Rotary-bending fatigue characteristics of medical-grade Nitinol wire
The rotary bending fatigue properties of medical-grade Nitinol wires were investigated under conditions of 0.5–10% strain amplitudes to a maximum of 107 cycles. The results from this study provide insight into the behavior of Nitinol under fully reversed (ε min/ε max=−1) fatigue conditions for three...
Ausführliche Beschreibung
Gespeichert in:
| Autor*in: |
Pelton, A.R. [verfasserIn] |
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| Format: |
E-Artikel |
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| Sprache: |
Englisch |
| Erschienen: |
2013transfer abstract |
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| Schlagwörter: |
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| Umfang: |
14 |
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| Übergeordnetes Werk: |
Enthalten in: A volume-shrinkage-based method for quantifying the inward solidification heat transfer of a phase change material filled in spherical capsules - Liu, Min-Jie ELSEVIER, 2016, Amsterdam [u.a.] |
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| Übergeordnetes Werk: |
volume:27 ; year:2013 ; pages:19-32 ; extent:14 |
| Links: |
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| DOI / URN: |
10.1016/j.jmbbm.2013.06.003 |
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ELV033020825 |
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| 245 | 1 | 0 | |a Rotary-bending fatigue characteristics of medical-grade Nitinol wire |
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| 520 | |a The rotary bending fatigue properties of medical-grade Nitinol wires were investigated under conditions of 0.5–10% strain amplitudes to a maximum of 107 cycles. The results from this study provide insight into the behavior of Nitinol under fully reversed (ε min/ε max=−1) fatigue conditions for three compositions, two surface conditions and three test temperatures. For pseudoelastic conditions there are four distinct regions of the strain-cycle curves that are related to phases (austenite, stress-induced martensite, and R-Phase) and their respective strain accommodation mechanisms. In contrast, there are only two regions for the strain-cycle curves for thermal martensite. It was further observed that the strain amplitude to achieve 107-cycles increases with both decreasing test temperature and increasing transformation temperature. Fatigue behavior was not, however, strongly influenced by wire surface condition. SEM of the fracture surfaces showed that the fatigue fracture area increased with decreasing strain amplitude. Finite element analysis was used to illustrate strain distributions across the wire as well as to calculate the tension-compression contributions to the rotary bending curves. The results from this investigation are discussed with respect to mechanisms of strain accommodation under cyclic tensile and compressive conditions. | ||
| 520 | |a The rotary bending fatigue properties of medical-grade Nitinol wires were investigated under conditions of 0.5–10% strain amplitudes to a maximum of 107 cycles. The results from this study provide insight into the behavior of Nitinol under fully reversed (ε min/ε max=−1) fatigue conditions for three compositions, two surface conditions and three test temperatures. For pseudoelastic conditions there are four distinct regions of the strain-cycle curves that are related to phases (austenite, stress-induced martensite, and R-Phase) and their respective strain accommodation mechanisms. In contrast, there are only two regions for the strain-cycle curves for thermal martensite. It was further observed that the strain amplitude to achieve 107-cycles increases with both decreasing test temperature and increasing transformation temperature. Fatigue behavior was not, however, strongly influenced by wire surface condition. SEM of the fracture surfaces showed that the fatigue fracture area increased with decreasing strain amplitude. Finite element analysis was used to illustrate strain distributions across the wire as well as to calculate the tension-compression contributions to the rotary bending curves. The results from this investigation are discussed with respect to mechanisms of strain accommodation under cyclic tensile and compressive conditions. | ||
