ASME PRESSURE VESSELS
The scope of this presentation is to present basic information and understanding of the ASME code for the design of pressure vessels for the chemical and process industry as applicable in the United States and most of North and South America.
A TO Z OF PRESSURE VESSELS - II
In this article, the topics are arranged according to the sequence of manufacture of a pressure vessel under the following assumptions:
- The dished ends and cones are bought from outside with the material supplied by the vendor under proper certification.
- All plates and piping materials, including but not limited to pipes, elbows, flanges, studs/ bolts and nuts, gaskets, etc., are bought out items from reputed vendors with proper certification.
RAW MATERIAL INSPECTION
Upon receipt of the material at the stores, the quality assurance and control (QAC) department will be informed through their intimation note. In the meantime, procurement department will forward the relevant documents pertaining to the received item to QAC to facilitate the inspection with a copy of the intimation marked to the planning department for information processing. Until the inspection is carried out, the raw materials are kept in the incoming material inspection bay of the stores for all materials other than plates and pipes, which are stored separately in the open yard attached to the stores.
Those items having undergone inspection will have either a green, yellow or red sticker. Green indicates accepted material, yellow is for items under hold, and red marks rejected items. Items under hold need clarifications from other departments as to their acceptability when a discrepancy in supply is observed. This is intimated to the concerned department in detail by an inspection note. The matter is to be resolved by the concerned department(s), and if the item is to be accepted, QAC should be notified. Until such time, the item will be under hold in an area designated for the purpose.
All accepted materials will have a green sticker implying that they meet all the requirements mentioned in the purchase order (PO) as well as the applicable codes and items supplied tally with the certificates furnished by the vendor. Those items that do not meet the PO or code requirements shall be rejected and are given a red sticker. The reason for rejection are given in the inspection note to be communicated to the vendor by the procurement department, and at the same time the material will be returned to the vendor by the stores department.
Each dished end shall be checked against its certificate. Then the outside circumference, inside diameter (ID) at four locations, thickness at straight flange (SF), and inside depth are measured and cross checked with the measurements given in the certificate. The heat number and the identifications certified by the third party inspector at the manufacturer’s end are also verified. If these are in order, the physical verification part of the inspection is over. The certificate is then verified for the material specification, type of tests, heat treatment etc. When these parameters have been verified per the PO and the applicable codes, the item is accepted.
Measure the possible physical dimensions, especially the thickness. Correlate the identification found on these items with the certificates furnished. If these are in order, the certificate is verified against PO and code requirements. If these are also in order, the items can be accepted.
Pipe Fittings/ Flanges
Record all possible dimensions and verify against those given in the applicable standards. Cross check the identification found on the items to that given in the certificate. Verify certificate against PO and code requirements.
Fasteners and Gaskets
Select random samples and subject them to a dimensional check. Correlate certificates to the identification given to the lot. Then check the certificates for compliance to PO and code requirements.
Identify the shell and correlate it to the certificate. Measure the outside circumference at both ends, the length of the shell, as well as its thickness at a few locations (Please refer to the previous issue of the newsletter). These are to be cross-checked with those given in the certificates. Further, if non-destructive testing is involved, its compliance and acceptability are also to be verified from the certificate.
Identify the cone to a particular certificate by identifying the actual stamping details on the plates, and check measurements as described earlier in the previous newsletter. Cross-check dimensions to those given on the certificate. Subsequently verify the certificate for compliance to PO and code requirements.
MARKING OF SHELLS TO SUIT HEADS AND IDENTIFICATION
This section applies when the inside diameter of the shell and the head matches. Take the outside circumference of the head at SF. Measure thickness of the head at SF from at least 12 points and take the average. Calculate the average ID of the head. Take the actual thickness of the shell plate. Find the mean diameter of the shell by adding the measured thickness to the calculated ID of the head. Based on this, find the mean circumference of the shell.
- Required ID = 98 inches (assuming that the ID of the shell and head match)
- Thickness at SF = 0.75 inch (per requirement)
- Average thickness at SF taken at 12 points (actual) = 0.83 inch
- Measured outside circumference of the head at SF (actual) = 315 inches
- Calculated ID of head = (315/π) – (2 x 0.83) = 98.58 inches
- Let the shell thickness required be 0.623 inch and the actual be 0.65 inch. The calculated mean circumference of the shell is (98 + 0.65)π = 312 inches.
Spread out the shell plate and mark the length 7918 mm as shown in Figure 1 and cross check the diagonals D1 and D2. The difference between D1 and D2 shall be within ±2 mm. If this is not possible using the mill cut edge of the plate, the plate must be squared again and the length and breadth re-marked. If the diagonals are within the tolerance, the plate identification has to be transferred to a corner of the shell plate with a personal identification stamp of the inspection engineer who witnesses the transfer of identification.
ADD Figure 1: Shell Marking
INSPECTION OF PLATES AFTER CUTTING AND EDGE PREAPRATION
The most commonly used process for the cutting and edge preparation of carbon steel plates is oxyacetylene cutting, and that for stainless steel plates is plasma-arc cutting. In both cases, the cut edges will have excessive oxide deposition that is black in color. This has to be removed by grinding, and the acceptable level is at least 1 mm deep into the parent metal so that the detrimental effects due to the presence of oxides shall be completely removed.
