling-related parameters to be input are:
diameter of the face mill,
feed rate for face mill.
Finish-milling-related parameters to be input are:
cutter diameter (of the ball end millinitially only
ball end mill was used),
cutter feed rate, cutter speed.
Parameters for Z control are:
Z-clear,
Z-rapid.
Parameters for work offset are:
X-work offset,
Y-work offset,
Z-work offset.
4.5. Weld deposition path
With the consideration of the limitations of the
welding process, the path for the welding gun has to
be generated to deposit the filler metal for attaining the
required slice profile shape and thickness. The tool path
is optimized to transfer heat uniformly over the layer as
the heat build-up due to the welding process may result
in part malformation and collapse of the structure.
Control of parameters and trajectory is added to the
start and the end portions of the weld in order to make
ARTICLE IN PRESS
Fig. 7. Various coarse slices in connecting rod. (a) Cross section at Bottom Slice, (b) Cross section at Middle Slice, (c) Cross section at Top Slice.
Fig. 8. Dialog Box of settings.
S. Akula, K.P. Karunakaran / Robotics and Computer-Integrated Manufacturing 22 (2006) 113123118
7/29/2019 Hybrid layer
7/11
their thickness and width similar to that of the central
portion of the weld. The joints (cross-sectional se-
quence) of weld pass decrease precision of the weld
deposition. So, to improve the deposition speed and
precision, it is necessary to optimize the number of weld
passes and joints between them.
Shrinkage and machining allowances are to be addedto Fine Slice contours. The outer contours will have a
positive offset, while the inner ones negative. The top
and bottom z_level contours of a layer are merged
(obtain the union of the outer contour and intersection
of inner contours). The slice thus obtained after
offsetting and merging is passed for mesh generation
in order to achieve the zigzag tool path segments
[2527]. These area-fill paths are then fed through the
controller to the three-axis manipulator (on which work
piece is fixed) and the weld machine to initiate the metal
deposition of the filler wire in a desired layer-by-layer
fashion.
4.6. Machining path
With the welding process, attaining the accurate
contour profile shape of the coarse slice is difficult.
For that, end-milling operation is performed to attain
the shape and accuracy. The tool path of the end mill is
generated with relation to coarse slicing and in
accordance to first-order edge adaptive approximation.
Adaptive slicing with first-order edge approximation
makes use of ruled surfaces [28]. As the coarse slice
passes the information of loops between the top and thebottom layers, a ruled surface has to be foud within the
upper limit deviation. In order to calculate the devia-
tion, a line is fitted to connect a point in the bottom loop
and the corresponding point in the top loop without
violating the tolerance constraint cusp height. The
corresponding point in the top loop is the one having the
same surface normal vector and nearest to the bottom
point. This results in the formation of a zigzag tool path
with the tool moving from top to bottom and back
several times. However, this tool path is not useful in
actual practice since it is possible to use it only for a tool
of negligible dimensions, i.e. a point tool. Therefore, the
data generated by this approach have to be modified for
tool accommodation. Hence, every point to be calcu-
lated is to be offset normal by an extent of tool radius
(in the plane of the loop). If the loop is extracted from a
positive simple body, outward normal is used and if it is
extracted from a negative simple body, the inward
normal is used. The normal is calculated by considering
the immediate vertices on both sides of the calculated
point. Thus, we get a zigzag path for the center of the
tool that is written out in a cutter location (CL) file. The
tool path generated contains a list of vertices that
contains the co-ordinates of the points. These paths are
then fed to the HLM machine for the generation of the
final shape of the model.