| 650 | 7 | |a Pseudoelasticity |2 Elsevier | |
| 650 | 7 | |a Shape memory |2 Elsevier | |
| 650 | 7 | |a Fatigue |2 Elsevier | |
| 650 | 7 | |a Strain amplitude |2 Elsevier | |
| 650 | 7 | |a Nitinol |2 Elsevier | |
| 700 | 1 | |a Fino-Decker, J. |4 oth | |
| 700 | 1 | |a Vien, L. |4 oth | |
| 700 | 1 | |a Bonsignore, C. |4 oth | |
| 700 | 1 | |a Saffari, P. |4 oth | |
| 700 | 1 | |a Launey, M. |4 oth | |
| 700 | 1 | |a Mitchell, M.R. |4 oth | |
| 773 | 0 | 8 | |i Enthalten in |n Elsevier |a Liu, Min-Jie ELSEVIER |t A volume-shrinkage-based method for quantifying the inward solidification heat transfer of a phase change material filled in spherical capsules |d 2016 |g Amsterdam [u.a.] |w (DE-627)ELV009727671 |
| 773 | 1 | 8 | |g volume:27 |g year:2013 |g pages:19-32 |g extent:14 |
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10.1016/j.jmbbm.2013.06.003 doi GBVA2013009000002.pica (DE-627)ELV033020825 (ELSEVIER)S1751-6161(13)00210-5 DE-627 ger DE-627 rakwb eng 570 570 DE-600 690 VZ 52.43 bkl 52.52 bkl 52.42 bkl 50.38 bkl Pelton, A.R. verfasserin aut Rotary-bending fatigue characteristics of medical-grade Nitinol wire 2013transfer abstract 14 nicht spezifiziert zzz rdacontent nicht spezifiziert z rdamedia nicht spezifiziert zu rdacarrier The rotary bending fatigue properties of medical-grade Nitinol wires were investigated under conditions of 0.5–10% strain amplitudes to a maximum of 107 cycles. The results from this study provide insight into the behavior of Nitinol under fully reversed (ε min/ε max=−1) fatigue conditions for three compositions, two surface conditions and three test temperatures. For pseudoelastic conditions there are four distinct regions of the strain-cycle curves that are related to phases (austenite, stress-induced martensite, and R-Phase) and their respective strain accommodation mechanisms. In contrast, there are only two regions for the strain-cycle curves for thermal martensite. It was further observed that the strain amplitude to achieve 107-cycles increases with both decreasing test temperature and increasing transformation temperature. Fatigue behavior was not, however, strongly influenced by wire surface condition. SEM of the fracture surfaces showed that the fatigue fracture area increased with decreasing strain amplitude. Finite element analysis was used to illustrate strain distributions across the wire as well as to calculate the tension-compression contributions to the rotary bending curves. The results from this investigation are discussed with respect to mechanisms of strain accommodation under cyclic tensile and compressive conditions. The rotary bending fatigue properties of medical-grade Nitinol wires were investigated under conditions of 0.5–10% strain amplitudes to a maximum of 107 cycles. The results from this study provide insight into the behavior of Nitinol under fully reversed (ε min/ε max=−1) fatigue conditions for three compositions, two surface conditions and three test temperatures. For pseudoelastic conditions there are four distinct regions of the strain-cycle curves that are related to phases (austenite, stress-induced martensite, and R-Phase) and their respective strain accommodation mechanisms. In contrast, there are only two regions for the strain-cycle curves for thermal martensite. It was further observed that the strain amplitude to achieve 107-cycles increases with both decreasing test temperature and increasing transformation temperature. Fatigue behavior was not, however, strongly influenced by wire surface condition. SEM of the fracture surfaces showed that the fatigue fracture area increased with decreasing strain amplitude. Finite element analysis was used to illustrate strain distributions across the wire as well as to calculate the tension-compression contributions to the rotary bending curves. The results from this investigation are discussed with respect to mechanisms of strain accommodation under cyclic tensile and compressive conditions. Pseudoelasticity Elsevier Shape memory Elsevier Fatigue Elsevier Strain amplitude Elsevier Nitinol Elsevier Fino-Decker, J. oth Vien, L. oth Bonsignore, C. oth Saffari, P. oth Launey, M. oth Mitchell, M.R. oth Enthalten in Elsevier Liu, Min-Jie ELSEVIER A volume-shrinkage-based method for quantifying the inward solidification heat transfer of a phase change material filled in spherical capsules 2016 Amsterdam [u.a.] (DE-627)ELV009727671 volume:27 year:2013 pages:19-32 extent:14 https://doi.org/10.1016/j.jmbbm.2013.06.003 Volltext GBV_USEFLAG_U GBV_ELV SYSFLAG_U 52.43 Kältetechnik VZ 52.52 Thermische Energieerzeugung Wärmetechnik VZ 52.42 Heizungstechnik Lüftungstechnik Klimatechnik VZ 50.38 Technische Thermodynamik VZ AR 27 2013 19-32 14 045F 570 |
