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UDC 539.319.6-434.1
RESIDUAL STRESSES IN CYLINDRICAL ARTICLES
S. I. Karatushin,1 D. V. Spiridonov,1 and Yu. A. Pleshanova1
Translated from Metallovedenie i Termicheskaya Obrabotka Metallov, No. 6, pp. 53 – 55, June, 2013.
A method of calculating residual stresses that arise in solid or hollow cylinders following thermochemical
treatment is considered. Computer calculations are performed by means of the ANSYS program.
Key words: residual stresses, thermochemical treatment, solid cylinder, hollow cylinder, ANSYS
program.
INTRODUCTION
Residual stresses have long drawn the interest of re-
searchers as a consequence of the fact that they exert a major
influence on the service characteristics of the parts of en-
gines [1]. However, even for articles of simple shape, a com-
plete calculation of stresses was impossible before the ap-
pearance of the method of finite elements. In turn, the
method of finite elements yielded tangible results only with
the development of computational mathematics. All these
advances were ultimately implemented in engineering analy-
sis programs, one of which is ANSYS [2 – 5].
Through the use of the ANSYS Workbench software
module it is possible to calculate all the components of the
stress-strain state at each point of the volume of a body. Arti-
cles of cylindrical form are widely used in engineering appli-
cations and include cylindrical springs, shafts, axles, and
other parts of machines and mechanisms.
The most common of the various methods of hardening
is casehardening with carbon. Casehardening with carbon in
particular will be considered as an example in the present ar-
ticle. Similar methods of calculation may be applied for any
type of thermochemical treatment.
Volumetric variations in subsequent heat treatment are a
source of residual stresses. In carburizing of a surface an in-
crease in the volume of material occurs as a consequence of
an increase in the quantity of carbon in a surface layer, but
the basic increase in the volume of a casehardened layer oc-
curs in a � � � transformation, i.e., in heat treatment. The
increase in volume that occurs in carburizing may be entirely
ignored not only in view of its small magnitude, but also be-
cause of relaxation of stresses throughout an entire volume
due to the high temperature of the process of casehardening.
The objective of the present study is to calculate the re-
sidual stresses that arise in the course of casehardening with
carbon in solid and hollow cylinders made of steel 20Kh.
COMPUTATION TECHNIQUE
To solve the problems involved in calculation of the
stress-strain state, the following initial data will be deter-
mined experimentally or specified:
(1) distribution of carbon across the width of the
casehardened layer of a part;
(2) coefficient of linear expansion of casehardened layers
with different carbon contents caused by a � � � transfor-
mation.
These basic parameters are determined in accordance
with a technique set forth in a previous report [6]. Using the
ANSYS program it is possible to introduce any known cha-
racteristic of the physical properties of a material. Concrete
properties of steel 20Kh (yield strength, Poisson’s coeffi-
cient, concentration of carbon at different distances from the
surface, rate of increase of volume of casehardened layer in
the course of heat treatment) are input into the program when
calculating the residual stresses. A three-dimensional (solid)
or two-dimensional (axisymmetric) model is used to calcu-
late the stress-strain state. The use of volumetric models is
justified for parts of low symmetry. The model is created as a
compound model in one of the graphics programs and is
translated into ANSYS in the Parasolid format. The more
complex the model and the greater its number of parts, the
greater is the length of time of the solution. Computer sys-
tems with high performance must be used for complex
models.
Axisymmetric two-dimensional models are entirely ac-
ceptable for symmetric parts such as bodies of revolution. In
this case a model is created directly in the ANSYS program.
Metal Science and Heat Treatment, Vol. 55, Nos. 5 – 6, September, 2013 (Russian Original Nos. 5 – 6, May – June, 2013)
339
0026-0673/13/0506-0339 © 2013 Springer Science + Business Media New York
1D. F. Ustinov Baltic State Technical University “VOENMEKh,”
St. Peterburg, Russia (e-mail: [email protected]).
For the parts that will be studied in the present article —
a solid cylinder 60 mm in diameter and a hollow cylinder
with outer diameter 72 mm and inner diameter 32 mm — a
variant of a solution in the form of an axisymmetric problem,
i.e., a two-dimensional model, is used. In this case, the solu-
tion is realized quite rapidly even with comparatively small
dimensions of the final elements. The volume of the file is
reduced roughly 10-fold.
RESULTS OF CALCULATIONS AND DISCUSSION
Results of a calculation for the articles being considered
here with an indication of, for example, certain magnitudes
of normal stresses are presented in Fig. 1.
The case-hardened layer is specified with step 0.25 mm.
As in [1], the calculations are presented for steel 20Kh. The
distribution of the stresses in a plane perpendicular to the
axis of the solid cylinder is shown in Fig. 2.
It is interesting to note that for these types of configura-
tions of articles, the tangential and axial normal stresses dif-
fer only very slightly in terms of magnitude and coincide in
terms of distribution law. The tangential stresses are not pre-
sented in the graph due to the lack of practical significance.
The thinner is the casehardened layer, the greater is the
level of the compression stresses and, correspondingly, the
level of the tensile stresses. The distribution pattern of the ra-
dial stresses changes. There is very little information in the
literature about tensile stresses, which balance the field of
compression stresses, though their role is no less important.
