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Thread: Chrome Moly 4130 Motor Mounts - Prefab Parts?

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  1. #1
    Aaron Novak's Avatar
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    Well this certainly got weird fast. The thing is I get where nixrox is coming from, as I work in NDT and materials as well, however there has to be a dose of reality there as I also work in prototyping where you don't have the advantage of making 100 identical parts to study and fine tune a process and procedure. We get one shot to do it. This is why I have preached using the most conservative approach to constructing any one of part. Is there shoddy welding in some homebuilts....honestly yes. Are there failed welds both OEM and homebuilt.....yes. Luckily most are caught and the designs robust enough to survive to repair so nobody hears about them. Should we rely on this robustness alone....absolutely not. There is room for education and improvement in the homebuilt area and the EAA is in an excellent position to do so, if they should ever choose.

  2. #2

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    Quote Originally Posted by Aaron Novak View Post
    Well this certainly got weird fast. The thing is I get where nixrox is coming from, as I work in NDT and materials as well, however there has to be a dose of reality there as I also work in prototyping where you don't have the advantage of making 100 identical parts to study and fine tune a process and procedure. We get one shot to do it. This is why I have preached using the most conservative approach to constructing any one of part. Is there shoddy welding in some homebuilts....honestly yes. Are there failed welds both OEM and homebuilt.....yes. Luckily most are caught and the designs robust enough to survive to repair so nobody hears about them. Should we rely on this robustness alone....absolutely not. There is room for education and improvement in the homebuilt area and the EAA is in an excellent position to do so, if they should ever choose.
    Aaron - do you have any x-ray film to prove that your welds are defect free? How about Ultrasonic weld inspection reports by a certified UT Tech? How many CGSB or ASNT level 2 or 3 certifications do you hold?

    You cannot weld on certified aircraft without a license.
    You cannot fly an aircraft without a license.
    You cannot perform maintenance on a certified aircraft without a license.
    You cannot perform NDT inspections on aircraft without a license.
    You cannot weld anything in the oil or construction industry without a license and a successful welder test at the site.
    What makes you think anyone should be allowed to weld on an aircraft without a license or any recognized training or testing?

    Did you notice that not one of the sarcastic responding trolls or naysayers mentioned the EIGHTEEN (18) destroyed aircraft due specifically to weld problems since 1996.

    I rest my case and will let Darwin's theory root out those individuals who like to tempt fate.
    As a person with some NDT knowledge, I would have expected you to have a better handle on defect propagation and structural analysis.
    Good luck by the way.

  3. #3
    rwanttaja's Avatar
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    Quote Originally Posted by nixrox View Post
    Did you notice that not one of the sarcastic responding trolls or naysayers mentioned the EIGHTEEN (18) destroyed aircraft due specifically to weld problems since 1996.
    1998-2016, actually. That's just about one accident a year, or roughly 0.5% (half a percent) of homebuilt accidents. Only three of them resulted in fatalities, accounting for 0.3% of the fatal accidents.

    Not saying a reduction wouldn't be nice, it's just not a major contributor to the homebuilt accident rate. The same amount of effort to "fix" other problems would save more lives.

    Here's a summary of the number of fatal accidents for given causes. This, again, covers the 1998-2016 time period. There were about 960 fatal accidents in this time period.
    Accident Cause
    Number of Fatal Accidents
    Pilot Miscontrol
    284
    Manuevering Low Alt
    116
    Engine Failure - Undetermined
    83
    Continued VFR into IFR Conditions
    38
    Fuel Exhaustion
    29
    Midair
    24
    Pilot Incapacitation
    20
    Internal Engine Issues
    18
    Failure to Recover from Aerobatics
    18
    Fuel Starvation
    12
    CG or Weight
    11
    Fuel System Issues
    10
    Carb Ice
    9
    Fuel Contamination
    8
    Inadequate Preflight
    7
    Reduction Drives
    6
    Fire
    6
    Disorientation
    5
    Ignition
    4
    Carb Mechanical
    4
    Oil System
    3
    Cooling System
    2
    Wake Turbulence
    2
    Airframe Icing
    2
    Suicide
    2
    Note that there were almost as many accidents involving suicide as there were fatal accidents involving bad welds. As far as I can determine, the weld issues just aren't that common.

    Mind you, bad welds only make the NTSB database if an accident meets the reporting criteria. Likely there were more failed welds, that either caused little or no damage or were detected on the ground prior to takeoff.