| spelling |
10.1016/j.jmbbm.2013.06.003 doi GBVA2013009000002.pica (DE-627)ELV033020825 (ELSEVIER)S1751-6161(13)00210-5 DE-627 ger DE-627 rakwb eng 570 570 DE-600 690 VZ 52.43 bkl 52.52 bkl 52.42 bkl 50.38 bkl Pelton, A.R. verfasserin aut Rotary-bending fatigue characteristics of medical-grade Nitinol wire 2013transfer abstract 14 nicht spezifiziert zzz rdacontent nicht spezifiziert z rdamedia nicht spezifiziert zu rdacarrier The rotary bending fatigue properties of medical-grade Nitinol wires were investigated under conditions of 0.5–10% strain amplitudes to a maximum of 107 cycles. The results from this study provide insight into the behavior of Nitinol under fully reversed (ε min/ε max=−1) fatigue conditions for three compositions, two surface conditions and three test temperatures. For pseudoelastic conditions there are four distinct regions of the strain-cycle curves that are related to phases (austenite, stress-induced martensite, and R-Phase) and their respective strain accommodation mechanisms. In contrast, there are only two regions for the strain-cycle curves for thermal martensite. It was further observed that the strain amplitude to achieve 107-cycles increases with both decreasing test temperature and increasing transformation temperature. Fatigue behavior was not, however, strongly influenced by wire surface condition. SEM of the fracture surfaces showed that the fatigue fracture area increased with decreasing strain amplitude. Finite element analysis was used to illustrate strain distributions across the wire as well as to calculate the tension-compression contributions to the rotary bending curves. The results from this investigation are discussed with respect to mechanisms of strain accommodation under cyclic tensile and compressive conditions. The rotary bending fatigue properties of medical-grade Nitinol wires were investigated under conditions of 0.5–10% strain amplitudes to a maximum of 107 cycles. The results from this study provide insight into the behavior of Nitinol under fully reversed (ε min/ε max=−1) fatigue conditions for three compositions, two surface conditions and three test temperatures. For pseudoelastic conditions there are four distinct regions of the strain-cycle curves that are related to phases (austenite, stress-induced martensite, and R-Phase) and their respective strain accommodation mechanisms. In contrast, there are only two regions for the strain-cycle curves for thermal martensite. It was further observed that the strain amplitude to achieve 107-cycles increases with both decreasing test temperature and increasing transformation temperature. Fatigue behavior was not, however, strongly influenced by wire surface condition. SEM of the fracture surfaces showed that the fatigue fracture area increased with decreasing strain amplitude. Finite element analysis was used to illustrate strain distributions across the wire as well as to calculate the tension-compression contributions to the rotary bending curves. The results from this investigation are discussed with respect to mechanisms of strain accommodation under cyclic tensile and compressive conditions. Pseudoelasticity Elsevier Shape memory Elsevier Fatigue Elsevier Strain amplitude Elsevier Nitinol Elsevier Fino-Decker, J. oth Vien, L. oth Bonsignore, C. oth Saffari, P. oth Launey, M. oth Mitchell, M.R. oth Enthalten in Elsevier Liu, Min-Jie ELSEVIER A volume-shrinkage-based method for quantifying the inward solidification heat transfer of a phase change material filled in spherical capsules 2016 Amsterdam [u.a.] (DE-627)ELV009727671 volume:27 year:2013 pages:19-32 extent:14 https://doi.org/10.1016/j.jmbbm.2013.06.003 Volltext GBV_USEFLAG_U GBV_ELV SYSFLAG_U 52.43 Kältetechnik VZ 52.52 Thermische Energieerzeugung Wärmetechnik VZ 52.42 Heizungstechnik Lüftungstechnik Klimatechnik VZ 50.38 Technische Thermodynamik VZ AR 27 2013 19-32 14 045F 570 |
