Establishing Squeeze Time
[from PWL#102 - Section 3]This is not the first time I pick up useful hints from the always interesting Q&A notes published by The Welding Journal (January 2012, page 20). I always recommend these informative pages.
A reader had asked where to find squeeze time data to spot weld cold rolled and galvanized steel, as it is not published along other schedule data in the RWMA Resistance Welding Manual. The Author, Roger Hirsch, suggested in his answer to find it by trial and error.
One should remind that squeeze time is the time interval between timer initiation and first application of current. It is designed to allow electrode movement and full force action deployment before performing the spot weld.
It appears that this interval is dependent on design details of each machine: because of this reason it cannot be a fixed datum to be published on tables.
Too short a squeeze time will manifest itself by the appearance of sparks from under the electrode. By simply increasing this time in parallel tests until sparking (almost) stops one can find the correct value (in cycles) needed for correct operation.
Note that any further increment does not add any advantages and wastes production time.The alternative answer that involves calculations seems less attractive.
If the equipment has a differential pressure transducer that monitors the air pressure on both sides of the cylinder, one can establish the time when full pressure is applied to the electrodes. If a signal can then be used to start the current cycles, squeeze time is redundant and can be bypassed (set to zero).
Interested readers are referred to the original article indicated above.
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How many weld repairs are allowed?
[From PWL#103 - Section 3]
You may recall having seen requirements limiting the number of allowed repairs performed on the same location, for the purpose of protecting the construction from weak spots likely to develop due to repeated weld repairs.
If you are bound by such a customer requirement you can either argue on its necessity or abide to it. But now you can at least find a reference to a research program intended to test if there is a reason supporting this request.
A group of researchers, knowing the limitations but unable to find on the subject precise indication of accepted Standards, undertake a testing program intended to verify, one way or the other, the influence of actual simulated cut and repair cycles on the properties of a welded joint.
You will find the summary in the February 2012 Issue of the Welding Journal at page 25.In the specific case the test was performed on low carbon steel, ASTM A 283 GrB, flat plates 3/8 in. (9.5 mm) thick.
Test pieces were welded together using direct current, with the gas metal arc welding (GMAW) process, in the flat (1G) position, with a wire of 1.2 mm diameter, type ER 70S-6 per AWS Specification A5.18, recommended for welding low-carbon steel. The shielding gas was 75% argon and 25% carbon dioxide.
Six equal test pieces 200 mm wide ׳ 440 mm long were welded after having been prepared with a 60 deg. bevel, manually cut with an oxyacetylene torch and cleaned with a grinding disk. After the face of the specimens was welded, the root was backgauged with a file and rewelded.
The first specimen was put aside for testing. The remaining specimens were cut with the same methods and rewelded. The second specimen having one weld and one repair weld after cutting was put aside for testing. The other specimens followed the same procedure. The third had one weld and two repairs, the fourth one weld and three repairs, the fifth one weld and four repairs and the last one had one weld and five repairs.
Test pieces removed from the six specimens were tested for bending, ultimate tensile, impact, elongation, average grain size, and metallographic structure of the HAZ.
The results showed a remarkable homogeneity, without dramatic conditions likely to alert the researchers of dangerous worsening of basic properties. The conclusion reached in this program was that welding can be performed safely on the same area at least six times (one weld and five repairs) on low-carbon steel.
My comment is that the conclusions may be correct for applications reflecting in all details the procedures of this research. It would be risky to extend them to different situations.
Interested readers are urged to seek the original article reported above.
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Controlling Distortion
[From PWL#104 - Section 3]
From time to time I get queries trying to locate parameter changes capable of reducing distortion while welding. The following, besides other queries, illustrate the kind of questions on this argument:
1) - "I need to do some extensive aluminum welding on a cast outboard block for modification purposes. I have a Lincoln square wave tig 255. I'm experienced in welding from thin Alu sheets to the much thicker ones and different parts etc.
I've been told to watch for warping/distortion when welding Aluminum that extensively. My question now is what can I do to reduce these risks of distortion or warping?"
2) - "We have a storage tank (18000m3, floating roof, type of metal A283C, diameter of tank 44m approximately, height 13m). Thickness of bottom 9mm. Thickness of floating roof 7mm. Thickness of shell (18,16,14,12,8,8,8)mm.
When we weld the tank by using submerged arc welding technique (electrode spec. EH12K, DIA 3mm,4mm), we notice distortion in welding joint in bottom 9mm and floating roof 7mm andshell at thickness of 12,10&8 mm. Please advise me what is the proper electrode and flux to weld this tank without causing distortion in welding joint."
My standard answer is as follows: "Unfortunately, distortion problems are among the most difficult and intractable of welding practice. Contrary to what you may think they will not go out by a simple change of electrode or flux.
You may wish to see my page
http://www.welding-advisers.com/Welding-distortion.html
In general the problem is attenuated by careful planning of the weld sequence and by limiting heat input."
What this means in practice is that a complete description of the structure must be secured and that a logical sequence must be established to limit concentrating heat input in a limited area.
This analysis is best done by an experienced welding engineer capable to calculate heat input based on used parameters and to exploit fabrication sequences so as to minimize residual stresses. In certain situations it may be possible to straighten out deformed plates or profiles.
See also PWL#104B.
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Brazing with Nickel AWS BNi-2/AMS 4777
[From PWL#105 - Section 3]
A quite common question from shops using AWS BNi-2/AMS 4777 nickel base filler brazing alloy to join elevated temperature resistant alloys in vacuum furnaces, refers to the frequent appearance of a center crack right through the brazing material.
ANSI/AWS A5.8M/A5.8:2011
Specification for Filler Metals for Brazing and Braze Welding Edition: 10th
American Welding Society / 17-Jun-2011 / 62 pages
Click to order.
The brazing range of this filler metal is given as 1010-1175 0C (1850-2150 0F), relatively low, due to melting point depressants included in its composition.
The added elements performing this function (boron, silicon, phosphorus) also reduce the ductility of the brazing alloy. As the solidification occurs in the direction from the outside toward the central part of the brazing gap, and as these elements are the last ones to freeze, it so happens that their concentration is higher in the center.
The location of concentration of those elements is also a weaker point because of their reduced ductility, prone to cracking in service but also, occasionally, during solidification.
If the capillary clearance existing at the brazing temperature results larger than 0.1mm (0.004"), then there are good chances that the brittle constituents solidify at the joint center, visible in a metallographic section as a dark line, indicating a continuous layer likely to crack.
If however the said clearance is smaller than that, the brittle parts solidify preferably as separated islands in a more ductile matrix, capable of sustaining minor strains without cracking.
Therefore, for successful brazing with this brazing alloy, besides all other precautions, it is essential to control the actual capillary gap at brazing temperature, to keep it consistently smaller than 0.05mm (0.002").
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