Spatter Reduction Report

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    PROJECT REPORT

    MARUTI SUZUKI INDIA LIMITED

    SPATTER REDUCTION

    Submitted by

    ABHISHEK MITTAL

    Roll No. - 101108003

    Under the Guidance of

    Mr. Supreet Bhullar Arun K Kumar

    Associate Professor Deputy Manager(L-12)

    Department of Mechanical EngineeringTHAPAR UNIVERSITY, PATIALA

    June 2014

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    DECLARATION

    I hereby declare that the project work entitled SPATTER REDUCTION is an authentic

    record of my own work carried out at MARUTI SUZUKI INDIA LIMITED as requirements

    of six months project semester for the award of degree of B.E. (Mechanical Engineering),

    Thapar University, Patiala, under the guidance of Mr. Supreet Bhullar and ER. Arun Kumar ,

    during January to June, 2014.

    ABHISHEK MITTAL

    101108003

    Date: ___________________

    Certified that the above statement made by the student is correct to the best of our knowledge

    and belief.

    Mr. Supreet Bhullar Arun Kumar K

    Associate Professor Deputy Manager(L-12)

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    ACKNOWLEDGEMENT

    I take this opportunity to express my profound gratitude and deep regards tomy guide Mr. Arun Kumar K.(Deputy Manager, Weld shop -3 MSIL), forhis exemplary guidance, monitoring and constant encouragement throughoutthe course of this project

    The blessing, help and guidance given by him time to time shall carry me along way in the journey of life on which I am about to embark.

    I also take this opportunity to express a deep sense of gratitude to Mr.Gobinath T(Assistant Manager, Weld shop - 3) and Mr.J.Edison (SeniorManager Process Engineering cell MSIL), for his cordial support, valuableinformation and guidance, which helped me in completing this task through

    various stages.

    I am obliged to staff members of MSIL for the valuable informationprovided by them in their respective fields. I am grateful for theircooperation during the period of my assignment.

    ABHISHEK MITTAL

    101108003

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    CONTENTS

    Declaration 2

    Acknowledgement 3

    Summary 5

    About MSIL 6

    Weld shop 24

    Spatter Reduction 25

    Procedure 29

    Implementation Training Module 36

    Weld Information Collection System 41

    Spot checking 52

    Parameter Determination 55

    Automation System 70

    Result 77

    conclusion 78

    References 79

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    SUMMARY

    Reduction of spatter in Ertiga line by maintain proper production process such as avoidingimproper face cutting, tip alignment, zero touch up and keeping parameters such as weld

    time, current and pressure to acceptable limit. Spatter causes huge monetary, productivity,quality losses.

    The project involves parameter determination which is a dominant factor in weld spatter.Also a concept was developed to automate the spatter reduction activities which were earlier

    done manually.

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    Maruti Suzuki India Limited (MSIL) is engaged in the business ofmanufacture, purchase and sale of motor vehicles, automobile components

    and spare parts (automobiles).

    The other activities of the Company consist of facilitation of pre-ownedcar sales, fleet management and car financing. The Companys portfolio

    includes the Maruti 800, Alto 800, Alto K10, A-star, Estilo, WagonR, Ritz,

    Swift, Swift DZire, SX4, Omni, Eeco, Kizashi, Grand Vitara, Gypsy,

    Ertiga and Stingray.

    The Companys services include Finance, Insurance, Maruti Genuine

    Accessories, Maruti Genuine Parts, Maruti Driving School and Autocard.The Companys subsidiaries include Maruti Insurance Business Agency

    Limited, Maruti Insurance Distribution Services Limited, True Value

    Solutions Limited, Maruti Insurance Agency Network Limited, Maruti

    Insurance Agency Solutions Limited, Maruti Insurance Agency Services

    Limited, Maruti Insurance Logistic Limited and Maruti Insurance Broker

    Limited.

    Listed in SENSEX ,BSE:532500 AND NSE:MARUTI

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    Earlier known as Maruti Udyog Limited, it was incorporated as a Public sector company on

    24 Feb,1981with the following objectives: -

    Modernization of Indian automobile industry.

    Production of fuel-efficient vehicles to conserve scarce resources.

    Production of large number of vehicles which was necessary for economic growth.

    Transfer of Technology

    Every minute two vehicles roll out of the Maruti Plant. It is therefore imperative that the

    transfer of contemporary technology from our partner Suzuki is a smooth process. Great

    stress is laid on training and motivating the people who man and maintain the equipment,

    since the best equipment alone cannot guarantee high quality and productivity. From the

    beginning it was a conscious decision to send people to Suzuki Motor Corporation for on-the-

    job training for line technicians, supervisors and engineers. This helps them to imbibe the

    culture in a way that merely transferring technology through documents can never replicate.At present 20% of our workforce have been trained under this program.

    Maruti Code Of Conduct

    A code has been developed to assist all the employees in their dealings with those with whom

    the company does business i.e., customers, dealers, and suppliers and with each other. The

    code is not a subst itute for the judgment and discretion of individual employee in day-to-day

    work. Neither is it a replacement for company policies, which will continue to apply. The

    code contains advice for making decisions in situations where there are no precedents, so that

    a common set of norms of business behavior can grow throughout the company.

    Following are the important points:

    Integrity

    Trust

    Image

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    Consumer Orientation

    Ethics

    Positive Attitude

    MSILS GURGAON PLANT

    The manufacturing plant, located about 25-km south of New Delhi in Gurgaon, has an

    installed capacity of 5,00,000 units per annum. The total area of the plant is 12,02,256 m2

    with a total covered area of 2,95,293 m2. The average daily production is around 2500

    vehicles a day.

    The whole production facility has been divided into 3 plants: -

    1. Plant I (M800, Omni, Eeco, Ritz, Wagnon R)

    2. Plant II ( Zen ESTILO, Swift Dzire)3. Plant III (Alto)

    The other activities include research & development and utilities (captive power plant, water

    and effluent treatment plant, compressor house, boiler house, air washers and incinerator

    facilities.

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    `Technician

    Supervisor

    Executive

    Asst. Manager

    Deputy Manager

    Manager

    Department Manager(DPM)

    Deputy Divisional

    Manager(DDVM)

    Divisional Manager(DVM)

    Director

    Joint Managing Director(JMD)

    Managing Director (MD)

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    The Various divisions in Maruti Udyog Limited are:

    Marketing & Sales

    Spares

    Engineering

    Quality Assurance

    Services

    Production

    Production Engineering

    Materials

    Information Services

    Finance

    Personnel and Administration

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    Modern manufacturing includes all intermediate processes required for the production and

    integration of a product's components. Some industries, such

    assemiconductor andsteel manufacturers use the termfabricationinstead.