5. Experiments and illustrations
Preliminary experiments are carried out on theTransPulse Synergic MIG/MAG machine, with 12 mm
diameter ER70S-6 filler wire and shielding gas composi-
tion of 82% Ar+18% CO2, to fine-tune the required
weld process parameters to attain the optimized weld
bead geometry. Unlike the conventional weld deposi-
tion, the HLM process requires low heat input and low
weld penetration [29]; so the preliminary weld para-
meters are constrained to the low current range (40 to
130 A) of short circuit and globular metal transfer
modes only. The excessive remelting of the previously
deposited metal will disrupt the geometry of the earlier
formed layers as the large droplet size will contribute
more heat to the substrate and result in a more
pronounced finger-shaped penetration [30]. Further,
the excess residual heat due to the delayed solidification
results in large amounts of porosity, poor surface finish
and increased material flow.
On a Mild Steel base plate, 10 uniform weld layers are
deposited by 1.2 mm ER70S-6 Filler wire at 1000 mm/
min weld speed maintaining 10 mm stick out distance
with a zigzag weld path to build a 80 80 12mm3
rectangular block. The final deposited specimen is cross
sectioned at different lengths to determine the hardness
and microstructure. The hardness is measured on the
Rockwell hardness-testing machine for each individualdeposited weld layer as shown in Fig. 9. The cross-
sectional views of the deposited specimen showed no
sign of porosity presence in between the layers. The
microstructure of the specimen was seen through the
ESEM for the identification of the growth of the
dendrites. The heat-affected zone of the weld pool
varies with the amount of heat input into the deposited
layer and influences on the formation of martensite,
which alters the hardness of the deposited layer.
Martensite, a hard brittle form of steel, has extreme
ARTICLE IN PRESS
18
18.5
19
19.5
20
20.5
21
21.5
22
22.5
1 2 3 4 5 6 7 8 9 10
Layer Number
RockWellHardness
Hardness
Fig. 9. Variation of hardness with weld layer.
S. Akula, K.P. Karunakaran / Robotics and Computer-Integrated Manufacturing 22 (2006) 113123 119
7/29/2019 Hybrid layer
8/11
hardness and low ductility, and its formation is
controlled by decreasing the rate of cooling of the weld
bead (Figs. 10 and 11).
To predict the intermediate weld bead width and
height at various operating process parameters of wire
feed rate and weld speed, experiments are performed
based on the statistical optimizing techniques of
regressive analysis [32,33]. The region of exploration
for fitting the first-order model is (1.22.8) m/min ofwire
feed rate and (400800) mm/min of weld speed.
Controlling factors Levels
1 0 +1
Wire feed rate (m/min) 1.2 2.0 2.8
Weld speed (mm/min) 400 600 800
The collected response data are fitted in the first-order
model forthe weld bead width as
^yw 3:6425 1:09x1 0:72x2
and the reinforcement weld bead height as
^yh 1:18125 0:2875x1 0:2625x2,
where x1 is wire feed rate and x2 is weld speed.
Due to the consistence of the TransPulse Synergic
MIG/MAG welding controller, with the co-relation of
the above-derived equations the corresponding wire feed
rate and weld speed are estimated to build the welddeposition for various slice layer thicknesses in relation
to adaptive slicing [34] (Figs. 12 and 13).
6. Fabrication of HLM machine
In the implementation of the HLM process, the
following steps are involved in retrofitting:
fabrication of the low-cost three-axis manipulator
(details in Table 1);
mounting of the welding torch on the spindle head as
shown in the Fig. 14;
interfacing welding machine and the three-axis
manipulator so that the welding operations can be
initiated and stopped through the NC codes;
a fixture for cooling the substrate;
incorporation of shields so that the occasional spatter
does not affect the structure of the three-axis
manipulator.
ARTICLE IN PRESS
0
200
400
600
800
1000
1200
1400
1600
20 40 60 80 100 120
Diffraction Angle 2*theta (degrees)
ArbitraryUnit
Fig. 10. X-ray diffraction pattern of the deposited layer.
6.74
5.78
4.363.76
7.66
6.54
5.44.92
0
2
4
6
8
10
400 600 800 1000
Weld Speed
WeldBeadWidth
at 20 volt
at 21 volt
Fig. 12. Variation of weld speed with weld bead width.