    No one's doubting that homebuilt welds could be better, just that bad welds aren't that major a problem.

    Ron Wanttaja

  4. #4
    Aaron Novak's Avatar
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    Quote Originally Posted by nixrox View Post
    Aaron - do you have any x-ray film to prove that your welds are defect free? How about Ultrasonic weld inspection reports by a certified UT Tech? How many CGSB or ASNT level 2 or 3 certifications do you hold? I have done X-ray yes, Ultrasonic yes, I don't live in Canada.

    You cannot weld on certified aircraft without a license. Here in the USA yes you can, you just cannot sign it off.
    You cannot fly an aircraft without a license. The OP is working on an ultralight, so yes he can.
    You cannot perform maintenance on a certified aircraft without a license. Unless you are the builder or it is an ultralight true. Or if you are working under someone with the proper credentials.
    You cannot perform NDT inspections on aircraft without a license. Again, in the homebuilt world yes you can, and even in the certified world anyone can do the work as long as a person with the proper credentials signs it off.
    You cannot weld anything in the oil or construction industry without a license and a successful welder test at the site. That is because the weldors self certify each weldment, and much of the history of pipeline welding is linked to unions and having to hold union "tickets" etc etc. Not that pipelines ever have failed welds.....
    What makes you think anyone should be allowed to weld on an aircraft without a license or any recognized training or testing? That's not up to me, that is up to the FAA, and they don't exclude anyone.

    Did you notice that not one of the sarcastic responding trolls or naysayers mentioned the EIGHTEEN (18) destroyed aircraft due specifically to weld problems since 1996. Are we counting the ones caused by the design and production engineers improper welding processes and procedures?

    I rest my case and will let Darwin's theory root out those individuals who like to tempt fate.
    As a person with some NDT knowledge, I would have expected you to have a better handle on defect propagation and structural analysis.
    Good luck by the way. The majority of the failures I see are fatigue initiating in the microstructure of the HAZ, nothing that can be found with NDT, and that is why my efforts have concentrated on best practices from a design and welding process perspective. The reinforcement sizes of proper welds on 4130 tubular structures are so oversize ( a good thing) that even large oxide inclusions seem to pose little threat.
    See above for my comments.

    Just for clarification, you were an inspector, not a weldor correct? I see in your list of tools that you have mig welders and a stick welder, so I am guessing you yourself do not do, or teach aerospace welding? Just trying to get an idea what your experience level and type is?
    Last edited by Aaron Novak; 10-10-2018 at 11:24 AM.

  5. #5

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    to add my small idea the forum. maybe the welder could cut into some of his welds , one poor weld ,one good weld , and one of his best welds. To see how to see his welding / heating penetrates the metal.........and on seeing photos ,the original poster. is using, some nice jigs / fixtures ..... good day /// rick

  6. #6

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    Well you guys certainly are extremely sensitive and very easy to get a rise out of.
    However, in the interests of clearing the air, I decided to go straight to the horses mouth - Miller Welding.
    I found an article that covers best practices for welding 4130 chrome-moly, low alloy tubing.
    Surprise, surprise - if you follow this article carefully, you should notice that the 'novice' home built welders on this forum have been giving you totally wrong information.
    So if you want the correct information you need to go to the specialist who actually do this for a living.
    Enjoy the article.


    Best Practices for TIG Welding of 4130 Chrome-Moly Tubing
    In General Motorsports and Aerospace Applications


    Chrome-moly steel offers a good blend of strength, weight and ductility
    for many motorsports and aerospace applications. The following article
    discusses some of the recommended procedures and equipment for
    successfully TIG welding 4130 chrome-moly steel.


    Just as a NHRA (National Hot Rod Association) drag racing team depends
    on blend of team talent to win races, the material selected for a
    particular application requires a blend of properties to withstand the
    stresses involved. For a drag racing chassis, and for many other
    motorsports and aerospace applications, that material is 4130
    chromium-molybdenum, or chrome-moly, which is selected for its blend of
    ductility, strength, weight and fabrication advantages.

    The 4130 grade of chrome-moly is a high-strength low-alloy (HSLA) steel
    that contains molybdenum (0.15 - 0.25 percent by weight) and chromium
    (0.8 - 1.1 percent by weight) as strengthening agents. However, it has
    relatively low carbon content (nominally 0.30 percent), so it welds,
    machines and bends almost as easily as 1018 DOM mild steel tubing (which
    has an 0.18 percent carbon content).