    MARUTI SUZUKI MANUFACTURING PROCESS

    Blanking is the cutting of a sheet metal part along a closed contour in one step. The piece cut

    out is called a blank and may be further processed. Many blanks are often continuously cutout of a sheet or strip. Blanking will waste a certain amount of material. When designing a

    sheet metal blanking process, the geometry of the blanks should be nestled as efficiently aspossible to minimize material waste. A distinction should be made between the two sheetmetal cutting processes of blanking and punching, since essentially they are the same process.

    In punching, the piece cut out is waste. In blanking, the piece cut out is the work and is kept.

    It is possible to employ fine blanking for many sheet metal cutting operations, particularlythose involving lower total sheet thickness. Fine blanking is an advanced precision

    pressworking process that can create cuts having close tolerances and straight smooth edges,without shaving or other secondary processes.

    A press forces a pressure pad on the sheet metal, holding the work tightly between the lower

    die and the pressure pad. Close to, outside and all around the edge of the cut, a v-shaped ring

    projecting from the bottom of the pressure pad impinges the work piece. This further securesthe work from movement and restricts metal flow. The cutting punch for this operation has a

    http://en.wikipedia.org/wiki/Fabrication_(semiconductor)http://en.wikipedia.org/wiki/Fabrication_(metal)http://en.wikipedia.org/wiki/Fabrication_(metal)http://en.wikipedia.org/wiki/Fabrication_(semiconductor)
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    very small clearance with the lower die, usually 1%. As pressure is applied to the work, thepunch cuts through the metal at a s low rate. Simultaneously, another punch app lies force to

    the other side of the sheet in the opposite direction. The secondary punch delivers less forcethan the cutting punch. Its purpose is to help with the cut and to prevent warping of the bank,

    a common problem in sheet metal blanking operations. The force of the support punch is less

    than and in the opposite direction of the cutting punch, therefore the summation of bothvectors indicates that the total force, (and hence the movement), will be in the direction

    dictated by the cutting punch.

    The press shop can be regarded as the starting point of car manufacturing process. Centrally

    located between weld1, weld2 and weld3 supplies components to all the three plants.

    The press shop has a batch production system whereas the plants have a line production

    system. The press shop maintains an inventory of at least two days. The weld shops as per

    their requirements pick the finished body parts. These may be divided as A, B & C. A

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    components are large outer components e.g. roof, door panels, front hood etc. These

    components are manufactured in the press shop at maruti due to design secrecy and huge

    investment requirements. B & C components are manufactured by joint ventures or

    bought from vendors.

    The press shop can be explained under following headings

    Raw Material

    Blanking Line

    Stamping Line

    RAW MATERIAL

    The raw material is in the form of cold rolled steel coils. It is specified in terms of steel grade

    and width of coil required. The coils weigh about 15000kg.

    BLANKING LINE

    There are two blanking lines; ROSL (Rotary Oscillatory Shear Line) for rectangular sheets

    and the other employing die cutting, for irregular shapes.

    The rectangular sheets are obtained on ROSL while dies are employed to obtain the required

    shape sheets.

    The sequences of operations on the blanking line are as following: -

    Uncoiling

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    Cleaning

    Leveling

    Measuring

    Shearing/cutting

    Piling/stacking

    STAMPING LINE

    There are six presses of capacity varying from 1500 tones to 4000 tones.

    Of these five are transfer presses and one is a semi-automatic press line, wherein the

    loading is manual. The dies can be changed to obtain different body components. The

    sequence of operations is as following: -

    Destacking

    Cleaning

    Drawing

    Trimming

    Bending

    Punching

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    a "filler metal" into the joint to act as a binding agent. Other methods rely on pressure

    to bind metal together, and still others use a combination of both heat andpressure.

    Unlike soldering and brazing, where the metal pieces being joined remain unaltered,

    the process of welding always changes the work pieces.

    This is restricted area and I could not get permission to go inside. A single particle of dust if

    embedded onto the body the paint would chip off. Hence the entry of non-factory personnel isrestricted in order to avoid the entry of dust particles.

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    However the information regarding the process outline in the paint shop gathered from other

    sources is as following: -

    I. Pre-treatment:The body is thoroughly washed to remove dirt and oil scales.

    II. ED coat:This is done by electric deposition method. After applying the ED coat body

    is baked in ovens.

    III.Intermediate coat:This is done by spray painting method. After applying the coat,

    the body is dried in the oven.

    IV.Final coat: For metallic coating, double coats are applied and aluminum flakes

    provide the shine to metallic paint. This is also done by spray painting

    method. The PBOK, i.e. Paint Body OK is sent to the assembly shop.

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    Painting process I/C

    & Top Coat painting

    Painting process Final

    Inspection

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    The assembly shop receives PB-OK i.e. paint body OK from the paint shop. Here the body is

    loaded on a conveyor on jigs. As the conveyor moves the fitments are made on the body at

    various stations.The sequencing of models is done by PLC i.e. Program Logic Control. In Plant-1 there are

    separate assembly lines for each model as compared toPlant-2which has only one U type

    plant layout for different models. Altering the speed of the conveyor can alter the capacity of

    shop. The Plant-3 conveyor runs at 2.7m/min. The conveyor belt can run at a maximum speed

    of 4 m/min.

    Assembly shops havecontinuous production system. The assembly line can be further

    subdivided as following: -

    Trim

    Chassis

    Final

    TRIM

    Tr im can be further subdivided as fol lowing: -

    1. Trim 1

    2. Trim 2

    3. Trim 3

    Trim 1:This is the beginning of the assembly line conveyor. Here amongst the first tasks

    done is attaching the hydraulic supporters for the boot. The assembly line check sheet is put

    inside the body.

    .

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    Trim 2:It starts with the head light fitting. Other operations done here are vacuum booster/

    brake master cylinder fitment, seat belts, fuse box, wiper sprayer and motor, accelerator,

    clutch, brake pedals, door glasses and a/c panel fitment. Trim 2 ends with the fitment of the

    instrument panel, which is received from an instrument panel, sub assembly. This sub

    assembly involves the fitting of the speedometer console, ashtray and stereo system. Besides

    all these ignition coil for Car800.

    Trim 3:The fittings done here are rear inside cover for boot, back door glass and windshield,

    quarter glasses and connecting pipe between fuel lid and fuel tank. Car800's front coil spring

    is also fitted here. Steering gear is mounted. For comedienne application on the windshield,

    Motoman robots are employed.

    There is a process check at the end of trim line wherein the points in the check sheet are

    verified and marked ok.

    CHASSIS

    The chassis receives a trim up body. Here underbody fitments are made; hence body is loaded

    on overhead jigs. Chassis can be subdivided as following: -

    1. Chassis 1

    2. Chassis 2

    Chassis 1:Various fitments made here are rear shock absorbers, brake pipes, front coil spring

    with knuckle, steering wheel, tie rods, rear suspension, fuel pipes, fuel tank and rear brake

    drum. There is a knuckle sub assembly that feeds the line with knuckles for the front

    suspension system. On front wheels disc brakes are used whereas on rear wheels drum

    brakes are used. There is a process check at the end of chassis 1.

