- Open Access
Investigation of mechanical properties of Armco-iron during fatigue test
© Vshivkov et al. 2016
- Received: 2 September 2015
- Accepted: 22 February 2016
- Published: 25 March 2016
In this paper the mechanical properties of armco-iron are studied experimentally. The ultrasonic testing machine USF-2000 was used to carry out fatigue tests involving 106–1010 loading cycles. The frequency of loading is 19.5 ± 0.5 kHz. Based on the experimental data, the Wöhler curve was obtained.
For the analysis of physical condition, two new sensors were designed, one of which measured the electric resistance of the sample and the other measured the magnetic permeability. Second measuring method can be applied to ferromagnetic materials only, though it may be useful for studying the mechanical properties of metals in general.
It was shown that the significant changes in physical processes accompanying the evolution of structural defects in the material were observed in the final stages of the experiment.
The applied measurement techniques allowed us to exactly determine the time of fatigue crack initiation below the surface the material, which cannot be monitored by the standard optic methods.
- Gigacyclic fatigue
- Crack length monitoring
The necessity of saving resources and improving the economic efficiency of industrial production is a strong impetus for designing new technologies and materials, which could ensure safe fatigue life of various mechanisms and structures such as bridges, railroad tracks, parts of machine and gas turbine engines, and so on, subject to about 1010 load cycles. The experimental study of fatigue properties of the material on such a cyclic basis involves significant time costs. Nowadays, with the advent of ultrasonic testing machines the researchers can operate with the real-time data and measurements (Bathias & Gigacycle 2004; Botvina 2004; Plekhov et al. 2005; Shaniavski & Skvortsov 1999; Zhu et al. 2006).
The characteristic features of the response of the material to giga cyclic fatigue test mode are the initiation of subsurface fatigue cracks and splitting (dual or duplex) of the Weller curve (Naimark et al. 2014; Sakai 2009; Wang et al. 1999). The analysis of published studies suggests that the physical mechanisms underlying these effects are not understood yet. At present, there are several models of this phenomenon, such as the model proposed in (Naimark et al. 2000; Plekhov et al. 2007a; Plekhov et al. 2007b).
The development and verification of the proposed models requires a detailed experimental study of the process of defect evolution in the material at the final stage of cyclic deformation with small amplitudes of load. The study on structural evolution of armco-iron was done in (Wang et al. 2012). Here it has been shown that in the region of gigacyclic fatigue, the cyclic deformation of pure iron can lead both to the formation of a stable shear band on the sample surface (by analogy with copper or nickel), and characteristic subsurface structures of the “fish eye” type.
These structural studies require interruption of fatigue experiment and therefore cannot give information on the kinetics of the critical defect evolution leading to the destruction of the macroscopic sample. In this paper, our primary concern was to develop an experimental methodology for detecting processes that accompany the evolution of defects in the material during fatigue test on the ultrasonic testing machine.
The mechanical properties of the sample were determined during tests on servo-hydraulic testing machine INSTRON 8500E. The fatigue test was carried out on the ultrasonic testing machine USF-2000 at loading frequency of 20 kHz. As a result, the mechanical characteristics of the material were estimated during quasi-static loading and fatigue properties were determined on the basis of tests including up to 1010 loading cycles.
The magnetic method and the method of measuring the potential drop were used as the most appropriate instruments for studying the kinetics of defect propagation, because they allowed us to record both the appearance of surface and subsurface cracks. The methods have been significantly modified to be able to use the non-linear effects that increase their sensitivity threshold. The obtained data support the view that recording of kinetics of subsurface crack evolution is possible and confirm the hypothesis for the intensive propagation of such cracks at the final stage of the deformation process.
The chemical composition of the armco-iron
The second cyclic test was carried out using the Shimadzu USF-2000 ultrasonic testing machine, which delivers accelerated testing of the fatigue properties of materials at 20 kHz. The 20 kHz vibration generated by the piezo element is amplified by the booster and the horn and transmitted to the sample to generate repeated stress. In the ultrasonic fatigue testing system, the vibration system is constructed so that the longitudinal waves transmitted through the solid body resonate. Consequently, stationary longitudinal waves are formed inside the vibration system (sample, horn and booster). From the physical point of view, the mass of the sample itself plays the role of a generating reactive force, and there is no need to immobilize one side of the sample. By measuring the displacement of a free side of the sample, the generated strain distribution into the sample can be calculated. The uniform stress testing can be carried out by controlling the amplitude of the vibration. The application of ultrasonic testing machines for fatigue experiments are described in (Bathias & Gigacycle 2004; Bathias & Paris 2005; Palin-Luc et al. 2010).
In the present study, all the samples were tested at the constant stress amplitude up to the failure. The cooling of the sample was realized by an air stream. The temperature of the sample was controlled by infrared camera. The ordinary temperature rise during the stable test regime was about 50C. The experiment lasted until the resonance frequency of the sample changed significantly (by more than 10 %).
During the experiments an infrared camera Flir SC 5000 (spectral range of 3–5 μ, the temperature sensitivity of 0.25 K) was used to control the temperature of the sample. The standard calibration table for 1000 ms exposure time was applied to calibrate the unit.
