Thermal fatigue occurs when an engine is consistently operated under full heavy load followed by light load. The constant drastic changes in combustion temperature eventually results in thermal cracks of the piston crown.
Piston skirt cracking is usually a result of constant excessive loading of the engine and high mileage fatigue or in some cases faulty piston design. The manufacturer usually corrects the later by supplying a superseded part.
Incorrect fitting of pistons to rods can cause stress fractures, which develop into serious skirt cracking early in the life of a repaired engine. Piston skirt cracking is not a common engine fault and IS ALMOST TOTALLY ELIMINATED OUT OF MODERN PISTON DESIGN
Cracked ringlands are usually caused in detonation or pre-ignition. Detonation causes excessive combustion temperature and pressure. By design the ring lands are one of the weaker positions on a piston and can crack under this type of stress. The land can completely crack away in sections. Rings will also crack under these conditions.
: Every care has been taken in writing this information and procedures, but no responsibility can be excepted for errors, omissions or misuse of this information and procedures. The information available on this site is for your instruction only and cannot be copied for sale, © copyright 2020 UMR Engines www.engineproblem.com.au
Once the cylinder head is removed, a tell tale sign of ring wear is washing of the outer edge of the piston. At high mileage this is a perfectly natural occurrence even when strict service guidelines are adhered too. The average medium sedan generally travels around 150,000 kilometres before being affected by worn out rings. We could be considering worn out rings a premature condition anything under this mileage, depending upon driving conditions and service records.
Premature ring wear is generally caused by poor service of the air and oil filter system. Performance of rings is effected by both the quality of the air and of the oil. Driving conditions will determine if service intervals should be shortened to guarantee the protection of the engine. Wrong choice of ring material to the application can be a cause. Eg: cast iron instead of chrome top rings.
Abrasive wear is the most common cause of ring failure soon after an engine rebuild. This condition is a result of poor workmanship and can never be blamed on the parts. Close inspection of the worn rings will confirm the cause. Multitudes of vertical scratches will be visible on the rings and the piston skirt. Normally the oil ring will be extremely worn and the piston will now measure under acceptable wear specifications. The edges of all rings will be excessively sharp. The engine oil will be extremely black within the first 1000 kms. Due to the cause of this failure almost every other engine component can be effected with abnormal premature wear. The engine will be destroyed before the first 800 km engine service. Due to the nature of the abrasive material involved it will also become imbedded in the bearings resulting in abnormal crankshaft wear.
The term used to describe an engine that has accelerated ring and bore wear due to air born abrasive contamination is a "DUSTED" engine. An engine subject to air borne contamination can be destroyed in a very short period. Poor air filter service procedures, inadequate filter system, vacuum leaks, intake hose leaks, intake manifold leak and leaking PVC system etc. can all lead to excessive premature ring wear and bore wear. The cause of this wear is very evident at strip down. An initial examination of the intake manifold can reveal the contaminant as it gets trapped in blind crevices and the rough casting areas. The air cleaner tube or the engine side of the air filter may also show evidence of the contaminant. Often at first glance the inside of the intake manifold looks abnormally clean with all marks and stains polished off. Upon dismantling the engine wear is very evident on the upper bores. The compression rings will have fine vertical scratches and the bores will have a worn polished look with no hone pattern evident. The ridge left by the top compression ring will be rather excessive and often all around the cylinder, rather different to normal ridge wear. All the rings will be excessively worn as the rings are subject not only to the airborne contaminant but also to the fine iron particles as the bores and rings wear out. If an engine operates in a dusty enviroment it is important to shorten the service intervals and ensure all filtration systems are adequate and well maintained.
: Every care has been taken in writing this information and procedures, but no responsibility can be excepted for errors, omissions or misuse of this information and procedures. The information available on this site is for your instruction only and cannot be copied for sale, © copyright 2020 UMR Engines www.engineproblem.com.au
: Every care has been taken in writing this information and procedures, but no responsibility can be excepted for errors, omissions or misuse of this information and procedures. The information available on this site is for your instruction only and cannot be copied for sale, © copyright 2020 UMR Engines www.engineproblem.com.au
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