V-Coupling is commonly used as a mechanical fastener to connect the turbine housing and the bearing housing in a turbocharger assembly. The back plate between the turbine housing and bearing housing would be compressed by tightening torque of the coupling bolt in order to protect the gas leakage at a turbocharger’s operation. This paper presents the numerical and experimental method for the prediction of the mechanical behavior and sealing performance of the coupling system. The test was conducted to verify the finite element model by measuring the circumferential and axial direction strains of V-coupling under turbocharger’s assembly load. Finite element analysis was carried out to obtain the mechanical strains and contact pressures of the coupling. It can be seen that the analysis results are in good agreement with the measured strains from the coupling’s assembly load. And, the pressure distribution of the back plate also presented to identify the sealing performance of the turbocharger’s coupling system.

The axial thrust acting on the turbocharger rotor is basically generated by the unbalance between turbine wheel gas forces and compressor wheel air forces. It has a significant influence on the friction losses, which reduces the overall efficiency and performance of high-speed turbocharger. Therefore, it’s important to calculate the thrust forces under operating conditions (surge, choke and etc.) in a turbocharger. The purpose of this paper is the development of numerical simulation methods which were verified by experimental results of axial thrust and thermally induced constraint tests of the turbocharger. The first FE model showed the relationship between thrust forces and strains by calculating the strains on specially designed thrust bearing and were compared with test results. And the second one is to identify the thermally induced strains in order to remove the thermal effects from measured strains. With these models, it’s possible to inversely predict the magnitudes of the axial thrust by directly measured strains and temperatures under operating turbocharger.

In this paper, the main objective is to determine the mechanical responses due to the axial forces on thrust bearing for an automotive turbocharger. The rotating shaft in a turbocharger is supported by the bearings, usually oil-lubricated radial journal bearings and a thrust bearing. The axial forces acting on the thrust bearing have significant influences on the mechanical friction losses, which reduces the efficiency and performance of high-speed turbocharger. There are simple well-known formulas such as Petroff’s equation for calculating the mechanical frictional losses in these types of bearings. However, it's difficult to estimate the accurate axial forces from this formula. Thus, this work determined the relationship between thrust forces and strains by measuring and calculating the strains on thrust bearing and compared both results. The result shown that behaviors of axial strain are changed linear and non-linear depend on the boundary condition. Therefore, it’s possible to predict the magnitudes of the axial forces by measuring the strains under operating turbocharger.

This paper presents a method for the assesment of thermal and vibration fatigues in integral exhaust manifold/turbine housing system. Most of failures on turbine housing are observed by thermal cyclic loads. In order to predict thermal failures by finite element analysis, we considered the temperature-dependent inelastic materials and transient temperature histories based on the thermal shock test. The results showed that the plastic strains of localized critical regions such as valve seat coincided well with crack locations from an endurance test. But, some failures around neck areas of turbine housing could not predict from thermal stress analysis. These cracks were originated due to the vibration excitations near resonance frequencies within engine operating ranges. The stress results of neck areas, which divided by temperature dependent yield stresses, from harmonic analysis showd a good agreement with experimental results.

In the late decade of 1930, under the Japanese Imperialism, the Korean abstract art which was formed with affection by Japan and Europe. They say the early Korean abstract art is colonized, from a point that it derives from exterior impact. And they say also it is colonized not to be related to the representation of their own life world. On the other hand, the early Korean abstract art in 1930s is told as the prehistory of ‘Korean Modernism in Art’, which flourished in 1970s followed ‘Informal Art Movement’ in the late 1950s. Because the status of abstract art in 1930s was not more than a germ of ‘Korean Modernism in Art’, while they understand until 1950s as a period dominated by representational art based on Chosun Exhibition or Korean National Exhibition, the period until 1970s as a period ruled by abstract art which was accepted as ‘Korean Modernism in Art’, and the period after 1980s as a period by Min-jung Art and Post-Modernism Art. However, the historical value of Korean Abstract Art in 1930s cannot be passed over, if not trying to understand the development of ‘Korean Modernism in Art’ especially focusing on not their own history but the impact of Western and Japanese art. In the late colonial period, the Korean early abstract art was the strongest utterance of the time paradoxically, even if not related much to optical representation of the Korean subjectivity. Therefore the existing viewpoints about the early Korean abstract art should be changed.