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10.1016/j.jmbbm.2013.06.003 doi GBVA2013009000002.pica (DE-627)ELV033020825 (ELSEVIER)S1751-6161(13)00210-5 DE-627 ger DE-627 rakwb eng 570 570 DE-600 690 VZ 52.43 bkl 52.52 bkl 52.42 bkl 50.38 bkl Pelton, A.R. verfasserin aut Rotary-bending fatigue characteristics of medical-grade Nitinol wire 2013transfer abstract 14 nicht spezifiziert zzz rdacontent nicht spezifiziert z rdamedia nicht spezifiziert zu rdacarrier The rotary bending fatigue properties of medical-grade Nitinol wires were investigated under conditions of 0.5–10% strain amplitudes to a maximum of 107 cycles. The results from this study provide insight into the behavior of Nitinol under fully reversed (ε min/ε max=−1) fatigue conditions for three compositions, two surface conditions and three test temperatures. For pseudoelastic conditions there are four distinct regions of the strain-cycle curves that are related to phases (austenite, stress-induced martensite, and R-Phase) and their respective strain accommodation mechanisms. In contrast, there are only two regions for the strain-cycle curves for thermal martensite. It was further observed that the strain amplitude to achieve 107-cycles increases with both decreasing test temperature and increasing transformation temperature. Fatigue behavior was not, however, strongly influenced by wire surface condition. SEM of the fracture surfaces showed that the fatigue fracture area increased with decreasing strain amplitude. Finite element analysis was used to illustrate strain distributions across the wire as well as to calculate the tension-compression contributions to the rotary bending curves. The results from this investigation are discussed with respect to mechanisms of strain accommodation under cyclic tensile and compressive conditions. The rotary bending fatigue properties of medical-grade Nitinol wires were investigated under conditions of 0.5–10% strain amplitudes to a maximum of 107 cycles. The results from this study provide insight into the behavior of Nitinol under fully reversed (ε min/ε max=−1) fatigue conditions for three compositions, two surface conditions and three test temperatures. For pseudoelastic conditions there are four distinct regions of the strain-cycle curves that are related to phases (austenite, stress-induced martensite, and R-Phase) and their respective strain accommodation mechanisms. In contrast, there are only two regions for the strain-cycle curves for thermal martensite. It was further observed that the strain amplitude to achieve 107-cycles increases with both decreasing test temperature and increasing transformation temperature. Fatigue behavior was not, however, strongly influenced by wire surface condition. SEM of the fracture surfaces showed that the fatigue fracture area increased with decreasing strain amplitude. Finite element analysis was used to illustrate strain distributions across the wire as well as to calculate the tension-compression contributions to the rotary bending curves. The results from this investigation are discussed with respect to mechanisms of strain accommodation under cyclic tensile and compressive conditions. Pseudoelasticity Elsevier Shape memory Elsevier Fatigue Elsevier Strain amplitude Elsevier Nitinol Elsevier Fino-Decker, J. oth Vien, L. oth Bonsignore, C. oth Saffari, P. oth Launey, M. oth Mitchell, M.R. oth Enthalten in Elsevier Liu, Min-Jie ELSEVIER A volume-shrinkage-based method for quantifying the inward solidification heat transfer of a phase change material filled in spherical capsules 2016 Amsterdam [u.a.] (DE-627)ELV009727671 volume:27 year:2013 pages:19-32 extent:14 https://doi.org/10.1016/j.jmbbm.2013.06.003 Volltext GBV_USEFLAG_U GBV_ELV SYSFLAG_U 52.43 Kältetechnik VZ 52.52 Thermische Energieerzeugung Wärmetechnik VZ 52.42 Heizungstechnik Lüftungstechnik Klimatechnik VZ 50.38 Technische Thermodynamik VZ AR 27 2013 19-32 14 045F 570 |