The distribution of stresses in a cylinder with an internal
opening is presented in Fig. 3a. In this case the radial stresses
are negative, as was assumed. As for plates, the position of
the maximum of the tensile stresses for cylindrical articles
corresponds to the full depth of casehardening. The effective
depth of casehardening in this case does not possess a dis-
tinct position in the graph. The program being used here
makes it possible to introduce a residual austenite parameter
and thereby estimate the influence of austenite on the distri-
bution of the residual stresses. However, there is a problem
here. There are practically no reliable data in the literature on
the distribution of the quantity of residual austenite by thick-
ness of the casehardened layer. The stresses in a case har-
dened layer that promote the existence of residual austenite
induce blurring of the diffraction lines and, correspondingly,
sharply reduce the precision with which the layer is deter-
mined. The distribution of the stresses in a hollow cylinder
based on the content of residual austenite is presented in
Fig. 3b. The distribution of residual austenite is conjectured
on the basis of generalized data from the literature and re-
lated studies.
CONCLUSIONS
Through the use of the ANSYS Workbench software
package it becomes possible to solve problems that arise in
the analysis of residual stresses in articles of practically any
shape where initial experimental data on the physical proper-
ties of the material of these articles are available. For thermo-
mechanical treatment these properties comprise the specific
volumes of structures and the transverse distribution of satu-
rating elements. For many cases that may be realized in prac-
340 S. I. Karatushin et al.
à b
Fig. 1. Results of a calculation in the form of an axisymmetric prob-
lem for a solid (a) and hollow (b ) cylinder.
60
50
40
30
20
10
– 100
– 200
– 300
– 400
– 500
– 600
– 700
– 800
– 900
�n , ÌPà
30 20 10 6 4 2 1.0 0.60.4 0.2 0.1
h, mm
Radial
Òàngential
and axial
Fig. 2. Distribution of normal stresses (�n
) in a solid case-hardened
cylinder (h — distance from surface).
tical applications, these data may be found in the literature or
determined experimentally. The volume of information that
may be obtained with the use of ANSYS is significantly
greater than that obtained by means of a solution performed
using analytic methods [7] even with the use of computer
programming. The precision of a calculation is assured with
the use of adaptive refinement of the net of final elements.
This yields an acceptable relative error expressed in terms of
the magnitude of the deformation energy, which should not
exceed 10%. Unfortunately, there are no reliable data in the
literature on the complete picture of the stress-strain state of
actual parts. There are no experimental studies in this area
while the computational studies deal only with a narrow
class of questions related to the stress-strain state. The results
that have been obtained in the present study do not contradict
the individual results in the cited literature.
The significance of the present method is that it makes it
possible to analyze in a comparatively simple fashion
changes in the stress-strain state that occur upon the applica-
tion of external forces.
REFERENCES
1. Ya. D. Vishnyakov and V. D. Piskarev, Management of Residual
Stresses in Metals and Alloys [in Russian], Metallurgiya, Mos-
cow (1989), 254 p.
2. K. A. Basov, ANSYS in Examples and Problems [in Russian],
Komp’yuter Press, Moscow (2002), 224 p.
3. O. M. Ogorodnikova, Structural Analysis in the ANSYS Environ-
ment [in Russian], UGTU, Ekaterinburg (2004).
4. A. B. Kaplun, E. M. Morozov, and M. A. Olfer’eva, ANSYS in the
Hands of the Engineer. Practical Manual [in Russian], URSS,
Moscow (2003), 272 p.
5. K. A. Basov, The Graphics Interface of the ANSYS Complex [in
Russian], DMK Press, Moscow (2006), 248 p.
6. S. I. Karatushin, D. V. Spiridinov, and Yu. A. Pleshanova, “Simu-
lation of residual stresses in the process of casehardening,” Izv.
Vysh. Ucheb. Zaved., Mashinostroenie, No. 3, 49 – 52 (2012).
7. I. A. Kazakovtsev and S. M. Shlyakhov, “Estimation of stress-
strain state of a hollow shaft casehardened along the contour with
lengthwise varying casehardening,” Izv. Vysh. Ucheb. Zaved.,
Mashinostroenie, No. 3, 33 – 40 (2008).
Residual Stresses in Cylindrical Articles 341
0.2 0.4 0.6 1.0 2 4 6 10 20 0.2 0.4 0.6 1.0 2 4 6 10 20
– 10
– 20
– 30
– 40
– 50
– 60
– 10
– 20
– 30
– 40
– 50
– 60
120
100
80
60
40
20
120
100
80
60
40
20
– 100
– 200
– 300
– 400
– 500
– 600
– 700
– 800
– 900
– 100
– 200
– 300
– 400
– 500
– 600
– 700
– 800
– 900
�n , ÌPà �n , ÌPà
�r , ÌPà �r , ÌPà
h, mm h, mm
Radial
Radial
Òàngential
and axial
Òàngential
and axial
à b
Fig. 3. Distribution of stresses in a hollow cylinder (external diameter 72 mm, internal diameter 32 mm) with casehardened in-
ternal surface (a) and with the presence of about 25% residual austenite (b ) (h — distance from internal surface).