    *Material* *Tensile Strength* *Yield Strength *Hardness, Rockwell B* *Elongation*
    4130 chrome-moly 97,200 psi 63,100 psi 92 25.5%


    Chrome-moly is not lighter than steel, a common misconception. Both
    weigh about 491 lbs. per cubic foot.
    However, chrome-moly offers a better strength-to-weight ratio and better
    elongation (a measure of ductility), which enables designers to use
    thinner wall and/or smaller diameter tubing to reduce overall weight.

    Because many motorsports, aerospace and sporting goods applications
    involve welding normalized 4130 chrome-moly tubing with a wall
    thicknesses of less than .125-in., this article will focus on best
    practices for these applications.

    Welding Consumables and Variables

    Material 4130 chrome-moly tubing (normalized).

    Thickness < 0.125 in. Most chassis tubing has a wall thickness ranging
    from 0.035 – 0.083 in. and diameters from 1/4in. - 1-5/8in.

    Amperage 1 amp per .001 in. of wall thickness.

    Polarity DC Electrode Negative. HF for arc starts only.

    Pulsing Optional.

    Filler Material ER70S-2 or ER80S-D2.

    Filler Diameter 0.030 – 1/8-in. Generally, do not use a rod larger than the thickness of the base metal.

    Tungsten Type 2% type (Ceriated is first choice, then Thoriated)

    Tungsten Diameter 1/16 – 3/32 (smaller diameter for thinner wall).

    Tungsten Prep Pointed.

    Arc Length
    Less than or equal to the electrode diameter. Generally, the tighter
    the better, as shorter arc lengths reduce heat input.

    Electrode Stickout
    No further than the distance of the inside diameter
    of the cup being used. However using a gas lens can extend this distance.
    Gas Lens Not required, but helpful if a tight joint configuration
    demands a longer stickout or involves multiple tubes. Keep the screen
    free of debris and spatter.

    Shielding Gas
    100% argon, 15 – 20 CFH. More is not better, as
    turbulence could suck atmosphere into the weld.

    Pre-flow
    .4 to .6 seconds.

    Post-flow
    10 – 15 seconds.

    Backing Gas
    Follow applicable codes/standards, if any; not required for NHRA applications.
    It is required for aircraft to reduce potetial contamination on the backside of the weld.

    Pre-heat
    Not required as long as tubing is above 60 – 70 degrees F.

    Stress Relief
    Not required on material < 0.125 inch; simply allow the weld to air-cool.

    Tack Welds
    Four tacks made 90 degrees apart; tacks ideally should be longer than wide.

    Joint Preparation
    Tubing notcher for coping, drum sander for final
    fit-up, deburring for edge preparation, Scotch-Brite™ or 120 grit sand
    paper to clean about 1 in. back from the joint, and final clean with
    acetone, lacquer thinner or similar solvent to remove oil.

    Joint Gap
    None! Realistically, gaps smaller than 0.010 are permissible; larger
    gaps promote poor quality.

    Weld Size
    Keep welds to within their specified size: a weld needs to be no larger
    than its thinnest section, which will be the “weakest link” in the
    chain. Larger-than-necessary welds add excess heat and waste gas, filler
    rod and time.

    Weld Technique
    Weld in one continuous motion, pulsing the foot control
    and adding filler rod to create the “stack of dimes” appearance (or use
    the machine’s pulsing controls). Do not stack separate puddles on top of
    each other, as this may lead to incomplete fusion.

    End-of-Weld Procedure
    Avoid pinholes by tapering off heat input at the end of the weld and
    maintaining a constant distance between the tungsten and the weldment.

    Weld Appearance
    A good weld looks shiny and has a bluish tint. A dirty, gray-looking
    weld may indicate poor shielding gas coverage or excess heat.


    Perfect Fit-Up

    When welding thin-wall tubing, whether chrome-moly or other metals, the
    welders at Cagnazzi Racing joke that their tolerances range from perfect
    to almost not perfect. That is, if the parts don’t fit perfectly, they
    start over because thin-wall tubing does not have sufficient mass to
    absorb excess heat.