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10.1016/j.jmbbm.2013.06.003 doi GBVA2013009000002.pica (DE-627)ELV033020825 (ELSEVIER)S1751-6161(13)00210-5 DE-627 ger DE-627 rakwb eng 570 570 DE-600 690 VZ 52.43 bkl 52.52 bkl 52.42 bkl 50.38 bkl Pelton, A.R. verfasserin aut Rotary-bending fatigue characteristics of medical-grade Nitinol wire 2013transfer abstract 14 nicht spezifiziert zzz rdacontent nicht spezifiziert z rdamedia nicht spezifiziert zu rdacarrier The rotary bending fatigue properties of medical-grade Nitinol wires were investigated under conditions of 0.5–10% strain amplitudes to a maximum of 107 cycles. The results from this study provide insight into the behavior of Nitinol under fully reversed (ε min/ε max=−1) fatigue conditions for three compositions, two surface conditions and three test temperatures. For pseudoelastic conditions there are four distinct regions of the strain-cycle curves that are related to phases (austenite, stress-induced martensite, and R-Phase) and their respective strain accommodation mechanisms. In contrast, there are only two regions for the strain-cycle curves for thermal martensite. It was further observed that the strain amplitude to achieve 107-cycles increases with both decreasing test temperature and increasing transformation temperature. Fatigue behavior was not, however, strongly influenced by wire surface condition. SEM of the fracture surfaces showed that the fatigue fracture area increased with decreasing strain amplitude. Finite element analysis was used to illustrate strain distributions across the wire as well as to calculate the tension-compression contributions to the rotary bending curves. The results from this investigation are discussed with respect to mechanisms of strain accommodation under cyclic tensile and compressive conditions. The rotary bending fatigue properties of medical-grade Nitinol wires were investigated under conditions of 0.5–10% strain amplitudes to a maximum of 107 cycles. The results from this study provide insight into the behavior of Nitinol under fully reversed (ε min/ε max=−1) fatigue conditions for three compositions, two surface conditions and three test temperatures. For pseudoelastic conditions there are four distinct regions of the strain-cycle curves that are related to phases (austenite, stress-induced martensite, and R-Phase) and their respective strain accommodation mechanisms. In contrast, there are only two regions for the strain-cycle curves for thermal martensite. It was further observed that the strain amplitude to achieve 107-cycles increases with both decreasing test temperature and increasing transformation temperature. Fatigue behavior was not, however, strongly influenced by wire surface condition. SEM of the fracture surfaces showed that the fatigue fracture area increased with decreasing strain amplitude. Finite element analysis was used to illustrate strain distributions across the wire as well as to calculate the tension-compression contributions to the rotary bending curves. The results from this investigation are discussed with respect to mechanisms of strain accommodation under cyclic tensile and compressive conditions. Pseudoelasticity Elsevier Shape memory Elsevier Fatigue Elsevier Strain amplitude Elsevier Nitinol Elsevier Fino-Decker, J. oth Vien, L. oth Bonsignore, C. oth Saffari, P. oth Launey, M. oth Mitchell, M.R. oth Enthalten in Elsevier Liu, Min-Jie ELSEVIER A volume-shrinkage-based method for quantifying the inward solidification heat transfer of a phase change material filled in spherical capsules 2016 Amsterdam [u.a.] (DE-627)ELV009727671 volume:27 year:2013 pages:19-32 extent:14 https://doi.org/10.1016/j.jmbbm.2013.06.003 Volltext GBV_USEFLAG_U GBV_ELV SYSFLAG_U 52.43 Kältetechnik VZ 52.52 Thermische Energieerzeugung Wärmetechnik VZ 52.42 Heizungstechnik Lüftungstechnik Klimatechnik VZ 50.38 Technische Thermodynamik VZ AR 27 2013 19-32 14 045F 570 |
