Fatigue behaviour of a laser beam welded CoCrFeNiMn-type high entropy alloy

Autor: Kashaev, Nikolai, Ventzke, Volker, Petrov, Nikita, Horstmann, Manfred, Zherebtsov, Sergey, Shaysultanov, Dmitry, Sanin, Vladimir, Stepanov, Nikita

Publikováno v: In Materials Science & Engineering A 24 October 2019 766

Probabilistic fatigue-life assessment model for laser-welded Ti-6Al-4V butt joints in the high-cycle fatigue regime

Autor: Fomin, Fedor, Horstmann, Manfred, Huber, Norbert, Kashaev, Nikolai

Publikováno v: In International Journal of Fatigue November 2018 116:22-35

Assessment of alternative joining techniques for Ti–6Al–4V/CFRP hybrid joints regarding tensile and fatigue strength

Autor: Kashaev, Nikolai, Ventzke, Volker, Riekehr, Stefan, Dorn, Falk, Horstmann, Manfred

Publikováno v: In Materials and Design 15 September 2015 81:73-81

Comparative study of mechanical properties using standard and micro-specimens of base materials Inconel 625, Inconel 718 and Ti-6Al-4 V

Autor: Kashaev, Nikolai, Horstmann, Manfred, Ventzke, Volker, Riekehr, Stefan, Huber, Norbert

Publikováno v: In Journal of Materials Research and Technology January-March 2013 2(1):43-47

Fatigue crack propagation influenced by laser shock peening introduced residual stress fields in aluminium specimens

Autor: Keller, Sören, Horstmann, Manfred, Kashaev, Nikolai, Klusemann, Benjamin

Publikováno v: Keller, S, Horstmann, M, Kashaev, N & Klusemann, B 2020, Fatigue crack propagation influenced by laser shock peening introduced residual stress fields in aluminium specimens . in A Niepokolczycki & J Komorowski (eds), ICAF 2019 – Structural Integrity in the Age of Additive Manufacturing : Proceedings of the 30th Symposium of the International Committee on Aeronautical Fatigue, 2019 . Lecture Notes in Mechanical Engineering, Springer, Cham, Schweiz, pp. 617-631, Symposium of the International Committee on Aeronautical Fatigue-ICAF 2019, Warsaw, Poland, 02.06.19 . https://doi.org/10.1007/978-3-030-21503-3_50

Laser Shock Peening (LSP) enables the generation and modification of residual stresses deep below the surface of metallic components. LSP-induced residual stress profiles provide penetration depths of compressive residual stresses in mm range, which

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=od______3697::d576011910ac3f16cb9809f1d8f710ef
http://fox.leuphana.de/portal/de/publications/fatigue-crack-propagation-influenced-by-laser-shock-peening-introduced-residual-stress-fields-in-aluminium-specimens(9bc2d114-58e2-4411-90a2-3bffff0e2071).html