Page - 3 Volume 5 , Issue 6 Dt - 01-06-2005 | ENB History | Home | << Page 2 | Page 4 >>
 
Fatigue Failure: Why, how and when?
A guide to prevention and rectification


Fatigue may be defined as the formation and gradual propagation of a crack through a material under conditions of varying tensile stress. The stress must be tensile, cracks will not open up during compressive stress, and it must vary with time, fatigue cracks do not propagate under static tensile stress.

A fatigue-failed component exhibits two distinct types of surface on its fractured faces.

1. There is the shell line marks of the fatigue crack growth, this may actually be polished due to the rubbing of the crack faces together, and
2. The very rough section of final failure where the remaining material was unable to withstand the applied load causing final failure in a brittle manner.

Typical Fatigue crack propagation
Welds are particularly susceptible to fatigue cracking not because they are highly loaded but because
1. Slag and other defects they contain act as stress raisers.
2. The presence of residual tensile stress in a weld also increases the total value of tensile stress when load is applied.

Following can cause these stress raisers:
1. Internal material defects such as slag, gas porosity, and existing cracks, but they may also be
2. Due to sharp changes in section caused by poor design or surface damage.
3. Surface damage during overhaul causes stress raiser effects whilst
4. Over tightening of bolts induces a higher static stress

In some situations such as piston crown it may be very difficult to detect cracks due to scale and other deposits. Likewise during the ballast tank inspections the areas usually that have cracks can be short-listed based on the above criteria. The stress risers must be identified and a closer inspection in such areas should be carried out.

DO WHATEVER YOU CAN TO TRY AND AVOID SUCH FAILURES!!

- Article contributed by Technical Superintendent K Srinivas Patnaik.

 
Page - 3 Volume 5 , Issue 6 Dt - 01-06-2005 | ENB History | Home | << Page 2 | Page 4 >>