During the experiment, two electromagnetic coils were placed on the sample: the magnetizing coil (diameter of copper wire is 0.5 mm., 800 turns) and measuring coil (diameter of copper wire is 0.1 mm., 200 turns). The alternating current in the magnetizing coil magnetized the sample to saturation. This point was fixed by the appearance of the nonlinear useful signal in the measuring coil. It was found that the second harmonic of the measuring coil signal was most sensitive to the magnetic field variation inside the sample (inductance of sample).
To switch the magnetizing coil, a mini amplifier of signals was assembled based on the TDA2030a chip (18 W HiFi power amplifier class AB). This amplifier provides high output current, has small harmonic and intermodulation distortions, wide bandwidth of the amplified signal, low level of intrinsic noise, the built-in protection against the output short circuit, automatic system to limit dissipated power, which holds the working point of the output transistors in the safe area. The built-in thermal protection element switches off the chip when the crystal is heated above 145 °C. The chip is produced in the Pentawatt package and has five pins.
The magnetizing coil can operate in two modes: stabilization of voltage and stabilization of current. The analog-digital convertor (ADC) NI is used to register the measuring coil signals. The instrument accuracy of the measurement voltage by ADC is 6 uV. The measurement data is analyzed in real time using the LabVIEW software package.
It should be noted that the armco-iron specimens under tensile loading demonstrate abnormal deformation behavior. According to literature (Plekhov et al. 2005), a decrease in the resonant frequency during the fatigue test on ultrasound machine is an irreversible process and corresponds to the emergence of a subsurface fatigue crack. In the case of armco-iron, the decay of the resonance frequency did not imply mechanical (macroscopic) destruction of the specimen after stopping the testing machine.
The specimens withstood practically unlimited number of subsequent runs during 106 loading cycles. An increase of the dwell time between successive runs allowed us to slightly increase the duration of one test run to 2•106 cycles. The Fig. 10 shows the results of using the potential drop method in the process of specimen loading in series of 106 cycles after its coming out of the resonance frequency range during the main test.
Such a behavior of the specimens suggests the presence of irreversible changes in the structure of the material, which can be critical for endurance limit of the specimen during ultrasonic loading tests. At the same time, these changes are not related to the formation of fatigue cracks and are indicative of a sharp increase in the dissipation ability of the specimen and impossibility of further specimen testing in the tensile test machine provided with a standard (air) cooling system. In the Fig. 5, the graph is plotted assuming that this state of the specimen corresponds to its fracture.
Two test programs were realized to investigate changes in magnetic permeability and electrical resistance of the specimen. Within the first program the specimens were tested to failure (overheating), and within the second program the specimens were subject to stepwise loading sets with increasingly growing amplitudes.
The Fig. 10a presents seven loading runs performed at different amplitudes of mechanical stress (from 198 to 258 MPa). By virtue of the structural features the magnetic method data were recorded in the form of a single array (Fig. 10b). The valleys on the curve correspond to the moments when the testing machine was stopped and the specimen was prepared for the next run of loading at higher amplitudes.
For small amplitudes of stress both measurement methods provided signals with constant amplitude (Fig. 10a and the first segment of the curve in Fig. 10b.). An increase in the stress amplitude leads to an increase of the electric resistance in the specimen and a decrease in the second harmonic amplitude of the measuring coil voltage. At sufficiently high mechanical stresses the data obtained by both methods demonstrate abrupt jumps, which correspond to the destruction (overheating) of the specimen.
We have investigated experimentally the mechanical behavior of armco-iron under conditions of giga cycle fatigue loading. The experiments were carried out on the ultrasonic testing machine USF-2000 with loading frequency 20 kHz and air cooling. Based on the results of tests comprising 1010 cycles the Weller curve for the examined material has been plotted. The value of the fatigue limit is 160 MPa.
The experiments have shown that armco-iron reaches its fatigue limit in the abnormal manner. A decrease of the resonance frequency was accompanied by strong (up to 220 °C) heating of the specimen. However, on the surface of the specimen the formation of structural defects has been not observed even with a standard metallographic microscope. In repeated tests, overheating of the specimen occurred after performing 106 loading cycles.
Two new systems for monitoring the physical properties of the specimens have been developed for studying the process of fatigue crack nucleation. These systems are based on the measurement of the electric resistance and induction of the magnetic field. It has been shown that a significant change in the physical processes accompanying the evolution of structural defects in the material is observed at the final stages of the experiment.
The preliminary experiments clearly demonstrated that these methods can be used to monitor the processes of evolution of the material structure during fatigue tests on the ultrasonic testing machine and to estimate the duration of the final stage, at which the specimen reaches its endurance limit. For small amplitudes of the applied stress, the significant changes of parameters are observed during the final 3•106 loading cycles. In this case the catastrophic changes leading to heating of the sample up to 2000 C. lasted during 105 loading cycles.
An exhaustive reply to the question, as to what changes in the structure of the material lead to an increase in its dissipation ability, requires intensive structural studies.
The reported study was funded by RFBR according to the research project No. 16-31-00155 мол_a and No. 14-01-00122.
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