9S4967 BUSHING Caterpillar parts
D4D, D7F, D9G, D9H
Rating:
Alternative (cross code) number:
CA9S4967
9S-4967
9S4967
CA9S4967
9S-4967
9S4967
Weight: 0.01 pounds 0 kg.
TRACK-TYPE TRACTOR,
Information:
Torsional Fatigue
Torsional fatigue failures are usually the result of fatigue of the crankshaft which is caused by excessive torsional vibration. Under normal conditions, the vibration damper will keep this torsional vibration from becoming excessive. If the vibration damper has failed, this excessive vibration can cause a torsional fatigue failure in the crankshaft.
The failure usually begins on a journal at a point of stress concentration, such as a flaw, crack, oil hole or lightening hole. It then progresses into a torsional fatigue failure. The fracture is generally at a 45° angle through the oil hole. It usually occurs about 2/3 of the way down the crankshaft from the damper.
Illustration 1 shows two examples of a torsional fatigue failure. The fracture usually goes in one of two directions as shown by the lower illustration in Illustration 1.
Illustration 1. Failure caused by torsional fatigue.Few crankshafts fail from true torsional fatigue, primarily because the vibration damper keeps the torsional vibrations within a safe limit. If the vibration damper does fail, normally the timing gears will fail before the crankshaft is damaged.
The following are some of the causes of crankshaft failures due to true torsional fatigue:
1. Defective or failed vibration damper.2. Failed torsional coupling.3. Improper applications of the engine. All engines in Caterpillar vehicles and packaged generator sets can be operated at approved loads and speeds without a torsional fatigue failure. Caterpillar engines in other applications will give acceptable operation if a torsional vibration analysis is made on the complete system before installation. This analysis can be performed by Caterpillar. For more information, see the Special Additions section of the Engines Price List.4. A large inclusion or groups of inclusions (foreign material) in or under the journal surface. These inclusions are generally characterized by a short longitudinal fracture with 45° fractures at each end as shown in Illustration 2. Many inclusions are not harmful. For more information, see Guideline For Reusable Parts, "Inspection Of Crankshafts For Cracks," Form No. SEBF8039.5. Nicks, large scratches and cracks in the oil hole. See Engine Bearings And Crankshafts, Form SEBD0531, Section 5, for more information and illustrations on crankshafts with nicks, large scratches and cracks.
Illustration 2. Torsional failure because of large inclusions.Bending Fatigue
Crankshaft failures that are the result of bending fatigue usually start at a point of stress concentration in the fillet. The bending forces on the crankshaft cause a small crack to form which moves through the web between the rod journal and the adjacent main journal. See Illustration 3.
Illustration 3. Failure caused by bending fatigue.The normal causes of a stress concentration in the fillet are: 1. Sharp nick, notch, or scratch.2. Inclusion.3. Grinder burn.4. Wrong fillet (radius too sharp, incorrect finish).5. Wrong or no shot peen operation after grinding. See Guideline for Reusable Parts, "Procedure to Grind Crankshafts," Form SEBF8047.6. Main bearing failure. The main journal is no longer supported correctly and the bending forces increase across the unsupported journal. The result is a bending fatigue failure.7. Misalignment of the crankshaft in the block. This
Torsional fatigue failures are usually the result of fatigue of the crankshaft which is caused by excessive torsional vibration. Under normal conditions, the vibration damper will keep this torsional vibration from becoming excessive. If the vibration damper has failed, this excessive vibration can cause a torsional fatigue failure in the crankshaft.
The failure usually begins on a journal at a point of stress concentration, such as a flaw, crack, oil hole or lightening hole. It then progresses into a torsional fatigue failure. The fracture is generally at a 45° angle through the oil hole. It usually occurs about 2/3 of the way down the crankshaft from the damper.
Illustration 1 shows two examples of a torsional fatigue failure. The fracture usually goes in one of two directions as shown by the lower illustration in Illustration 1.
Illustration 1. Failure caused by torsional fatigue.Few crankshafts fail from true torsional fatigue, primarily because the vibration damper keeps the torsional vibrations within a safe limit. If the vibration damper does fail, normally the timing gears will fail before the crankshaft is damaged.
