2014
DOI: 10.3221/igf-esis.30.41
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In-service fatigue cracking of the propeller shafts joined by a spline-pinned construction to the engines of AN-24, AN-26, and IL-18 aircrafts

Abstract: ABSTRACT. The paper delivers a critical review of the research data on the crack initiation and crack growth patterns characteristic of the components of the spline-bolted joints between the propeller shaft and reducer shaft at An-24, An-26, and Il-18 aircrafts. Cracks in the shafts nucleated because of reduced bolt-fastening force. Actually, the bolt (bolts) failed first (also by fatigue) and then fatigue cracks nucleated and grew in the shafts, the spline surface fretting zones and/or sharp edges of the atta… Show more

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“…Research conducted by the author of [1] demonstrated that the measurable traces of damage at the surface of the examined elements occur as early as at approximately 10 3 load cycles. When the number of cycles becomes greater, wear intensity increases as long as the cycle number reaches over 10 6 .…”
Section: Resultsmentioning
confidence: 99%
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“…Research conducted by the author of [1] demonstrated that the measurable traces of damage at the surface of the examined elements occur as early as at approximately 10 3 load cycles. When the number of cycles becomes greater, wear intensity increases as long as the cycle number reaches over 10 6 .…”
Section: Resultsmentioning
confidence: 99%
“…The sample wear test parameters were as follows: -revolutions: n = 1360 rpm -load on the sample: Q = 550 N -number of cycles: 7×10 6 .…”
Section: Test Methodologymentioning
confidence: 99%
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