2016
DOI: 10.15587/1729-4061.2016.65454
|View full text |Cite
|
Sign up to set email alerts
|

Modeling of the case depth and surface hardness of steel during ion nitriding

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...
1
1
1
1

Citation Types

0
17
0
5

Year Published

2016
2016
2021
2021

Publication Types

Select...
7
2

Relationship

3
6

Authors

Journals

citations
Cited by 26 publications
(24 citation statements)
references
References 3 publications
0
17
0
5
Order By: Relevance
“…A detailed description of the preliminary laser treatment was given in [17]. As is well known ( [8,12]), the optimal nitriding temperature is 550 °C. Therefore, variation of Table 1 Chemical composition of steels nitriding duration was of particular interest for analysis of the effect of nitriding on thickness of the hardened layer and microhardness of the surface layers.…”
Section: Results Of the Experiments For Determining Thickness Of Tmentioning
confidence: 99%
See 1 more Smart Citation
“…A detailed description of the preliminary laser treatment was given in [17]. As is well known ( [8,12]), the optimal nitriding temperature is 550 °C. Therefore, variation of Table 1 Chemical composition of steels nitriding duration was of particular interest for analysis of the effect of nitriding on thickness of the hardened layer and microhardness of the surface layers.…”
Section: Results Of the Experiments For Determining Thickness Of Tmentioning
confidence: 99%
“…As shown in [12], ion-plasma nitriding shortens processing to 2-8 hours. However, this kind of nitriding is associated with the use of special complex equipment.…”
Section: Development Ofmentioning
confidence: 99%
“…Quantitative phase analysis for residual austenite in the alloy was carried out using the x-ray machine DRON-3 (Russia) according to the standard procedure [22].…”
Section: Research Methods and Modeling The Values Of Tensile Strenmentioning
confidence: 99%
“…For example, if assigned by the permissible values of technological time of a semi-flight, one may find the appropriate three input variables (х 1 , х 2 , х 3 ). Geometrically, this means designing the cross-section of response surface by the plane of equal level, which corresponds to the selected value of output variable, on the plane (х 1 , х 2 ), (х 1 , х 3 ), (х 2 , х 3 ) and subsequent construction of nomograms [14]. However, of the largest interest is the study of the response surface to detect local extrema that occur on the boundaries, described by the curves, obtained in the cross-section of response surface by cylinders of the radius r. The latter are the analytical description of limitations in the form of the crests that allow determining the suboptimal values of output variables and the values of input variables corresponding to them [15].…”
Section: Formalized Description and Development Of A Mathematical Modmentioning
confidence: 99%