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ssc-367 - Ship Structure Committee

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The S-N curves that can be used directly with the nominal stresses<br />

most often apply to ship structuredetails. Munse’s SSC-318 report<br />

(Reference 1.3) documents the S-N curves for 69 ship structure<br />

details and refers to earlierwork by Jordan and Cochran (Reference<br />

7.2) on in-service performance of ship structure details.<br />

Tubular offshore components have more complex geometries and are<br />

subjected to corrosive ocean environment, requiring careful<br />

assessment of all parameters contributing to fatigue failure and<br />

selection of appropriateS-N curves.<br />

Many design, fabrication and in-service factors affect the fatigue<br />

lives of details/joints. Fatigue cracks in welded joints often<br />

initiate at weld discontinuities introduced during fabrication.<br />

Weld quality problems that contributeto the degradation of fatigue<br />

strength include:<br />

●<br />

●<br />

●<br />

●<br />

●<br />

Planar defects in the body of the weld<br />

Incompletepenetration<br />

Imperfectweld root quality<br />

Imperfectweld toe profile<br />

Development of an embrittled heat affected zone (HAZ)<br />

Fatigue assessment requires definition of the number of applied<br />

stress cycles (N). Welded details/joints subjected to repeated<br />

cyclic stresseswill go through several stages of crack growth. For<br />

each hot-spot stress range (s), failure is assumed to go through<br />

three stages:<br />

●<br />

●<br />

●<br />

First discernible surface cracking (Nl)<br />

First through-wall cracking (N2)<br />

Extensive cracking and end of testing (N3)<br />

Ideally, cracks should be large enough to detect, yet not large<br />

enough to cause failure and alterationof load path. To ensure that<br />

cracks are repairable, the number of cycles to failure in fatigue<br />

7-3

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