Usage:
CONFIDENTIAL TIBU4580-00
TECHNICAL INFORMATION BULLETIN |
June 22, 2005 |
Engines |
3512B (1PW) 3516 (73Z) 3516B (9AN, 2FW) |
Component Code(s) 7060 |
SUBJECT: Petroleum generator set packages exhibit cracks on the base rails as well as the generator mounts.
PROBLEM:
On 3512/3516 Petroleum generator set packages installed on off-shore oil rigs, cracks may be found on the rails, left and right side rear engine mounts, and the left and right side generator mounts.
3512B 7W7915 Base Assembly
- 7W7919 Base Assembly
3516B 7C-7123 Generator mounts
From the period January 1985, through June 2005, the possibility exists petroleum generator set bases may crack. Refer to Illustrations 1 through 3.
Illustration 1.
Illustration 2.
Illustration 3.
SOLUTION:
During preventive maintenance and routine inspections, cracks may appear at the rear engine base mount and generator mounts. The following weld procedure should be used in order to repair the cracks.
Note: When corresponding with Caterpillar regarding this problem, be prepared to provide the specific site information listed in Table 2.
Welding on Machines and Engines with Electronic Controls
Proper welding procedures are necessary to avoid damage to electronic controls. The following steps should be complied with when welding on any machine or engine with electronic controls.
Engine Preparation
- Turn off the engine. Place the engine start switch in the OFF position.
- If equipped, turn the battery disconnect switch to the OFF position. If there is no battery disconnect switch, disconnect the negative battery cable at the battery or negative 24V power supply.
- Connect the welding ground cable directly to the actual base to be welded. Clean the area where the clamp is applied to ensure a good current path. Clamp the cable as close as possible to the weld in order to reduce the possibility of current damage to the drive train bearings, generator bearings, electrical components (such as ground straps), and other engine/generator components.
- Protect any harnesses from welding debris or splatter.
- Use the following welding procedure to weld materials together.
Note: This is the position of the machine Service or storage.
_________________________NOTICE_________________________________
Do not use electrical components (ECM?s or ECM sensors) or electronic component grounding points for grounding the welder.
________________________________________________________________
PROCEDURE
Step 1: Prepare for Welding
- Remove the crack, creating a groove weld joint geometry. (Remove material 25.4 mm (1 inch) beyond the end of the visible sign of crack). This may be accomplished using an arc gouge or by grinding.
- Shape the weld joint such that the welder will have good access to the root and can produce a continuous full penetration weld.
- Clean the grooves by removing all residual carbon, grease, oil, etc. If arc gouging is used, take care to remove all of the residual base metal. The melted base metal has a tendency to adhere to the un-melted base metal and is difficult to remove by grinding. A pneumatic chipper will remove this material.
- Remove 12.7 mm (.50 inch) of the outer edge of the gusset (point) by grinding. This will result in a vertical surface.
- Remove the paint, by grinding, on the top surface of the plate at least 50.8 mm (2 inches) from the weld joint.
- Visually inspect to make sure the entire crack is removed.
- Use an NDT process, such as a dry mag with a yoke, to verify that the entire crack is removed.
Note: If by chance the cracks are originating and propagating thru the center of a fillet weld, simply remove the fillet weld and replace it with a fillet weld of the same size. Do not increase the size of the fillet weld. Grind the toe of the fillet weld to produce a smooth transition to the base metal.
Step 2: Weld Repair
- Weld the joint with a low hydrogen process and a matched electrode. See Table 1.
- The fillet welds along the sides of the angled gusset should extend 12.7 mm (.50 inch) beyond the end of the gusset.
- Clean the weld surface between each pass.
- Visually inspect each pass for surface defects.
- See Illustrations 4 and 5 for weld details and to ensure that the final weld is within the fillet size requirements of these drawings, (i.e., Do not add multiple passes making the fillet size larger than plan.).
Note: The end of the gusset must remain open and not welded.
Note: As a rule of thumb, the "more overwelded" the fillet (any) weld, the poorer the geometry; the higher the stress concentration, the shorter the fatigue life.
Illustration 4. Engine Mount
Illustration 5. Generator Mount
PRODUCTION WELDS FOR ENGINE AND GENERATOR MOUNTS
ALLOWED FILLER METAL |
|
AWS A5.1 |
E7018 |
AWS A5.18 |
ER70S-2, ER70S-3, ER70S-6, ER70C-6M |
AWS A5.20 |
E70T-1, E71T-1 |
Table 1.
Note: The open root, grove weld procedure used must meet or exceed the following specification and the welder should be trained and certified per the following specification for the welding procedure used for the repair:
- AWS D1.1 Structural Welding
Step 3: Post Weld Inspection
- Visually inspect the weld for surface discontinuities and defects.
- The weld should have reinforcement above the surface of the base plate.
Note: If any defects are found, repeat the process starting at Step 1.
Step 4: Post Welding Processing
- Grind the surfaces of the weld smooth with the top surface of the base metal.
- Maintain the original contour of the base material.
- Use a NDT process, such as a dry mag with a yoke, to verify that there are no cracks in the weld.
Note: Examiner certification shall be in accordance with the Contractor?s written procedures, which shall use American Society for Non-Destructive Testing Recommended Practice No.SNT-TC-1A as a guide.
Step 5: Establish a Periodic Inspection Plan for Repaired Region
At Each regularly scheduled engine Preventive Maintenance service interval (at a minimum), perform the following action:
- Inspect repaired region(s).
INSTALLATIONS WITH CRACKED BASES
The information in Table 2 is requested from each site that has experienced a base crack. This information should be forwarded to:
Murphy_Mike_J@CAT.com
1. ENGINE SERIAL NUMBER |
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2. GENERATOR COUPLING PART NUMBER |
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3. GENERATOR ALIGNMENT VERIFIED |
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4. VIBRATION READING ? ENGINE DATA SHEET 73.1 OBTAIN BEFORE AND AFTER REPAIR |
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5. BLOCK LOADING PROFILE |
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6. HOURS ON ENGINE |
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7. HOURS ON COUPLING BOOT 5N-3272 NOTE: IT IS RECOMMENDED COUPLING BOOT 5N-3272 BE CHANGED OUT EVERY 5000 HOURS |
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8. IF THE COUPLING BOOTS 5N-3272 WERE CHANGED, WHAT WERE THE HOURS AT TIME OF REPLACEMENT. |
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9. VERIFY ENGINE ISOLATORS HAVE BEEN ADJUSTED FROM THE SHIPPING CONDITION |
|
10. LOCATION OF WELD CRACKS - DIGITAL PICTURES REQUIRED: ENG REAR RIGHT ENG REAR LEFT GEN MOUNT RIGHT GEN MOUNT LEFT |
Table 2.
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