    The usual “trick” to filling gaps with GTAW is to use a larger diameter
    filler rod. However, larger rods require more heat and excess heat
    promotes burn-through, warping and embrittlement. Using a larger rod
    might be an acceptable solution in a non-critical application, but it’s
    a poor practice when welding chrome-moly.

    Consistency
    Cagnazzi uses hundreds of jigs and fixtures bolted to a surface that is
    flat to within a few thousandths of an inch for fabricating even the
    smallest items to help ensure tight fit-up and consistent tube
    placement, which provides repeatability

    Chrome Moly Tubing Consistency
    By producing a new chassis nearly identical to the previous, the crew
    chief can hone his craft of gear ratio and clutch management without
    worrying about a new chassis introducing unknown variables. Many
    fabricators believe that they cannot afford to build fixtures for all of
    their components or for larger weldments. However, if repeatability and
    accuracy are important, good fixturing is mandatory.


    Coping Mechanism
    Most of Cagnazzi’s jigs have a go/no-go type fit, which enables
    “sneaking up” on a perfect fit by making small incremental adjustments.

    After cutting to approximate length with a band saw, Cagnazzi uses a
    tube notcher for rough coping. The fabricator will then check
    the length and use a drum sander to sneak up on a perfect fit by slowly
    sanding away excess metal from the mouth of the tube. Before
    welding, the fabricator will deburr the edge , clean back 1 in.
    from edge using Scotch-Brite or 120 grit sandpaper and remove oils or
    other contaminants with a solvent. Be sure to wear nitrile
    gloves, as the natural oils from your fingers can ruin a weld just as
    thoroughly as grease or cutting fluid. Don’t forget to use the sandpaper
    and solvent on the filler rod, too.

    Filler Metal Selection
    In many motorsports and aerospace applications, engineers want some
    degree of ductility in the weld to help absorb impacts and prevent
    cracking. For this reason, most NHRA fabricators intentionally dilute
    the strength of the parent material by selecting ER70S-2 for filler for
    roll cages, chassis and other applications requiring more flexibility.
    While actual tensile strength of the weld will vary and depend on other
    factors, 4130 diluted with ER70S-2 filler likely produces a weld with a
    tensile strength in the 80,000 to 82,000 psi range.

    For areas requiring higher strength, such as spindles and upper and
    lower control arms, fabricators select ER80S-D2 filler, which produces
    welds with a high tensile strength (as a side note, consider that S-2
    fillers clean impurities better than D-2 fillers). In any event, do not
    use 4130 filler, as the weld will not have sufficient ductility unless
    it undergoes stress relief.

    As for filler rod diameter, use a rod diameter that matches the
    thickness of the base metal. Trying to weld 0.035-in. tubing with a
    1/16th inch filler (0.063-in.) is a bad idea because the tubing wall
    will melt before the filler rod is up to temperature. Cagnazzi
    predominantly uses 0.030-, 0.045- and 0.063-in. (1/16th) filler rods
    , with .045 and .063 being the most common. For thicker, larger
    diameter tubing they use 3/32- and 1/8-in. rods.

    Heat Control
    Successfully welding 4130 requires preserving its mechanical properties
    by heating and cooling the weld in a controlled manner. Excess heat
    causes carbide precipitation, and cooling too quickly causes
    embrittlement. Fortunately, the GTAW process provides sufficient heat
    control. Welds made on tubing 1/8-inch or thinner do not require
    pre-heating or post-weld stress relief, yet they will have sufficient
    penetration as long operators follow the general rule of the thumb by
    using 1 amp per 0.001 in. of metal thickness.
    Note that if the tubing is below 60 degrees F, use a small propone torch
    to heat the base metal to up to 300 degrees F. Otherwise, the metal
    could cool too quickly and become brittle. Welding cold metal may also
    promote hydrogen cracking, so that’s another reason to preheat 4130 if
    it’s cold.


    Puddle Size and Arc Length
    While welding too slowly increases overall heat input, operators should
    not necessarily focus on welding travel speed. Rather, they should focus
    on controlling their body (Fig. 11), controlling puddle size by making
    the puddle only as wide as necessary and holding a tight arc length of
    1/8-in. or less.

    Note that a longer arc length, or tungsten tip-to-work distance,
    increases overall heat input, because a GTAW power source automatically
    increases voltage when arc length increases. If the joint configuration
    limits access because of cup size, do not try to weld with a longer arc.
    Rather, use a smaller cup or a gas lens and extend the tungsten.