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10.1016/j.jmbbm.2013.06.003 doi GBVA2013009000002.pica (DE-627)ELV033020825 (ELSEVIER)S1751-6161(13)00210-5 DE-627 ger DE-627 rakwb eng 570 570 DE-600 690 VZ 52.43 bkl 52.52 bkl 52.42 bkl 50.38 bkl Pelton, A.R. verfasserin aut Rotary-bending fatigue characteristics of medical-grade Nitinol wire 2013transfer abstract 14 nicht spezifiziert zzz rdacontent nicht spezifiziert z rdamedia nicht spezifiziert zu rdacarrier The rotary bending fatigue properties of medical-grade Nitinol wires were investigated under conditions of 0.5–10% strain amplitudes to a maximum of 107 cycles. The results from this study provide insight into the behavior of Nitinol under fully reversed (ε min/ε max=−1) fatigue conditions for three compositions, two surface conditions and three test temperatures. For pseudoelastic conditions there are four distinct regions of the strain-cycle curves that are related to phases (austenite, stress-induced martensite, and R-Phase) and their respective strain accommodation mechanisms. In contrast, there are only two regions for the strain-cycle curves for thermal martensite. It was further observed that the strain amplitude to achieve 107-cycles increases with both decreasing test temperature and increasing transformation temperature. Fatigue behavior was not, however, strongly influenced by wire surface condition. SEM of the fracture surfaces showed that the fatigue fracture area increased with decreasing strain amplitude. Finite element analysis was used to illustrate strain distributions across the wire as well as to calculate the tension-compression contributions to the rotary bending curves. The results from this investigation are discussed with respect to mechanisms of strain accommodation under cyclic tensile and compressive conditions. The rotary bending fatigue properties of medical-grade Nitinol wires were investigated under conditions of 0.5–10% strain amplitudes to a maximum of 107 cycles. The results from this study provide insight into the behavior of Nitinol under fully reversed (ε min/ε max=−1) fatigue conditions for three compositions, two surface conditions and three test temperatures. For pseudoelastic conditions there are four distinct regions of the strain-cycle curves that are related to phases (austenite, stress-induced martensite, and R-Phase) and their respective strain accommodation mechanisms. In contrast, there are only two regions for the strain-cycle curves for thermal martensite. It was further observed that the strain amplitude to achieve 107-cycles increases with both decreasing test temperature and increasing transformation temperature. Fatigue behavior was not, however, strongly influenced by wire surface condition. SEM of the fracture surfaces showed that the fatigue fracture area increased with decreasing strain amplitude. Finite element analysis was used to illustrate strain distributions across the wire as well as to calculate the tension-compression contributions to the rotary bending curves. The results from this investigation are discussed with respect to mechanisms of strain accommodation under cyclic tensile and compressive conditions. Pseudoelasticity Elsevier Shape memory Elsevier Fatigue Elsevier Strain amplitude Elsevier Nitinol Elsevier Fino-Decker, J. oth Vien, L. oth Bonsignore, C. oth Saffari, P. oth Launey, M. oth Mitchell, M.R. oth Enthalten in Elsevier Liu, Min-Jie ELSEVIER A volume-shrinkage-based method for quantifying the inward solidification heat transfer of a phase change material filled in spherical capsules 2016 Amsterdam [u.a.] (DE-627)ELV009727671 volume:27 year:2013 pages:19-32 extent:14 https://doi.org/10.1016/j.jmbbm.2013.06.003 Volltext GBV_USEFLAG_U GBV_ELV SYSFLAG_U 52.43 Kältetechnik VZ 52.52 Thermische Energieerzeugung Wärmetechnik VZ 52.42 Heizungstechnik Lüftungstechnik Klimatechnik VZ 50.38 Technische Thermodynamik VZ AR 27 2013 19-32 14 045F 570 |
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Enthalten in A volume-shrinkage-based method for quantifying the inward solidification heat transfer of a phase change material filled in spherical capsules Amsterdam [u.a.] volume:27 year:2013 pages:19-32 extent:14 |
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Enthalten in A volume-shrinkage-based method for quantifying the inward solidification heat transfer of a phase change material filled in spherical capsules Amsterdam [u.a.] volume:27 year:2013 pages:19-32 extent:14 |
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rotary-bending fatigue characteristics of medical-grade nitinol wire |
