Simulation testing of the shipping package mock-ups under the impact of a falling aircraft engine. Part 2
Authors: Kazantsev A.G., Abramov V.V., Petrov O.M., Radchenko M.V.
Published in issue: #2(158)/2025
DOI: 10.18698/2308-6033-2025-2-2420
Category: Mechanics | Chapter: Mechanics of Deformable Solid Body
The impact of a falling down aircraft is included as an external event in analyzing accidents in the transportation and outdoor storage of the shipping packages (SP) with the spent nuclear fuel. Part 2 presents a methodology for testing the SP set-ups depending on the impact type and taking into consideration technological defects in the SP body. In accordance with the proposed methodology, an artificial crack-like defect is created in the set-up body in the zone of the maximum tensile stresses to justify the SP integrity. Its dimensions are determined by technological defects in the forgings and welds approved in the SP manufacture, set-up scale, and dispersion of the fracture toughness characteristics in the body material. Conservatism of the simulation test results is ensured by the fact that a probability of the set-up failure with an artificial defect exceeds a probability of the full-scale SP failure. Using the master curve concept makes it possible to assess probabilities of the full-scale SP failure and of the reduced set-up dimension depending on the test temperature. The paper shows that the 09N2MFBA-A steel used in manufacturing the SP body provides the high dynamic fracture toughness values and ensures the SP integrity at the temperatures as low as –60°С.
EDN YGFSQN
References
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