2018
DOI: 10.1007/s11665-018-3581-6
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Effect of Tool Temperature on Microstructure and Properties of Tailored Hot Stamping Components

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Cited by 7 publications
(4 citation statements)
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“…A threshold temperature of about 436 °C that leads to a homogeneous bainitic microstructure on the component is found. These results are in agreement with Tang et al [ 32 ] and Zang et al [ 33 ] who demonstrated that the tool temperature should be greater than 400 °C if a noticeable change in mechanical properties is desired on the ductile part of the component.…”
Section: Resultssupporting
confidence: 92%
See 1 more Smart Citation
“…A threshold temperature of about 436 °C that leads to a homogeneous bainitic microstructure on the component is found. These results are in agreement with Tang et al [ 32 ] and Zang et al [ 33 ] who demonstrated that the tool temperature should be greater than 400 °C if a noticeable change in mechanical properties is desired on the ductile part of the component.…”
Section: Resultssupporting
confidence: 92%
“…FE results showed that the temperature of heated tools is the parameter that mainly affects the homogeneity of the bainitic microstructure, in agreement with the literature. [32,33] This result is confirmed by the metamodels in Figure 8, 9 related to the bainitic transformation as a function of process parameters. For reasons of simplification, results are shown only for ductile region III (Figure 1); however, it was verified that the results for both ductile regions are similar.…”
Section: Influence Of Process Parameterssupporting
confidence: 67%
“…They achieved a hardness and ultimate tensile strength (UTS) of the energy absorption area that was reduced by 52% and 49%, respectively, compared with the anti-invasion area. Zhang et al [8] performed similar studies with die temperatures up to 500 °C and achieved hardness levels of 230 HV in the slow cooling zone and 470 HV in the quenching zone. Zhou et al [9] reported a UTS of approximately 916 MPa in the tailored region compared with a UTS of approximately 1411 MPa in the fully hardened region.…”
Section: Introductionmentioning
confidence: 93%
“…The frequent alternation of large-scale ambient temperature changes will inevitably affect the performance of spacecraft. Compared with satellites or manned spacecraft flying around the earth, the space environment faced by deep space exploration spacecraft and extraterrestrial resident platforms is more complex and harsher [2] .…”
Section: Introductionmentioning
confidence: 99%