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    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

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    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).

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    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

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    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.

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    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.

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    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.

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    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.

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    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.

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    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.

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    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.

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    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.

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    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

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    Under stable operating conditions, density close

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    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

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    Further Reading

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    ARTICLE IN PRESS

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