The following are some of the causes of crankshaft failures due to true torsional fatigue:
1. Defective or failed vibration damper.2. Failed torsional coupling.3. Improper applications of the engine. All engines in Caterpillar vehicles and packaged generator sets can be operated at approved loads and speeds without a torsional fatigue failure. Caterpillar engines in other applications will give acceptable operation if a torsional vibration analysis is made on the complete system before installation. This analysis can be performed by Caterpillar. For more information, see the Special Additions section of the Engines Price List.4. A large inclusion or groups of inclusions (foreign material) in or under the journal surface. These inclusions are generally characterized by a short longitudinal fracture with 45° fractures at each end as shown in Illustration 2. Many inclusions are not harmful. For more information, see Guideline For Reusable Parts, "Inspection Of Crankshafts For Cracks," Form No. SEBF8039.5. Nicks, large scratches and cracks in the oil hole. See Engine Bearings And Crankshafts, Form SEBD0531, Section 5, for more information and illustrations on crankshafts with nicks, large scratches and cracks.
Illustration 2. Torsional failure because of large inclusions.Bending Fatigue
Crankshaft failures that are the result of bending fatigue usually start at a point of stress concentration in the fillet. The bending forces on the crankshaft cause a small crack to form which moves through the web between the rod journal and the adjacent main journal. See Illustration 3.
Illustration 3. Failure caused by bending fatigue.The normal causes of a stress concentration in the fillet are: 1. Sharp nick, notch, or scratch.2. Inclusion.3. Grinder burn.4. Wrong fillet (radius too sharp, incorrect finish).5. Wrong or no shot peen operation after grinding. See Guideline for Reusable Parts, "Procedure to Grind Crankshafts," Form SEBF8047.6. Main bearing failure. The main journal is no longer supported correctly and the bending forces increase across the unsupported journal. The result is a bending fatigue failure.7. Misalignment of the crankshaft in the block. This
Cat SIS web machinery list:
Parts bushing Caterpillar catalog:
1183757
BUSHING
315B, 933, 933C, D3C III, D4C III, D5C III
315B, 933, 933C, D3C III, D4C III, D5C III
4342986
BUSHING AS
301.7D CR
301.7D CR
4397939
BUSHING
301.7D CR
301.7D CR
4385870
BUSHING
301.7D CR
301.7D CR
4385857
BUSHING
301.7D CR
301.7D CR
4220731
BUSHING
308E SR
308E SR
8S9543
BUSHING
140G, 627, 637D, D6C, D7G
140G, 627, 637D, D6C, D7G
7K1103
BUSHING ASSEM. (.040" oversize)
225, 941, D4D, D4E
225, 941, D4D, D4E
7K1089
BUSHING
215, 215B, 225, 561M, 561N, 939, 939C, 941, 943, D4D, D4E, D4E SR, D4H, D4H XL, D4HTSK III, D5C III, D5G, D5K LGP, D5K2 XL, D5M, D5N, D6K LGP, D6K2, D6K2 LGP, PL61, PM-201, PM-565, PM-565B, PR-750B
215, 215B, 225, 561M, 561N, 939, 939C, 941, 943, D4D, D4E, D4E SR, D4H, D4H XL, D4HTSK III, D5C III, D5G, D5K LGP, D5K2 XL, D5M, D5N, D6K LGP, D6K2, D6K2 LGP, PL61, PM-201, PM-565, PM-565B, PR-750B
7K1102
BUSHING ASSEM. (Standard)
225, 941, D4D, D4E
225, 941, D4D, D4E
9K4061
BUSHING
215, 225, 323D LN, 941, D4D, D4E, D4E SR, PM-201, PM-565, PM-565B, PR-1000
215, 225, 323D LN, 941, D4D, D4E, D4E SR, PM-201, PM-565, PM-565B, PR-1000
7K2020
BUSHING (Master)
215, 225, 323D LN, 941, D4D, D4E, PM-201, PM-565, PM-565B, PR-1000
215, 225, 323D LN, 941, D4D, D4E, PM-201, PM-565, PM-565B, PR-1000