    To better control heat input, and to enable repositioning the body to
    better control torch movement, do not weld the circumference of a tube
    in one pass. Rather, weld it in four quarters. Weld only two of the
    quarters (on opposite side of the tube) then move to another joint. When
    the first joint cools, come back and complete the remaining sections.


    No Slacking Allowed — EVER

    The authors of this article weld 4130 tubing in critical applications,
    and they have a combined 50 years of welding experience. As such, they
    take every step of the fabrication process seriously.

    “Close enough” is simply not good enough for NHRA or AEROSPACE work,
    nor should it be, for a child’s go-kart or bicycle.

  7. #7
    Aaron Novak's Avatar
    Join Date
    Aug 2011
    Location
    Oshkosh, Wi
    Posts
    361
    Quote Originally Posted by nixrox View Post
    Well you guys certainly are extremely sensitive and very easy to get a rise out of.
    However, in the interests of clearing the air, I decided to go straight to the horses mouth - Miller Welding.
    I found an article that covers best practices for welding 4130 chrome-moly, low alloy tubing.
    Surprise, surprise - if you follow this article carefully, you should notice that the 'novice' home built welders on this forum have been giving you totally wrong information.
    So if you want the correct information you need to go to the specialist who actually do this for a living.
    Enjoy the article.


    Best Practices for TIG Welding of 4130 Chrome-Moly Tubing
    In General Motorsports and Aerospace Applications


    Chrome-moly steel offers a good blend of strength, weight and ductility
    for many motorsports and aerospace applications. The following article
    discusses some of the recommended procedures and equipment for
    successfully TIG welding 4130 chrome-moly steel.


    Just as a NHRA (National Hot Rod Association) drag racing team depends
    on blend of team talent to win races, the material selected for a
    particular application requires a blend of properties to withstand the
    stresses involved. For a drag racing chassis, and for many other
    motorsports and aerospace applications, that material is 4130
    chromium-molybdenum, or chrome-moly, which is selected for its blend of
    ductility, strength, weight and fabrication advantages.

    The 4130 grade of chrome-moly is a high-strength low-alloy (HSLA) steel
    that contains molybdenum (0.15 - 0.25 percent by weight) and chromium
    (0.8 - 1.1 percent by weight) as strengthening agents. However, it has
    relatively low carbon content (nominally 0.30 percent), so it welds,
    machines and bends almost as easily as 1018 DOM mild steel tubing (which
    has an 0.18 percent carbon content).


    *Material* *Tensile Strength* *Yield Strength *Hardness, Rockwell B* *Elongation*
    4130 chrome-moly 97,200 psi 63,100 psi 92 25.5%


    Chrome-moly is not lighter than steel, a common misconception. Both
    weigh about 491 lbs. per cubic foot.
    However, chrome-moly offers a better strength-to-weight ratio and better
    elongation (a measure of ductility), which enables designers to use
    thinner wall and/or smaller diameter tubing to reduce overall weight.

    Because many motorsports, aerospace and sporting goods applications
    involve welding normalized 4130 chrome-moly tubing with a wall
    thicknesses of less than .125-in., this article will focus on best
    practices for these applications.

    Welding Consumables and Variables

    Material 4130 chrome-moly tubing (normalized).

    Thickness < 0.125 in. Most chassis tubing has a wall thickness ranging
    from 0.035 – 0.083 in. and diameters from 1/4in. - 1-5/8in.

    Amperage 1 amp per .001 in. of wall thickness.

    Polarity DC Electrode Negative. HF for arc starts only.

    Pulsing Optional.

    Filler Material ER70S-2 or ER80S-D2.

    Filler Diameter 0.030 – 1/8-in. Generally, do not use a rod larger than the thickness of the base metal.

    Tungsten Type 2% type (Ceriated is first choice, then Thoriated)

    Tungsten Diameter 1/16 – 3/32 (smaller diameter for thinner wall).

    Tungsten Prep Pointed.

    Arc Length
    Less than or equal to the electrode diameter. Generally, the tighter
    the better, as shorter arc lengths reduce heat input.

    Electrode Stickout
    No further than the distance of the inside diameter
    of the cup being used. However using a gas lens can extend this distance.
    Gas Lens Not required, but helpful if a tight joint configuration
    demands a longer stickout or involves multiple tubes. Keep the screen
    free of debris and spatter.