    Chassis 2:The various fitments made here exhaust system (silencer and catalytic converter),

    engine cum transmission case assembly, gear shift rod, front and rear bumpers, stabilizer bars

    and tyres. Radiator of Car800 is fitted here. The tie rod and drive shafts are connected to the

    knuckle to complete the front suspension system. There is a process check at the end of

    chassis 2.

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    FINAL

    Since all the fitments have been made, we will refer the body as vehicle from now onwards.

    The vehicle is loaded on the conveyor. It can be further subdivided as: -

    Final 1

    Final 2

    Final 1: The fitments made here are Spare wheel cover, ID plate, scuff, seats, roof trim and

    carpet, boot carpet, battery and air cleaner. Clutch cable and parking brake connections are

    made. Brakes are evacuated and brake oil is filled. Coolant is also filled.

    Final 2:Five liters of petrol is filled in the vehicle. A/C evacuation and charging is done

    here, the refrigerant used here is R134a (400 gm +- 50). Door gaps are checked and adjusted,

    front grill of Car800 is fitted.

    There is a process check at the end of this line. Here the vehicle is checked for the following

    as per the check sheet: -

    Final-Engine room

    Final-Cabin

    Final-Pit

    Final-Side body

    Final-Engine room:Engine oil, brake oil and coolant level. Electrical connections, viz.

    ignition coil to distributor, battery terminals, and wiper motor connections. Air cleaner

    fitment, radiator hoses &clamp tightening, fuel hoses clamping, radiator mtg. bolt fitments,

    clutch cable connection, accelerator pedal play &choke cable play are checked.

    Final-Cabin: All lamps viz. head lamp high/low, parking lamp, cabin lamp, wiper water

    spray, reverse lamp, ac cooling, blower etc. are checked here.

    Mirror view, clutch pedal play and brake pedal play & operation of parking

    levers are checked here. Steering shaft column and shaft nuts and bolts are tightened.

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    Final-pit: The vehicle is checked for brake oil leakage, coolant leakage, fuel leakage etc.

    And these are marked OK on the check sheet.

    Final-side body:All door fitments checked. Spare wheel fitment and rear seat fitments are

    checked. Seat adjustments are checked.

    The vehicle is said to be AB-OK now. It is sent to vehicle inspection dept.

    The assembly check sheet is removed. A new check sheet is added to vehicle carrying AB-

    OK stamps. The vehicle is called FC-ON i.e. final check on.

    Work-pieces are held together under pressure exerted by electrodes. Typically the

    sheets are in the 0.5 to 3 mm (0.020 to 0.118 in) thickness range.

    The process uses two shapedcopperalloyelectrodesto concentrate welding current

    into a small "spot" and to simultaneously clamp the sheets together.

    Forcing a large current through the spot will melt the metal and form the weld. The

    attractive feature of spot welding is that a lot of energy can be delivered to the spot in

    a very short time (approximately 10 - 100 milliseconds).

    http://en.wikipedia.org/wiki/Copperhttp://en.wikipedia.org/wiki/Copperhttp://en.wikipedia.org/wiki/Alloyhttp://en.wikipedia.org/wiki/Alloyhttp://en.wikipedia.org/wiki/Electrodehttp://en.wikipedia.org/wiki/Electrodehttp://en.wikipedia.org/wiki/Electrodehttp://en.wikipedia.org/wiki/Electrodehttp://en.wikipedia.org/wiki/Alloyhttp://en.wikipedia.org/wiki/Copper
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    That permits the welding to occur without excessive heating of the remainder of the

    sheet.

    The amount of heat (energy) delivered to the spot is determined by the resistance

    between the electrodes and the magnitude and duration of the current.

    The amount of energy is chosen to match the sheet's material properties, its thickness,

    and type of electrodes.

    Applying too little energy will not melt the metal or will make a poor weld. Applying

    too much energy will melt too much metal, eject molten material, and make a hole

    rather than a weld.

    Another feature of spot welding is that the energy delivered to the spot can be

    controlled to produce reliable welds.

    Weld spatter occurs when small liquid molten metal particles are expelled from thesurface of the materials while welding, due to pressure and heat.

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    WHY WE NEED TO CONTROL SPATTER ? ??

    Deterioration of quality due to metal dust and burrs caused by spatter

    Spatter can leave marks and also makes spots weak which degrades quality of

    production.

    Damage of costly PLS , Limit switches , and other sensors in automation line.

    Lots of high cost equipments are installed in automation line,spatter can hinder in the

    working of these instruments and in extreme case can lead to failure of these

    instruments also.

    Increased down time due breakdowns related to LS & Sensor damage

    For company like MSIL ,completing their production targets in time is most important

    requirement, but spatter can lead to breakdown ,so it is important to control spatter.

    Health and safety implications for employees

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    For MSIL safety comes first and for this we need to control spatter as it can harm eyesand skin .

    Higher electrical power usage

    Spatter can be because of wrong parameters like current. Generating more current on spotthen required means improper usage of costly resources.

    FFaaccttoo rrss CCoo nnttrriibbuuttee ttoowwee llddssppaattttee rr!!

    Tip alignment and mismatch problem

    One of the most common factor that contributes to spatter, mismatch of tip of guns i.e

    movable and stationary gun.Abnormal Zero touchup

    Absence of zero touch between body to be welded and stationary gun can make way forspatter because of air gap.

    Abnormal dressing condition

    Improper dressing or grinding can also produce spatter because it leads to improper dressingtip.

    Abnormal gun pressure and welding current.

    Too low gun pressure or to high current contributes to spatter.Improper location of weld spot

    Another factor that contributes due to incorrect location of weld spot ,which can be because

    of overlapping of spots etc.

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    1stStepis collect initial data, follow these steps:

    a. Collect the data at standard condition

    Use standard format for this purpose.

    2ndStepis Tip alignment & matching Checking and correction of

    Shank alignment

    Cap Tip alignment

    Tip matching

    * Tip alignment and matching to be done in new tip, after dressing* If wear down value is NG then gun mastering to be done

    3rd

    Stepis Welding Current & pressure calibration

    Checking of welding current output vs Input ( by weld checker & Turn ratio setting)

    Pressure calibration (by pressure checker )

    4thStep is Dresser Check

    Dresser mounting check

    Dresser cutter and holder condition check

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    Air blow and cutter rotation direction check

    Tip condition after Tip Dressing

    5

    th

    Step is Zero touch up Checking and correction of

    - Zero touch up with body surface

    6thStep is pressure setting correction

    Checking and correction of

    - Weld pressure as per standard

    7th

    Stepis Dressing time and dressing frequency setting

    Checking and correction of

    - Dressing frequency

    - Dressing timeOther than the above procedures following factors also affect thewelding condition:

    Excessive dust on the welding surface

    Gap and mismatch of comp. in jigs

    Vibrations in Servo gun & Robot

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    The aim of the project is to reduce spatter and improve welding

    process. Spatter free weld shop was motto of this project.