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The rotary bending fatigue properties of medical-grade Nitinol wires were investigated under conditions of 0.5–10% strain amplitudes to a maximum of 107 cycles. The results from this study provide insight into the behavior of Nitinol under fully reversed (ε min/ε max=−1) fatigue conditions for three compositions, two surface conditions and three test temperatures. For pseudoelastic conditions there are four distinct regions of the strain-cycle curves that are related to phases (austenite, stress-induced martensite, and R-Phase) and their respective strain accommodation mechanisms. In contrast, there are only two regions for the strain-cycle curves for thermal martensite. It was further observed that the strain amplitude to achieve 107-cycles increases with both decreasing test temperature and increasing transformation temperature. Fatigue behavior was not, however, strongly influenced by wire surface condition. SEM of the fracture surfaces showed that the fatigue fracture area increased with decreasing strain amplitude. Finite element analysis was used to illustrate strain distributions across the wire as well as to calculate the tension-compression contributions to the rotary bending curves. The results from this investigation are discussed with respect to mechanisms of strain accommodation under cyclic tensile and compressive conditions. |
| abstractGer |
The rotary bending fatigue properties of medical-grade Nitinol wires were investigated under conditions of 0.5–10% strain amplitudes to a maximum of 107 cycles. The results from this study provide insight into the behavior of Nitinol under fully reversed (ε min/ε max=−1) fatigue conditions for three compositions, two surface conditions and three test temperatures. For pseudoelastic conditions there are four distinct regions of the strain-cycle curves that are related to phases (austenite, stress-induced martensite, and R-Phase) and their respective strain accommodation mechanisms. In contrast, there are only two regions for the strain-cycle curves for thermal martensite. It was further observed that the strain amplitude to achieve 107-cycles increases with both decreasing test temperature and increasing transformation temperature. Fatigue behavior was not, however, strongly influenced by wire surface condition. SEM of the fracture surfaces showed that the fatigue fracture area increased with decreasing strain amplitude. Finite element analysis was used to illustrate strain distributions across the wire as well as to calculate the tension-compression contributions to the rotary bending curves. The results from this investigation are discussed with respect to mechanisms of strain accommodation under cyclic tensile and compressive conditions. |
| abstract_unstemmed |
The rotary bending fatigue properties of medical-grade Nitinol wires were investigated under conditions of 0.5–10% strain amplitudes to a maximum of 107 cycles. The results from this study provide insight into the behavior of Nitinol under fully reversed (ε min/ε max=−1) fatigue conditions for three compositions, two surface conditions and three test temperatures. For pseudoelastic conditions there are four distinct regions of the strain-cycle curves that are related to phases (austenite, stress-induced martensite, and R-Phase) and their respective strain accommodation mechanisms. In contrast, there are only two regions for the strain-cycle curves for thermal martensite. It was further observed that the strain amplitude to achieve 107-cycles increases with both decreasing test temperature and increasing transformation temperature. Fatigue behavior was not, however, strongly influenced by wire surface condition. SEM of the fracture surfaces showed that the fatigue fracture area increased with decreasing strain amplitude. Finite element analysis was used to illustrate strain distributions across the wire as well as to calculate the tension-compression contributions to the rotary bending curves. The results from this investigation are discussed with respect to mechanisms of strain accommodation under cyclic tensile and compressive conditions. |
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