2
1.4
1.2
1
2.2
1.6
1.4
1.2
0
0.5
1
1.5
2
2.5
400 600 800 1000
Weld Speed
WeldBeadHeight
at 20 volt
at 21 volt
Fig. 13. Variation of weld speed with weld bead height.
Fig. 11. ESEM image microstructure of the layer.
S. Akula, K.P. Karunakaran / Robotics and Computer-Integrated Manufacturing 22 (2006) 113123120
7/29/2019 Hybrid layer
9/11
With low investment, a three-axis manipulator was
fabricated for the HLM process as shown in Fig. 6. The
horizontal X, Y motions are attained by the movement
of the substrate table on the ball lead screw arrangement
and vertical Z motion is achieved by the movement of
the tool head. Each axis has its motion controlled by an
individual stepper motor in open-loop drive with rapid
and linear interpolations, such that all 3 axes can be
moved simultaneously. Initially, tool head was designed
to have the spindle motor and the face-milling cutter to
be on the same base plate for their simultaneous
movement. Later it was modified as shown in Fig. 14
to have a spline shaft arrangement for the power
transfer between the isolated geared motor that was
fixed to the frame of the HLM machine and the spindle
motor. During the vertical movement of tool head,
isolating the spindle motor from its tool head reduces
the net load on the stepper motor. Thus, the accuracy
and repeatability of the z-axis movement is enhanced
(Fig. 14).
Heat buildup due to the welding processes results in
partial malformation or collapse of the structure. A
cooling channel plate has been fixed to incorporate
effective heat control management. This plate is
mounted on the machine table and cold compressed
air is circulated through the duct. The substrate is
mounted on top of this while the weld deposition occurs.
The temperature variation within the deposition layerwith the severity of cooling influences the generation of
internal stresses and the resulting microstructure of the
deposited layer (Fig. 15).
To relieve these undesirable residual stresses, a
suitable heat treatment is performed using normalizing
and annealing processes. As these residual stresses are
unchecked, they may induce warping, loss of edge
tolerance and delaminating, thereby reducing the
strength and influence on the tool life.
The material homogeneity of the tools obtained with
this HLM process is between those of cast and machined
parts. Thus, this process is not suitable for making
forging dies where very high impact forces are
encountered. But the die used in injection molding,
die casting and sheet metal forming undergoes con-
siderably less fatigue loading during the operation,
so these tools can serve the purpose even without any
homogenization operation such as the HIP process.
Further, these die halves are free from overhanging
features, as they need to open and close in operation.
Building such dies and mold with free from re-entrant
profiles by this novel methodology will not require any
support structure, thus making the process more
attractive (Table 2).
ARTICLE IN PRESS
Table 1
Specifications of the low-cost PC-based three-axis manipulator
Traverse X400 mm, Y300 mm, Z300 mm
Accuracy on each axis 70.05 mm
Rapid speed 2500 mm/min (max)
Speed during interpolation 1000 m m/min (max)
Interpolations required Rapid and linear motions simultaneously on all three axesNumber of switching functions Eight controllable through NC program such as M codes
Lead screw type Ball lead screws on all three axes
Drive type Stepper motors in open loop
Kinematics X, Y motions by moving the table and Z by the tool head.
Structure Machined and fastened structure
Maximum load on the table 100 k g (the job being built)
Spindle 1 H P motor with gear reduction to give 200 r pm. Face mill is clamped through collet and draw bolt
Attachment for welding torch A pneumatically operated slide with 50mm traverse
Fig. 14. HLM machine with modified tool head.
S. Akula, K.P. Karunakaran / Robotics and Computer-Integrated Manufacturing 22 (2006) 113123 121
7/29/2019 Hybrid layer
10/11
7. Conclusions
Direct production of the metal part is unique among
current RP techniques. With the proposed and devel-
oped HLM process, the overall cycle time of tools and
dies can be developed much faster than the current
existing commercial RP systems. The HLM process can
be developed entirely as a new RP system or even
retrofit to the existing three-axis CNC machine, thus
minimizing the investment cost. Strength of the depos-
ited metal layer depends mainly on the availability of
suitable filler wires and all the desired material proper-
ties cannot be attained with the welding process. The
tools produced using this process may be inferior to
their conventional counterparts in composition and tool
life period but these will generate the final products as
accurately as any other tool. Flooded with competitors
and thronged by customer demands, manufacturing
industries find Direct Metal RP as a golden goose for
their new product development.