    Shielding Gas
    100% argon, 15 – 20 CFH. More is not better, as
    turbulence could suck atmosphere into the weld.

    Pre-flow
    .4 to .6 seconds.

    Post-flow
    10 – 15 seconds.

    Backing Gas
    Follow applicable codes/standards, if any; not required for NHRA applications.
    It is required for aircraft to reduce potetial contamination on the backside of the weld.

    Pre-heat
    Not required as long as tubing is above 60 – 70 degrees F.

    Stress Relief
    Not required on material < 0.125 inch; simply allow the weld to air-cool.

    Tack Welds
    Four tacks made 90 degrees apart; tacks ideally should be longer than wide.

    Joint Preparation
    Tubing notcher for coping, drum sander for final
    fit-up, deburring for edge preparation, Scotch-Brite™ or 120 grit sand
    paper to clean about 1 in. back from the joint, and final clean with
    acetone, lacquer thinner or similar solvent to remove oil.

    Joint Gap
    None! Realistically, gaps smaller than 0.010 are permissible; larger
    gaps promote poor quality.

    Weld Size
    Keep welds to within their specified size: a weld needs to be no larger
    than its thinnest section, which will be the “weakest link” in the
    chain. Larger-than-necessary welds add excess heat and waste gas, filler
    rod and time.

    Weld Technique
    Weld in one continuous motion, pulsing the foot control
    and adding filler rod to create the “stack of dimes” appearance (or use
    the machine’s pulsing controls). Do not stack separate puddles on top of
    each other, as this may lead to incomplete fusion.

    End-of-Weld Procedure
    Avoid pinholes by tapering off heat input at the end of the weld and
    maintaining a constant distance between the tungsten and the weldment.

    Weld Appearance
    A good weld looks shiny and has a bluish tint. A dirty, gray-looking
    weld may indicate poor shielding gas coverage or excess heat.


    Perfect Fit-Up

    When welding thin-wall tubing, whether chrome-moly or other metals, the
    welders at Cagnazzi Racing joke that their tolerances range from perfect
    to almost not perfect. That is, if the parts don’t fit perfectly, they
    start over because thin-wall tubing does not have sufficient mass to
    absorb excess heat.

    The usual “trick” to filling gaps with GTAW is to use a larger diameter
    filler rod. However, larger rods require more heat and excess heat
    promotes burn-through, warping and embrittlement. Using a larger rod
    might be an acceptable solution in a non-critical application, but it’s
    a poor practice when welding chrome-moly.

    Consistency
    Cagnazzi uses hundreds of jigs and fixtures bolted to a surface that is
    flat to within a few thousandths of an inch for fabricating even the
    smallest items to help ensure tight fit-up and consistent tube
    placement, which provides repeatability

    Chrome Moly Tubing Consistency
    By producing a new chassis nearly identical to the previous, the crew
    chief can hone his craft of gear ratio and clutch management without
    worrying about a new chassis introducing unknown variables. Many
    fabricators believe that they cannot afford to build fixtures for all of
    their components or for larger weldments. However, if repeatability and
    accuracy are important, good fixturing is mandatory.


    Coping Mechanism
    Most of Cagnazzi’s jigs have a go/no-go type fit, which enables
    “sneaking up” on a perfect fit by making small incremental adjustments.

    After cutting to approximate length with a band saw, Cagnazzi uses a
    tube notcher for rough coping. The fabricator will then check
    the length and use a drum sander to sneak up on a perfect fit by slowly
    sanding away excess metal from the mouth of the tube. Before
    welding, the fabricator will deburr the edge , clean back 1 in.
    from edge using Scotch-Brite or 120 grit sandpaper and remove oils or
    other contaminants with a solvent. Be sure to wear nitrile
    gloves, as the natural oils from your fingers can ruin a weld just as
    thoroughly as grease or cutting fluid. Don’t forget to use the sandpaper
    and solvent on the filler rod, too.

    Filler Metal Selection
    In many motorsports and aerospace applications, engineers want some
    degree of ductility in the weld to help absorb impacts and prevent
    cracking. For this reason, most NHRA fabricators intentionally dilute
    the strength of the parent material by selecting ER70S-2 for filler for
    roll cages, chassis and other applications requiring more flexibility.
    While actual tensile strength of the weld will vary and depend on other
    factors, 4130 diluted with ER70S-2 filler likely produces a weld with a
    tensile strength in the 80,000 to 82,000 psi range.