    Reduced power consumption

    Better weld quality and less rework

    Reduced maintenance costs

    Safer and cleaner environment

    Lower consumable costs

    Increased production up-time

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    A team was formed including expertise, line supervisor,summer

    trainee. A proper checksheet was designed to record daily spatterdata. The project started with aim of reducing spatter in YL8 line

    .During initial data collection spatter percentage was found out to be

    42%which was way above acceptable level.A proper procedure to control spatter was followed as discussedabove and the results obtained were commendable. The spatter

    percentage of Left side body was reduced from 40%to 5%.

    A view of spatter control checksheet can be seen below which is

    updated for each and every robot in welding shop and stepwisesequence was followed to achieve desired results.

    40

    22

    5

    0

    5

    10

    15

    20

    25

    3035

    40

    45

    W1 Jan 14 W2 Jan 14 W3 Jan 14 W4 Jan 14

    S

    p

    a

    t

    t

    e

    r

    %

    Period

    YL8 Ertiga - LH Side body Spatter

    control progress

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    And now after 4 monthsthe current spatter and the difference thathas been made can be seen in below bar graph:

    0

    5

    10

    15

    20

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    30

    35

    40

    S

    P

    A

    T

    T

    E

    R

    %

    YL8 LINE SPATTER STATUS AS ON 28.04.2014

    YL8 Line Feb'14

    YL8 Line Mar'14

    YL8 Line Apr'14

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    A standardized process for recording data was formulated which

    includes summary sheet of a particular area, supervisor check sheet,monthly data graph which is updated on regular basis. It helps us to

    analyze spatter data of a particular area and decide next course ofaction. Given below are the examples of data collection sheets to give

    the insight of how things work.

    Monthly Spatter status update sheet which give us the monthly

    spatter status.

    Individual robot wise check sheet updated on regular basis to

    know the current spatter status of particular robot.(Supervisor

    check sheet.)

    40

    6.6 9 6

    0

    5

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    40

    45

    Jan'14 Feb'14 March'14 April'14

    S

    P

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    %

    Period

    YL8 LSB Line Spatter Status

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    Area wise Summary sheet updated on regular basis :

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    Zero touch up and dressing training module was made for line superviser and workers.

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    Below is the step by step instruction for Fanuc robot to conduct zero touch up procedure.

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    WELD INFORMATION CONTROL SYSTEM

    INTRODUCTION

    As we know, the spots of a car are the most prcised work done on a car as their failure can

    cause accident. So, the company prefers to check the spots of car as it directly refer us to the

    company quality. But, it was not possible for the company to check the spots of every car as

    it was a very time consumable process as the processes done to check the spots were

    hammering test and peeling test. Till now, Maruti Suzuki India Limited was checking the

    spots of every export car and every 10th import car. But this does not give assurance to the

    customer for the best quality car as there was no tool for analysis of weld spot quality. So,

    there was a need to implement a method which would help the company in providing the best

    quality car. Due to this reason, weld information control system came to being in use.

    WELD INFORMATION CONTROL SYSTEM

    Weld information control system is a non-destructive testing technique to check the spots. In

    this technique, a spot id is given to every spot of the car. The datas of welding parameters

    are noted. These data have been fed to the PLC (programmable logic controller). IT

    department has implemented a server which would be directly linked with the PLC. PLC

    provides a graphical characteristic of every spot in computer screen with the help of server

    from which we could ensure defective spots on line. Also, the robot line would stop in which

    problem has occurred i.e. if the spots does not have the same characteristics as provided to

    the PLC, the robot would stop working itself and show faults on computer screen. So that, we

    can correct the spot by taking counter measure. Also, this technique will help us in having a

    control on NG welding flow.

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    NG Welding Flow

    NG welding flow occurs at a point where the robot is not able to weld the spot correctly i.e.

    the weld does not took properly due to following reasons:-

    a) Spatter control

    b) Spot Miss

    c) Gun alignment NG

    d) Tip / Tip Dressing NG

    e) Half spot

    f) Spot out of position

    g) Gun shunting

    h) Part deformation (part mismatch)

    W.I.C.S. FUNCTIONALITY

    Prevents NG Welding Flow

    Accurate Detection of Faults

    a) Spatter controlb) Spot Miss

    c) Gun alignment NG

    d) Tip / Tip Dressing NG

    e) Half spot

    f) Spot out of position

    g) Gun shunting

    h) Part deformation (part mismatch)

    Analysis of every weld spot

    Storage of weld spot parameters (upto 10 years)

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    W.I.C.S. METHODOLOGY

    The methodology on which W.I.C.S. depends is to study about the resistance waves as the

    reason for the spot failure could be known by this methodology.

    RESISTANCE WAVES

    Resistance waves are the graphical representation between resistance values and the weld

    time to show that the nugget formed is absolutely correct.

    Fig. 3.2. Principle of Resistance Waves

    As we can see from the above figure 3.2, the resistance value first decreases but as the temp.

    of base metal is raised the resistance value climb up and form a nugget and as the nugget

    expansion takes place with the increase in electrical path, the resistance value again decline.

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    BENEFITS FOR OBSERVING RESISTANCE WAVES

    Resistance wave profile is full spot welding, white body check.

    Detect the abnormal conditions early. Prevent NG Welding Flow.

    RESULTS OBTAINED BY OBSERVING RESISTANCE WAVES

    By observing the resistance waves, we could get to know the various methods because of

    which the NG Welding Flow occurs.

    1. Fault due to get out of parts position.

    Fig. 3.3. Fault seen due to get out of parts position

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    From the above fig. 3.3, we can clearly see that the nugget formation takes place at any other

    position than required.

    2. Fault due to bend parts.

    Fig. 3.4. Fault seen due to bend parts

    From the above fig. 3.4, we can clearly see that the nugget formation does not took place

    correctly as the parts in which the spot was to be applied was bent.

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    3. Fault due to get out of position.

    Fig. 3.5. Fault due to get out of position seen

    From the above fig. 3.5, we can clearly see that the nugget formation was formed slightlyside from its position due to which spot was not formed as required.

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    FAULTS RELATED TO RESISTANCE WAVES

    E79 Resist wave fault

    Fault occurs due to low quantity of heat, Tip diameter expansion, Lack or 2sets of work, Shift

    of weld position, Gun touch, terrible expulsion etc.

    Fig. 3.6. Fault of E79 resistance waves

    -Reset possible at reset box

    -Be cautious that when same control no. and same condition has been used continuously,

    judgment will not be done.

    NG body dont stop, even if no check and reset.

    When you returns weld points before more than 1 weld point by manual operation and you

    re-welded the weld points, it is possibility existence to stop by fault again.

    E85 Wave Resist Frequent

    Fault occurs due to tip dress, etc.