After grinding, the cut edges shall be examined visually for any defects like lamination or any other local defects due to improper cutting parameters. In cases needed, visual examination of cut edges may be supplemented by liquid penetrant testing (LPT). When cuts are found satisfactory, the piece can be released for bending.
BENDING OF PLATES
The shell plate will have more strength in the direction of rolling; hence, as far as possible, the direction of bending of plate shall be same as that of the original direction of rolling, which is in the direction of the length of the plate. Once the shell plate is fed into the bending machine, first both the ends are pressed to the required shape – this process is called pre-pinging (See Figure 2). After pre-pinging, the profile at ends is checked using a template and, if satisfactory, full bending is carried out. Usually, the bending is carried out in a few stages so that the elongation of the shell will be negligible and no further trimming of the plate will be needed.
ADD Figure 2: Pre-pinging of Plate Edges
The template for checking the profile during bending shall be as per the requirements of UG-29.2, namely twice the arc length obtained from chart UG-29.2 (See Figure 3). As a rule of thumb, if we take a segmental template that subtends 20o at the center, it will definitely meet requirements of the ASME clause.
ADD Figure 3: UG-29.2
Set-Up for Welding of Long Seam and Inspection
Upon completion of bending, the longitudinal seam is fitted for welding. Please refer to the August 2013 issue of the newsletter for the dimensions that shall be recorded for the shell. Apart from those dimensions, the profile all around the shell shall be checked and deviation in profile form the template beyond acceptable levels shall be repaired. Additionally, the V-configuration shall be checked for its compliance to the design and its uniformity throughout the length of the seam (i.e., gap, root face or throat, V angle, etc.).
Precautions to Control Distortion
Distortion of weld joints is more problematic in the case of the longitudinal seams when compared to the circumferential seams. The usual types of distortion that can take place at a long seam are either peaking in or peaking out. Given here are a few proposals for the reduction of distortion whose judicious application will yield positive results.
- When the thickness of the shell plate is less than 5/8 inch, single-V double welded joints are recommended. In such cases, the groove shall be provided as far as possible at the inside.
- When the thickness of the shell plate is greater than 5/8 inch, double-V joints are recommended. In this case, as far as possible, the joint configuration shall be unequal V with the major V on the inside.
Qualified welders shall carry out the welding as per approved procedures. However, every weld has the potential for distortion – it can’t be avoided. If judicious precautions are taken, distortion is easily brought under acceptable limits.
The edge preparation has a very significant role in controlling distortion. When a rational design of the weld design is made, the quantum of weld metal is to be minimized, so the quantity of weld on either side of the weld can be balanced. Obviously, the associated distortion will also be less. The selection of single or double-V joints for various thicknesses of shell plate have already been discussed. Even though the V-sizes and angles are stipulated by the Code, where to apply them and where to do the first welding, etc., are not addressed.
ADD Figure 4: Recommended V-Joint Preparation
Tack Welding of Joints
Tack welding on the seam or the use of clamps and wedges may be resorted to for holding the joint in position. Provided a qualified welder does the tack weld, using a qualified welding procedure under the requisite conditions of preheat, it can be a part of the actual weld. In that case, it’s starting and stopping points shall be properly prepared by grinding prior to full welding. Tacks shall be provided at a spacing of 8 to 10 inches, with the length of tack ranging from 1 inch to 1.5 inches. The holding devices used for maintaining the shape of shells shall be retained until the welding from the major-V side is completed, as the distortion is maximum in the first few passes of the weld.
Run-in and Run-out of Plates
Two pieces of plate of 2 to 4 inch length shall be provided at the beginning and end of each seam, preferably with the same V-configuration. This will help the welder to start the weld from the run-in plate, and by the time the welder reaches the shell, welding will be stabilized and the weld on the shell will be free from defects. This is possible only for longitudinal seams and a serious bearing on the quality of the weld at the start and end of each longitudinal seam, which eventually turn out to be T-joints.
Stiffeners to maintain Circularity
All sections shall be provided with spiders for maintaining the circularity while rotating the shells on the floor as well as on rotators. At least four spiders shall be given at both the ends of the shell avoiding the longitudinal seam area. The spiders can be of angle iron preferably with adjustment provision to maintain the circularity precisely. Apart from these spiders meant for maintaining circularity, one additional stiffener shall be provided on the weld with a preset as shown in Figure 5.
Precleaning of Welds
A weld seam shall be thoroughly cleaned and shall be free from rust, grease, mill scale, or any other foreign material not only on the weld but also on either side of the V-groove to a width of at least 1 inch. This should be done meticulously on both sides of the seam prior to the start of the weld on the first side. The use of a circular wire brush attached to a grinding machine could produce the desired results, whereas the simple wire brush cleaning is not sufficient as specified in many of the welding procedures.