References
[1] Ashley S. Rapid prototyping systems. Mech Eng ASME
1991:3443.
[2] Kruth JP, Leu MC, Nakagawa T. Progress in additive manu-
facturing and rapid prototyping. Ann CRIP 1998;47(2):52539.
[3] Karapatis NP, Griethuysen JPS, Glardon R. Direct rapid tooling:
a re vie w of cu rren t re sear ch. Rapid Prot otyp ing J
1998;4(2):7789.
[4] Hopkinson N, Dickens P. Rapid prototyping for direct manu-
facture. Rapid Prototyping J 2001;7(4):197202.
[5] Fritz Klocke K, Wirtz H, Meiners W. Direct manufacturing of
metal prototypes and prototype tools. Solid freeform fabrication
proceedings, 1996. p. 1418.
[6] Merz R, Prinz FB, Ramaswami K, Terk M, Weiss LE. Shape
deposition manufacturing. Proceedings of solid freeform sympo-
sium, Austin, Texas, 1994. p. 18.
[7] Spencer JD, Dickens PM, Wykens CM. Rapid prototyping of
metal parts by three-dimensional welding. Proc. Inst Mech Eng
PartB, ImechE 1998;212:17582.
[8] Kovacevic R, Beardsley H. Process control of 3D welding as a
droplet-based rapid prototyping technique. Proceedings of solid
freeform symposium, Austin, Texas, 1998. p. 5764.
ARTICLE IN PRESS
Fig. 15. Fabrication of the connecting rod with the HLM process. (a) Deposited Weld Layer for Connecting Rod, (b) Face Milled weld deposited
Connecting Rod.
Table 2
Comparison of tool making using laser sintering and HLM process
Characteristic SLS and 3DP HLM
Principle Powder metallurgy (PM) Welding and millingwell-known processes
Density and strength Porous part (without compaction). Since it is not
totally steel, not very strong
Under stable operating conditions, density close
to 100% is possible. Strength depends only on the
availability of suitable filler wires which are
available in a variety of choices
Pos t-pro ce ssi ng Impr egnatio n with cop per i n a fu rnac e is re quir ed
which takes several hours
No post processing for density improvement.
However, Hot Iso-static Pressing (HIP) improves
fatigue strength
Accuracy Limited by particle and layer sizes Same as CNC machining
Slicing type Only uniform slicing of zeroth-order edge Adaptive and visible slicing is possible. The whole
die is a single visible slice
Overall cycle time Slower than HLM Much faster than SLS and 3DP
Safety Hazardous due to use of laser Not hazardous
Available as A complete and costly machine A retrofit or complete machine
S. Akula, K.P. Karunakaran / Robotics and Computer-Integrated Manufacturing 22 (2006) 113123122
7/29/2019 Hybrid layer
11/11
[9] Song YA, Park A, Jee H, Choi D, Shin, Bosung. 3D welding and
millinga direct approach for fabrication of injection molds.
Proceedings of solid freeform symposium, Austin, Texas, 1999.
p. 793800.
[10] Zhang YM, Li M, Chen Y, Male TA. Automatic system for weld
based rapid prototyping. Mechatronics 2002;12:3755.
[11] Sreenathbabu Akula, Karunakaran KP. Direct metallic rapid
prototyping: a decisive aid in new product development, in theproceedings of international conference on e-manufacturing: an
emerging need for 21st century world class enterprises held in
Bhopal, India, on 1719 November 2002. p. 26570.