    -Timers output E85, when weld points more than thresholds of a warning level occurred

    frequently in res. decrease width or aver. res.

    -Reset possible in reset box

    E80 High Resistance

    Faults occur due to dust between the tip, power cable break etc.

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    Fig. 3.7. Fault of E80 high resistance waves

    -Timers output E80 when it detect resistance value ahead of a threshold of high resistance

    and it doesnt send weld current according to the setting value.

    -Discontinue the power supply at the detection of the fault

    - Measures are the basically same as low current fault.

    - We can reset the fault at a reset box, but it occurs again till the fault state is removed

    GRAPHICAL REPRESENTATION OF RESISTANCE WAVES

    Fig. 3.8, shows the graphical representation of resistance values at the time of welding.

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    Fig. 3.8. Graphical representation of resistance values

    This representation shows us the difference in the resistance decreasing width. This is shownby the line arrays of red, ye llow and blue colour in above fig.

    METHOD FOR OBSERVING RESISTANCE WAVEFORM

    To measure the transition of resistance value in every 0.5 cycle in welding, we have to

    calculate the parameter 1 to 4 and supervise them. The parameter to be calculated are as

    follows:-

    1. Resistance width decrease: - Max. resistance valuefinal resistance value

    2. Average resistance value:- Average of resistance value between 2.5cyc and weld time

    (setting time) -0.5cyc

    3. 3.Max resistance value:- Max value between setting time and weld time (setting time)

    -1.5cyc

    4. Final resistance value:- Resistance Value of weld time (setting time) -0.5cyc

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    Fig. 3.9 Resistance waveform

    SETTING OF RESISTANCE LIMIT

    Resistance limits refers us to a position after which alarm would rang. Resistance limits are

    classified in two levels: -

    1. Alarm Level: - When the nugget formation does not take properly, limit of alarm level

    is reached and the alarm rang so that the worker or engineer could take the counter

    measure.

    2. Fault level: - When the engineer or worker does not take counter measure after the

    alarm, then the line would automatically spot.

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    PROBLEMS OCCURING IN OBSERVATION

    There is a case when there is not a change of resistance. In this case, only the thin

    sheet side is weld NG on sheet combination such as thin- thick-thick sheets and in the

    case of sheet combination of thin-thin sheets. Therefore, there is the case that NG

    points cannot stop.

    Whether fault stops or not depend on a limit setting. Misjudgment occur a lot of

    times, when limit setting is too rigorous. But it cannot detect weld NG, when limit

    setting is too indulgent.

    Now, we set limits from average and unevenness of the present data which WICS

    system collect.

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    WELD SPOT CHECKING PROCESS STANDARDIZATION

    Maruti Operation Standard Inspection

    MOS I is known as Maruti Operation Standard Inspection sheet in which a list of all the spots

    are made and their robots are mentioned which apply these spots. Cycles are divided

    according to the application of spots. This sheet has a full spot detail of a car and the copy of

    every sheet is listed in the file on the line so that any engineer could go on the line and with

    this sheet could know about the inspection of this spot. The sheet is divided according to

    main body, main body pit, white body, cowl box, etc. and their cycles.

    DESCRIPTION OF MOS I

    The first thing that an engineer should know in welding department is the layout of

    department.

    He should know that which robot is working on which car.

    He should know which spots can be checked and which cannot be checked.

    He should know how many men are needed for checking the spots in a given

    component.

    For this, MOS I has been made so that the engineer have a list of all the spots being

    implemented on the components of the car.

    OBJECTIVES OF MOS I

    1. To mark the spots with different colours of different robots working on the

    component.

    2. To mark the G.A. spots and Maru - A spots of the component.

    3. To mark the cycle so that we could know how many men are needed for checking the

    spots? No. of cycles is equal to no. of men needed to check the spots.

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    4. To know how many robots are doing welding in a given component and how many

    spots are there in the given component.

    METHODOLOGY ADOPTED

    A MOS I sheet was made in which the picture of component with the spots was

    printed.

    The robots which are applying those spots in a given component were noted down

    along with their spots.

    Maru- A spots and G.A. spots were seen and marked on it.

    The men working on a given component to check the spots were noted and cycles

    were made according to their work.

    Modified MOS I of Main body checked at white body area

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    CONCLUSIONS

    Easy for engineer to trace back the broken spot robot

    Easy to find out the component details with the help of index.

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    PARAMETER DETERMINATION

    Parameters such as tip pressure, weld current, squeeze time and weld time affects weldquality and expulsions. Low pressure, high current and weld time were found to be main

    reasons for weld expulsions.

    METHODOLOGY

    Stage 1 - calculating pressure at particular current, time, hold time, sheet thickness ratio,material

    stage 2 - determining current and weld time combination through lobe diagram

    stage 3 - verifying by peel test nugget size,depth, shear strength

    stage 4 - spot sample

    PRESSURE CALCULATION

    Expulsion in welding is determined by many factors involving electrical, thermal,metallurgical, and mechanical processes.

    Although there are many complicated causes of expulsion, its basic process can be describedby the interaction between the forces from the liquid nugget and its surrounding solidcontainment. Major forces acting on a weldment during welding are illustrated in Fig. 3.

    They include the squeezing force provided by the electrodes (FE,applied) and the force fromthe liquid nugget (FN) onto its solid containment, which is generated by the pressure (P) in

    the molten metal and a compressive force between the workpieces. There is also a resistanceto sheet separation provided by solid diffusion (corona bonding) at the faying interface. Thisforce is usually much smaller than the others and can be neglected in the analysis, as this

    model considers extreme expulsion conditions only.

    Expulsion occurs when the force from the liquid nugget (FN) onto the solid containment

    equals or exceeds the effective electrode force (FE), i.e., FN FE.

    In practice, the applied electrode force is rarely collinear with the total force from the liquid

    nugget because of complications in electrode geometry such as wearing, electrode alignment,and part fitup. Therefore, the applied electrode force, in many cases, is not the same as theone used to contain the liquid nugget from expulsion. The effective electrode force is

    introduced in this situation to accurately represent the force used to suppress the force fromthe liquid nugget.

    EVALUATION OF EFFECTIVE ELECTRODE FORCE

    An effective electrode force, which is usually a portion of the total applied electrode force, isused to balance the force from the liquid nugget.

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    FE,appliedis the applied electrode force, FNis the total force from the liquid nugget against thesolid containment, and Fxis a force imposed by the other workpiece. FEis the effective

    electrode force, which will be explained in the following. In Fig. 5, d is the distance betweenthe total nugget force and the electrode force; r is the distance between FNand the edge of the

    nugget (it is the radius in the case of a round weld); x is the distance between force FxandFE,applied. Moment equilibrium with respect to the acting point of Fxproduces the following

    relationship between FE,appliedand FN:

    FE,appliedx = FN (d + X)

    An offset between the applied electrode force and that from the

    nugget, which is created by an angular misalignment of electrodes.