    For areas requiring higher strength, such as spindles and upper and
    lower control arms, fabricators select ER80S-D2 filler, which produces
    welds with a high tensile strength (as a side note, consider that S-2
    fillers clean impurities better than D-2 fillers). In any event, do not
    use 4130 filler, as the weld will not have sufficient ductility unless
    it undergoes stress relief.

    As for filler rod diameter, use a rod diameter that matches the
    thickness of the base metal. Trying to weld 0.035-in. tubing with a
    1/16th inch filler (0.063-in.) is a bad idea because the tubing wall
    will melt before the filler rod is up to temperature. Cagnazzi
    predominantly uses 0.030-, 0.045- and 0.063-in. (1/16th) filler rods
    , with .045 and .063 being the most common. For thicker, larger
    diameter tubing they use 3/32- and 1/8-in. rods.

    Heat Control
    Successfully welding 4130 requires preserving its mechanical properties
    by heating and cooling the weld in a controlled manner. Excess heat
    causes carbide precipitation, and cooling too quickly causes
    embrittlement. Fortunately, the GTAW process provides sufficient heat
    control. Welds made on tubing 1/8-inch or thinner do not require
    pre-heating or post-weld stress relief, yet they will have sufficient
    penetration as long operators follow the general rule of the thumb by
    using 1 amp per 0.001 in. of metal thickness.
    Note that if the tubing is below 60 degrees F, use a small propone torch
    to heat the base metal to up to 300 degrees F. Otherwise, the metal
    could cool too quickly and become brittle. Welding cold metal may also
    promote hydrogen cracking, so that’s another reason to preheat 4130 if
    it’s cold.


    Puddle Size and Arc Length
    While welding too slowly increases overall heat input, operators should
    not necessarily focus on welding travel speed. Rather, they should focus
    on controlling their body (Fig. 11), controlling puddle size by making
    the puddle only as wide as necessary and holding a tight arc length of
    1/8-in. or less.

    Note that a longer arc length, or tungsten tip-to-work distance,
    increases overall heat input, because a GTAW power source automatically
    increases voltage when arc length increases. If the joint configuration
    limits access because of cup size, do not try to weld with a longer arc.
    Rather, use a smaller cup or a gas lens and extend the tungsten.

    To better control heat input, and to enable repositioning the body to
    better control torch movement, do not weld the circumference of a tube
    in one pass. Rather, weld it in four quarters. Weld only two of the
    quarters (on opposite side of the tube) then move to another joint. When
    the first joint cools, come back and complete the remaining sections.


    No Slacking Allowed — EVER

    The authors of this article weld 4130 tubing in critical applications,
    and they have a combined 50 years of welding experience. As such, they
    take every step of the fabrication process seriously.

    “Close enough” is simply not good enough for NHRA or AEROSPACE work,
    nor should it be, for a child’s go-kart or bicycle.
    Miller is not an authority on aerospace weldments on 4130, they are a company that makes welding equipment ( To be fair NONE of the welding machine manufacturers should be considered design experts for weldments). They have no materials lab, no NDT lab, no MTS lab, do no structural or fatigue testing of any kind. This is not their job, they are not something like edison welding institute or southwest research or NASA, they are a tool maker. Their suggestions are kind of sketchy do you not agree? How can you use material thickness alone to determine if you need PWHT? No mention of joint configuration at all? It looks like they grabbed that thickness from what I am guessing is a jominy bar test and misunderstood the data or totally missed the material thickness equivalency calculations. This is not a bash on Miller at all, they are a fine company that I have visited many times. I'm really trying to figure out where you are going here? You claim nobody knows what they are doing in aviation, yet post a copy and paste off the internet from a company that has no authority in aviation. Considering your push to put engineering into weldments I am just surprised.

  8. #8

    Join Date
    Jan 2018
    Posts
    15
    obviously you have a reading handicap.
    Miller never wrote the article - they just put it in the magazine.
    The article was written by two journeyman welders with 50 years of experience.
    I trust journeyman far more than part-time trainee welders - like you.

    You should not be giving welding advice to anyone, because you do not have the license, training nor experience.
    The difference between you and me is that I always take welding projects to journeyman welders.
    I may be a certified weld inspector and licensed NDT Inspector but my welding sucks.
    I complete all the mechanical work and farm out the welding and upholstery to the experts.
    have a nice day.

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