[12] Jager PJ, Broek JJ, Vergeest JSM. A comparison between zero
and first order approximation algorithms for layered manufactur-
ing. Rapid Prototyping J 1997;3(4):1449.
[13] Sabourin E, Houser SA, Bohn JH. Adaptive slicing using stepwise
uniform refinement. Rapid Prototyping J 1996;2(4):206.
[14] Mukesh KA, Bourell B, David L, Beaman B, Joseph J.
Densification of selective laser sintered metal parts by hot
isostatic pressing. Solid freeform fabrication proceedings, The
University of Texas at Austin, 1994. p. 6573.
[15] Sreenathbabu Akula, Karunakaran KP. Hybrid Layered Manu-
facturing for Injection Molds and Dies at International Con-
ference on CAD, CAM, Robotics & Autonomous Factories(INCARF 2003), held at I.I.T Delhi, India, on August 1113,
2003.
[16] Pridham MS, Thomas G. Part fabrication using laser machining
and welding. Proceedings of solid freeform symposium, Austin,
Texas, 1993. p. 7480.
[17] Mani K, Kulkarni P, Dutta D. Region-based adaptive slicing.
Comput Aided Des 1999;31(2):31733.
[18] Xiuzhi Qu, Brent E, Stucker. STL-based finish machining of rapid
manufactured parts and tools. Solid freeform fabrication pro-
ceedings, 2001. p. 30412.
[19] Zhou ZD, Zhou JD, Chen YP, Ong SK, Nee AYC. Geometric
simulation of NC machining based on STL models. CIRP Ann
Manuf Technol 2003;52(1):12934.
[20] Dolenc A, Makela I. Slicing procedures for layered manufactur-
ing techniques. Comput Aided Des 1994;26(2):11926.
[21] Jamieson R, Hacker H. Direct slicing of CAD models for rapid
prototyping. Rapid Prototyping J 1995;1(2):412.
[22] Ganesan M, Fadel GM. Hollowing rapid prototyping parts using
offsetting techniques. Proceedings of the fifth international
conference on rapid prototyping, Dayton, OH, June 1994.
[23] Kulkarni P, Dutta D. An accurate slicing procedure for layered
manufacturing. Comput Aided Des 1996;28(9):68397.
[24] Tyberg J, Bohn JH. Local adaptive slicing. Rapid Prototyping J1998;4(3):11827.
[25] Held M. On the computational geometry of pocket machining.
New York: Springer; 1991.
[26] Held M. Voronoi diagrams and offset curves of curvilinear
polygons. Comput Aided Des 1998;30(4):287300.
[27] Rajan VT, Srinivas V, Tarabini KA. The optimal zig-zag
direction for filling a two-dimensional region. Rapid Prototyping
J 2001;7(5):23140.
[28] Hope RL, Roth RN, Jocabs PA. Adaptive slicing with sloping
layer surfaces. Rapid Prototyping J 1997;3:8998.
[29] Kmecko I, Hu D, Kovacevic R. Controlling heat input, spatter
and weld penetration in GMAWelding for solid freeform
fabrication. Proceedings of solid freeform symposium, Austin,
Texas, 1999. p. 73542.
[30] Kim YS, Eagar TW. Metal transfer in pulsed current gasmetal arc welding. Welding research supplement, July, 1993.
p. 279s87s.
[32] Murray PE. Selecting parameters for GMAW using dimensional
analysis. Welding J 2002:125s31s.
[33] Montgomery DC. Design and analysis of experiments. 3rd ed.
Singapore: Wiley; 1991.
[34] Sreenathbabu Akula, Karunakaran KP. Application of Taguchi
methods in hybrid layered manufacturing for the optimization of
the process parameters. Proceedings of the 26th RP symposium of
Japan, June 15th 2004, Tokyo. p. 13743.
Further Reading
[31] Gas Metal Arc Welding, Welding Handbook AWS, 1996.
ARTICLE IN PRESS
S. Akula, K.P. Karunakaran / Robotics and Computer-Integrated Manufacturing 22 (2006) 113123 123