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    Before metal melts, x = 0 because FN= 0, and FE,appliedand Fxhave to be collinear. As the

    liquid nugget grows, FNgets larger (FNis proportional to the area of the nugget at the fayingsurface) so Fxgets smaller because Fx+ FN= FE,appliedassuming FE,applied= constant.

    Meanwhile, x goes up as can be derived from a moment equilibrium with respect to theacting point of FE,applied: FNd = Fxx when assuming d = constant. Because the magnitude ofFN increases and that of Fx goes down, x has to get larger, or F xgets farther away from the

    center of the nugget during nugget growth. It is reasonable to assume that when Fxmovesacross the right edge of the nugget (Point A), the solid loses its containment of the nugget.

    Therefore, x = rd can be regarded as a critical condition for expulsion to happen.

    Expulsion condition : FE = (rd)/r * FE,applied

    The discrepancy d is usually created by asymmetric loading, such as in the case of electrodemisalignment (axial and angular misalignments), electrode wear, or improper workpiece

    fitup. It can be approximated by the distance between the geometric center of the indentationmarks and that of the nugget. The force provided by the electrodesis fully used against thenuggetforce such that d = 0 and FE = FE,applied. Figure 6 shows a case with angular

    misaligned electrodes. The nugget forms around the shortest electrical current path, which isnot the same as where the total electrode force is applied because of the angular

    misalignment. As a result, an offset d is created between the applied electrode force and theforce from the nugget.The location of the applied electrode force is estimated from thesurface indentation and the nugget force is at the geometric center of the nugget.

    A guideline for selecting an electrode force/welding schedule can be obtained by estimatingthe conditions of extreme cases. The force from the liquid nugget can be calculated with the

    knowledge of its size and pressure.

    Schematic diagram of simplified forces and their locations on one

    workpiece at expulsion.

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    PRESSURE AND FORCES IN LIQUID NUGGET

    A volume increase occurs during heating in the solid state, solid to liquid phase

    transformation, and heating in the liquid state. The volume change due to melting happens atthe melting point for pure metals and between solidus and liquidus temperatures for alloys

    (except eutectic alloys). However, a free volume expansion of the nugget during resistancespot welding is not possible due to its surrounding solid containment and the squeezing ofelectrodes. As a result, pressure in the nugget may be significant because of the relatively low

    compressibility of liquids. Another source of pressure in the liquid nugget is the pressure ofmetal vapors. Such pressure exists because at temperatures above the melting point, a closed

    system tends to reach liquid/vapor equilibrium according to general thermodynamicprinciples. In add ition to metal vapor pressure, pressure from gases resulting from thermaldecomposition of surface agents should also be considered. Examples of surface agents are

    lubricants on metal sheets, pretreatment agents, adhesives (in the case of weld-bonding), and

    Forces acting on the weldment during resistance spotweldin in idealized

    Schematic diagram of the balance of forces considered in themodel.FN is the force from the nugget due to liquid pressure and FE is theeffective

    electrode force.

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    adsorbed moisture or gases. The pressure can be evaluated by considering the type andamount of gaseous products, and their reactivity with, and solubility in, the liquid alloy.

    So there are four major components of pressure in a liquid metal during resistance spot

    welding: solid to liquid phase transformation (melting), expansion in the liquid state, vapors

    from the liquid metal, and decomposition of surface agents.

    P =Pmelt +Pexp +Pvapor +Pdecomp

    PRESSURE DUE TO MELTING

    As the result of melting a certain portion of the metal surrounded by the solid phase,

    compression of the liquid takes place. The relationship between the volume V and pressurePin the liquid nugget at a given absolute temperature T can be described by the coefficient of

    compressibility

    V/P)T*1/ V

    Therefore, for a small increment of volume, the resulting increase in pressure is

    dP = d V*1/VSince the molten metal is not allowed to expand freely due to the containment of its solidsurrounding and electrode forces, the increase in pressure resulting from melting is

    approximately the same as that from compressing the liquid metal from VLto VS. Thispressure can be obtained by integrating where VSand VLare molar volumes of solid and

    liquid states, respectively, at the melting temperature. Therefore, the pressure due to meltingisPmelt= 1/ln(VL/ VS)

    So a high volume change during melting results in a high pressure contribution.

    PRESSURE CHANGE DUE TO LIQUID EXPANSION

    A quantitative relationship between pressure and temperature under a constant volume can be

    described by thermal pressure coefficient

    = 1/P(P/T)v

    Its value is unknown for most liquid metals. However, the partial derivative of P/T may be

    presented as the product of two partial derivatives:

    (P/T)v = - (V/T)p(P/V)vBy introducing a coefficient of volume thermal expansion,

    = 1/V(V/T)r

    and using compressibility coefficient , can be expressed by variables whose values can be

    found in published metallurgical data sources:

    = (1/P)(/

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    Hence, for a small increment of temperature, the increase in pressure is: D

    dP = (/dT

    Integraing the above yields the contribution of pressure due to the expansion of the liquid

    nugget in the range from melting point Tm to a given temperature Tat a constant volume inthe following form: de

    Pexp = (/(TTmelt)

    Because the contributions of vapor and surface agents to the total pressure are usually small,

    they can be neglected in estimating liquid pressure and force from the nugget. Therefore

    P = 1/ln(VL/ VS) + (/(TavgTmelt)

    PROCEDURE FOLLOWED IN PRESSURE CALCULATIONS

    Obtain material properties o f the maina lloying elements and surface contaminants.

    Obtain information of temperature distributionand value, and dimensions of the nugget. Calculate pressure components and thetotal pressure.

    Calculate forces in the directions of interest

    CURRENT AND WELD TIME DETERMINATION

    Weldability range (lobe) is the area where acceptable welds can be produced using a specificcombination of welding current and weld t ime. Welding range is limited by the minimumacceptable weld size and splash limit. In spot welding, weldability range is usually defined

    using coordinate axes where weld time is located on one axis and welding current on theother. The electrode force used, electrode geometry and cleanness, and the consistency and

    thickness of the welded material affect the shape and size of the weldabilityrange. Materials with good welding properties have a large weldability range, which meansthat welding parameters can be selected from a great number of different combinations. Cold

    rolled metal sheets usually have a large weldability range. Welding current can vary from1.02.0.kA in common weld times. The alloying of the steel and thick zinc coat ing, in

    particular, may decrease the weldability range. In this case, the correct use ofappropriate welding parameters is very important in terms of producing good spot welds.For a given combination of materials, electrodes, process conditions, and at a particular

    electrode-force, the weld lobe describes a region of acceptable welding parameters.The parameter axes are generally weld time (duration) & weld current. The "lower" boundary

    is the parameter combination that produces a weld button of minimum acceptabledimensions. The "upper" boundary is defined by expulsion conditions. Expulsion is a

    probabilistic event, so one way to define the limit is to find the conditions that lead to (say)

    50% of welds expelling. The area inside the lobe represents the "safe" welding window fornew electrodes. Generally the wider the better.

