In the previous paper on some behaviors of rubber vibration absorber in the torsional fatigue test, we reported the relation between the fatigue life and the hardness of the specimen. Here we want to explain more in detail the fatigue cracks under various test conditions and the fatigue life.
The test was carried out for specimens 30mm. in diameter and about 5mm. in length using the hysterograph.
The obtained results were as follows:
(1) The fatigue crack observed in the torsional test was produced in the direction of the angle about twice that calculated from the shearing angle on the surface of the specimen.
(2) The fatigue crack observed on the specimen which was given an initial compression was making an angle of about 25 degrees with the pasted plane and developed obliquely into the interior forming a cone. Furthermore, if we compressed the specimen and cut off the protruding part along the cylindrical surface connecting the circumferences of the pasted parts, then we observed that the angle between the pasted plane and the tangential plane of the depressed part was about 25 degrees.
(3) In the case of the fatigue test which was carried out on the specimen given either initial tensile or compressive deflection, the amplitude of the torsional moment either decreased or increased compared respectively with the value obtained for the specimen which was not given any initial deflection. The fatigue life, that is the repeated cycles until the crack appeared, increased or decreased for the cases respectively.
(4) The fatigue life of the specimen was very long in the case where the protruding part produced by the initial compression was cut off along the surface connecting the circumferences of the parts. For example, under the same shearing angle, even if the specimen undergoes the same amplitube of the torsional moment, the fatigue life of the specimen given the abovementioned operation was about three times longer compared with the specimen which was not given any intial compression.
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