ADD Figure 5: Restraint on Long Seam for Welding from Outside
Based on the material of the shell section and also on the WPS, the joint may have to be preheated prior to welding. This is given in the Appendix R of the ASME Section VIII, Division 1. Depending on the thickness of the plate to be welded and the temperature to be attained, suitable attachments shall be made to achieve the same. The maximum length of the attachment needed is 40 inches, as it can be moved in the direction of the weld as the weld progresses. The heating shall be done from the outside when the welding is done from inside and vice versa.
For a longitudinal seam of approximately 5 to 6 feet long, the weld can start from one end of the seam and finish at the other. While setting the joint for such welding, care shall be taken to see that the gap provided at the starting end of the longitudinal seam shall be exactly as per the drawing, and toward the closing end it shall be increased a bit. For along seam of length 5 to 6 feet, 0.8 inch excess gap at the closing end can be given which will shrink to the desired level as the weld progresses towards the closing end, as shown in Figure 6.
When the length of the seam is more than 6.5 feet, it is better to adopt a staggered welding sequence. For a weld seam of about 13 feet, it is recommended to start welding from one end to a length of about 3 feet and next from the other end for about the same distance. The remaining 6 feet left at the center is welded last.
After every pass, the weld has to be cleaned using proper tools to remove all slag and spatters from the V-groove. In most cases, power brush cleaning after chipping the slag is sufficient. However, in case of the root run, it may call for grinding, as it is difficult to remove slag from a deep groove. When the welded surface is free from slag, spatters and surface defects, it can be taken for depositing subsequent beads after checking the interpass temperature. [For any welding to go on, the welded joint shall have a minimum preheat temperature and at the same time, it shall not exceed the maximum interpass temperature indicated in the WPS]
ADD Figure 6: Longitudinal Seam Fit-Up and Sequence of Welding
In the case of longitudinal seams, it is recommended to complete the welding from inside first and then perform the back-gouging from outside. Back-gouging may be carried out either by carbon electrode gouging or by grinding alone. In the case of carbon electrode gouging, it shall be ensured that all black carbon gouge marks on the gouged area are removed by grinding into sound metal by at least 0.04 inch. This is to prevent the carbon particles from going into the molten metal, which may cause detrimental effects.
The LPT of the back-gouged joint is always useful in detecting gross defects like lack of fusion, cluster porosity, slag inclusion, etc., in the root run and hence is recommended for all full penetration welds.
Care should be taken in carrying out the back-gouging so that an unequal V-joint after back-gouging from the minor side shall never exceed half the thickness of the shell. In other words, the weld from both sides shall be almost balanced in quantum. In addition, care shall be taken to ensure that the V-width is not increased beyond that specified in the design. However, the resultant V shall have a V angle of at least 10-15 degrees.
Final Visual Examination
On completion of welds on either side, the restraints provided during welding may be removed for ease in carrying out other jobs. However, the spiders provided to maintain the circularity of shells, especially for thin shells, may be retained until the vessel is complete so that it can take loads on its own.
The weld joints shall be inspected after the completion of welding from both sides using an inside and outside template to assess the peaking in or out of the seam. If this is within the acceptable limits as per the code or client specification, visual inspection of the seam is carried out with regard to the following aspects:
- Surface finish of the weld and its uniformity according to specifications for welded surfaces permitted in UW-35. The surface of weld shall be sufficiently free from coarse ripples, grooves, overlaps, and abrupt ridges and valleys to permit the proper interpretation of radiographs.
- Reinforcement of weld shall be as per the table given in UW-35.
- Profile of welded joint
- Under cuts
- Removal of tack metals in the nearby areas.
When all these parameters are satisfactory, the weld can be released for non-destructive testing (NDT) as needed.
Non-destructive Testing of Long Seams
All seams that have undergone satisfactory visual inspection can be taken for NDT, the most prominent of which is RT. As per the applicable specification, UW-11, ultrasonic examination carried out in accordance with UW-53 may be substituted for radiography for the final closure seam of a pressure vessel if the construction of the vessel does not permit interpretable radiographs. The technique and acceptance criteria shall be in accordance with Appendix 12 of the ASME Section VIII, Div. 1 code.
Full Radiographic Testing:
The applicable sections of the code in this regard are UW-11 and UW-51. Full radiography is required when joint efficiency is considered as 1 in the design. In addition, all butt-welds in shells and heads of vessels meant to carry lethal substances and all butt-welds in shells whose thickness exceeds 1.5 inches shall also undergo full radiography.
Spot Radiographic Testing:
The applicable code is UW-52. As per the referred code, one spot on each vessel is required for each 50-ft increment of weld or fraction thereof. The minimum size of spot shall be 6 in. When such a spot RT film does not meet the acceptance criteria as specified in UW-51, two additional spots in the same weld away from the initial spot shall be taken. If these two spots are acceptable and the original spot is repaired and the new radiograph also meets the acceptability norms, the joint represented by these welds can be considered as accepted. When either of the additional spots fails to meet the requirements, the entire length of the weld represented by this weld shall be fully radiographed.
The acceptance norms in case of both full and spot radiography are as per UW-51 for linear defects, and Appendix 4 for rounded indications.
1. Practical Guide to Pressure Vessel Manufacturing, by Sunil Pullarcot
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