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    CONSRUCTION OF LOBE CURVES

    1. First you decide what is Cold, Hot, and OK. I use: Cold = undersize weld button when thecoupon is peeled apart, OK = greater than minimum acceptable size. Hot = expulsion

    occurred during the weld.2. Select the proper tips, that have a contact size of at least the minimum button size required.3. Then setup the proper force for the job.4. Next you condition the tips with 25 welds, this is very important for coated materials.

    5. Make a weld in a small coupon, record the current with an accurate weld current meter,along with the cycle time.

    6. Peel the coupon apart, measure button size, length plus width, and divide by two. (Lengthand width are at a 90 degree axis)7. Classify the weld, OK, Hot, or Cold. Note, if you got expulsion, it is Hot, dont bother to

    peel it.8. Enter the weld current under the appropriate column, there are four columns for OK, three

    for Cold, and three for Hot, use whatever one you want.9. Continue with different current levels10. Then change cycle time to 4 cycles, and entered 7 more welds.

    11. Then 6 cycles, then 7 cycles, then 3 cycles.As we fill in the area on the left, a chart is constructed on the right, that is our weld lobe. The

    spreadsheet also finds which cycle time gave the widest acceptable current range, andannounces that is the cycle time to use, along with a current that is about 10% below theexpulsion level.

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    Weld lobe data collection

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    Electrode force = 200kgf/cm2

    Elecrode force = 250 kgf/cm2

    Elecrode force = 300 kgf/cm2

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    SQUEEZE TIME SETTING

    Figure 2 shows how the weld time can be started at different times relating to theforce cycle. In the middle example, the welding current comes on too early and the

    squeeze time is too short to allow sufficient force to build up between componentsto produce a satisfactory weld. Many welding defects can be attributed to weldingwith too short a squeeze time.

    The lower example shows a welding cycle where the current is applied late and the peak

    force has been established for some time. Although acceptable welds may result from thissequence, time is wasted unnecessarily, and in volume production this can add significantcosts.

    Examples of different squeeze times in resistance welding

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    In the top figure, the squeeze time is adjusted so that the current is initiated just before thepeak welding force is achieved. This produces the best quality weld at the highest production

    rate.

    Modern programming systems for spot welding equipment enable the welding force current

    value and the relevant time sequence to be programmed. On closer inspection theprogrammed sequence actually performed by the welding gun may differ from the intendedwelding cycle. This is because of delays in the control system due to mechanical inertia,

    performance of the pneumatic force cylinder and other mechanical losses which modify the

    intended time sequence. It is essential to calibrate not only the forge force and the weldingcurrent but also to set the squeeze time correctly.

    The key forces are displayed on an illuminated bar on the Squeeze Analyser, shown

    schematically in figure 2. Short squeeze times are indicated by a large gap between thesqueeze force and the peak force. Long squeeze times result in the squeeze force and the peakforce being identical so that no gap in the illuminated bar occurs. Ideal squeeze times show as

    a small gap (one unlit light emitting diode) between squeeze and peak force. The simplevisual display of the Squeeze Analyser enables the supervisor quickly to assess the operatingvalues of a spot welding installation. In practice, it takes minutes to calibrate a gun correctly

    for optimum operating conditions. The actual values of the forces are also indicated on thefront panel display.

    PNUEMATIC VS SERVO GUN

    Pneumatic or hydraulic cylinders actuate most spot welding guns. The electrodes move the

    entire range of the cylinder when the gun opens and closes. Clamping force is normallyfixedby a pressure regulator, and there is usually no means to provide feedback regarding the

    actual clamping pressure. The motor-controlled servo gun provides variable electrodeopenings and programmable regulated pressure.

    Pneumatic guns often have two cylinders; one is used for short open and the other creates afull open space between electrodes. The servo gun (in position control) provides

    programmable electrode opening anywhere between the full stroke of the gun. The electrodeopening can be programmed to move simultaneously with other axes of the robot.

    Application flexibility cycle time savings are realized by the servo-gun's ability to open theelectrodes only a short distance, or a larger amount, to provide the exact clearance neededaround tooling or parts.

    During the weld, the servomotor switches to torque control and provides a uniform calibratedclamping force. This is easily programmed in the robot control and is expressed as a unit of

    force. The force can be stepped during an individual weld cycle or varied from weld to weldfor different material thickness stack-ups.

    Pneumatic guns close at full clamping force, which creates high impact on the tips. Theservo gun controls the rate at which the electrodes close and ramps up to the clamping force.This controlled process extends the life of tips and is a major reason auto manufacturers have

    been using them. The controlled clamp force also improves quality and cosmetics, allowingwelds to be made on Class A surfaces

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    Hence squeeze time for pneumatic guns is set to 3-4 cycle whereas squeeze time for servoguns can be set to 0 as weld trigger is given only after the application of tip force.

    SHEAR STRENGTH CALCULATION

    The shear strength of a single spot weld can be calculatedas follows:Shear strength(N)= 2.6 t d Rm

    where:t = sheet thickness, mmd = weld diameter, mmRm = tensile strength of the material, MPa

    PEEL TEST

    This test is conducted to determine nugget size and depth to ascertain the quality of spotweld.

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    SPOT SAMPLE

    For final verification spot samples were taken and their shear strength calculated by tensile-

    shear testing machine in R&D lab.

    Chisel test is conducted to check if spots are not broken

    Spot sample jig

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    Spot sample : 0.8-1.2mm sheet combination, current = 6.5, weld time = 15, pressure = 200

    Spot sample : 1.2-1.2mm sheet combination, current = 6.5, weld time = 18, pressure = 250

    Spot sample : 1.4-1.2mm sheet combination, current = 6.5, weld time = 20, pressure = 300

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    AUTOMATIC DETECTION SYSTEM

    There was a consistent problem of tip mis-alignment, improper face cutting and dresser not

    rotating. As a result these problems were regularly checked by the maintenance and quality

    department personnel. There was an urgent need to automate this process to avoid any

    possibility of degradation in spot quality due to tip mis-alignment and face cutting.

    TIP ALIGNMENT DETECTION

    CONTRUCTION AND WORKINGThis device consists of a mild steel strip of dimension 30 X 100 resting on cast iron rods.

    There is a pressure sensor below one of the rod. During tip dressing the tips will exert a

    vertical force in opposite direction on the plate. Any misalignment will cause a moment in theplate which in turn would increase or decrease the force exerted by the rod on the pressure

    sensor.

    Tip separated by x

    Mild steel strip

    Cast iron hollow rods

    Force sensor

    Mx

    R

    R

    F

    FW

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    TIP FORCE DETERMINATION

    Usually for steel design, the yield strength is used with a factor of safety, or, alternatively, aload factor is applied to the design load, and bending stresses must not exceed the

    yield stress.

    The bending stiffness is equal to the product of the elastic modulus E and the area moment ofinertia I of the beam cross-section about the axis of interest. In other words, the bending

    stiffness is EI . According to elementary beam theory, the relationship between the appliedbending moment M and the resulting curvature K of the beam is

    M = EIK

    The flexure of the plate depends on:

    1. The plate thickness

    2. The elastic properties of the plate

    3. The applied load or forceAs flexural rigidity of the plate is determined by the Young's modulus, Poisson's ratioand

    cube of the plate's elastic thickness, it is a governing factor in both (1) and (2).

    Flexural Rigidity,

    D = (Ehe3)/12(1v2)

    E = Young's Modulus

    he = elastic thickness (~1015 km)

    v = Poisson's Ratio

    Flexural rigidity of a plate has units ofPam3

    , i.e. one dimension of length less from the onefor the rod, as it refers to the moment per unit length per unit of curvature, and not the totalmoment. I is termed as moment of inertia.J is denoted as 2nd moment of inertia/polarmoment of inertia

    Factor of safety for mild steel = 3

    Bending stress b = (MY)/I

    Where M(X) = Bending Moment at X

    Y = Maximum distance from the neutral axis

    Ix= second moment of area= (bh3)/12 = 6.86* 10-12

    Sheet thickness = 1.4, length = 100 mm, breadth = 30 mm

    x = Maximum distance between misaligned weld tips in X direction = 15 mm = 1.5*10-2

    Bending moment ,M(Nm) = F(50)F(50 + X)

    Y = 1.4/2 = 0.7 mm = 7* 10-4 m

    Maximum bending stress will be at the bottom most point.

    b = (Fx*7* 10-4)/I

    =( F*1.5*10-2*7* 10-4)/( 6.86* 10-12)

    F = b /1.53*106

    http://en.wikipedia.org/wiki/Pascal_(unit)http://en.wikipedia.org/wiki/Pascal_(unit)http://en.wikipedia.org/wiki/Pascal_(unit)http://en.wikipedia.org/wiki/Pascal_(unit)
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    Bending stress has to be less than allowable tensile stress

    Allowable tensile stress = Youngs modulus(E)/FOS

    E for mild steel = 420 Mpa

    Allowable stress , t = 420/3 = 140 Mpa

    F = 140*106/1.53*106

    = 93 N

    MISALIGNMENT CALIBRATION

    Mx = 0

    0 = 50(1500)1500(50+X)RB(100)RB = 15x

    RB can be determined from the load cell reading. Accordingly x is calculated to determine thedegree of misalignment.

    Tips can be adjusted using L keys. 5 full rotation moves the tip 1mm towards the fixed tip.

    FACE CUTTING DETECTION

    Proper dress ing is required to bring the tip diameter to the required level. This is necessary so

    that the required current density is maintained. It is also necessary to remove any carbondeposits that may obstruct the flow of current during welding.The device consists of component locating pin which is paced at the top of the metal strip.

    The Robot gun travels a certain perpendicular distance from a datum until the gun tip touches

    the locating pin. The distance is recorded to determine whether there is any hole at the tip

    centre due to improper dressing.

    To check the tip diameter after dressing the tip is made to exert certa in force over the gauge

    pressure sensor. If the tip diameter is less pressure exerted would be high and hence improper

    dressing would be detected.

    X

    Datum

    Locating

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    The material used is cast iron. Since the minimum force detectable from the load cell is veryless available cone with tip diameter 1.5 mm is feasible. The compressive stress developed

    would be very less.ROBOT PROGRAMMINGTip dressing programm was modified in accordance with the sensor requirement. For e.g.

    programm was made for the additional path robot follows after dressing, giving differentpressure schedule during testing and logic was given to check the conditions for proper

    process in macro module.

    1: !*** 371A TIP DRESS *** ;2: ;

    3: UTOOL_NUM = 1 ;4: UFRAME_NUM = 0 ;5: $USEUFRAME = 0 ;

    6: PAYLOAD[1] ;7: ;

    8: !*** IO_RESET *** ;9: CALL IO_RESET ;10: ;

    11: !*** AROUND HOME POSITION*** ;

    12:L PR[2] 2000mm/sec FINE ;13: ;14: Reset Tip Wdn ;

    15: ;16: LBL[1] ;

    17: R[17] = 0 ;18: DO[213] = ON ;19: ;

    20:L P[3] 2000mm/sec FINE ;21: ;

    22: !*** BEFORE DRESS POSITION*** ;23:L P[4] 2000mm/sec FINE ;

    24: ;25: DO[221] = ON ;

    26: R[99] = $MCR.$GENOVERRIDE ;27: OVERRIDE = 100% ;28: ;

    29: !*** DRESS POSITION *** ;

    30:L P[5] 200mm/sec FINEPRESS_MOTION P=[99,89] ;

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    31: ;32: WAIT 0.50(sec) ;

    33: WAIT DI[203] = ON ;34: ;

    35: !*** BEFORE DRESS POSITION

    *** ;36:L P[4] 300mm/sec CNT0 ;

    37: ;38: DO[221] = OFF ;

    39: DO[213] = OFF ;41: ;42:L P[3] 1000mm/sec CNT10 ;

    43: ;44: CALL TWD ;

    45: ;46:L P[3] 1000mm/sec CNT10 ;

    47: ;48: DO[210] = ON ;49: ;

    50: !*** Tip Change Request *** ;51: IF DI[210] = ON,JMP LBL[10] ;52: ;

    54: ;55: DO[210] = OFF ;

    56: WAIT 0.50(sec) ;57: ;58: CALL WDN_CHK ;

    59: ;60:L PR[2] 2000mm/sec CNT100 ;

    61: ;62: CALL IO_RESET ;63: ;

    64: !*** HOME POSITION *** ;65:L PR[1] 2000mm/sec FINE ;

    66: ;67: !*** IO_RESET *** ;68: CALL IO_RESET ;

    69: ;70: IF R[17] = 1,JMP LBL[1] ;

    71: ;72: END ;73: ;

    74: LBL[10] ;75: ;

    76: ;77: !*** Tip Change Position *** ;78:L P[9] 2000mm/sec FINE ;

    79: ;

    80: Reset Tip Wdn ;81: ;

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    CONCLUSION

    Spatter reduction activities were a huge success. We reached our target of 5 % in 4 weld areas

    in Ertiga line. Parameter determination for different sheet combination helped us achieve the

    required spot quality at low current and weld time.

    REFERENCES

    1. Expulsion Prediction in Resistance Spot Welding by J. SENKARA, H. ZHANG,

    AND S. J. HU2.

    Spot Weld Properties When Welding With ExpulsionA Comparative Study by M.

    Kimchi3. Ruukki-Resistance-welding-manual4.

    Miller Handbook for Resistance Spot Welding

    5.

    http://www.updatetechnology.com/

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