The Rise of “National Heritage” in Modern China

Video of full lecture with presentation slides edited into the video.Guolong Lai, Associate Professor of Chinese Art and Archaeology, University of Florida - As a national cultural policy, heritage preservation was introduced into China from the West as part of the modernizing efforts under the late Qing dynasty. In fact, the very concept of “national heritage” emerged with modernity, which in turn compelled the changes in how cultural heritage was conceived and what measures were taken to conserve it. In this talk Professor Lai attempts to trace the process of the transformation of cultural property from imperial and mostly private possessions in late imperial China to public monuments and state-owned “national heritage” of the Republic and the People’s Republic China through the use of state legislations and administrative orders. In particular, Professor Lai focuses on several important legislative documents on cultural heritage in the first three decades of the 20th century, which set up the basic legal framework for the protection of cultural heritage in modern China.Cornell East Asia Program1_1kf02ll

Effect of Cutting Surface Integrity on Fatigue Properties of TC17 Titanium Alloy

The turning process of titanium alloy material will affect the surface structure of the material and lead to a change in its service life. In this paper, the fatigue behavior of the TC17 titanium alloy turning sample was studied through the bending fatigue test. The fatigue life variation rule under the action of thermal coupling was then discussed. This revealed the fatigue fracture mechanism of TC17; the cracks originated from the surface of the source region, and the transient fault region was a ductile fracture. The mathematical model of turning parameters and surface integrity (roughness, microhardness and residual stress) was established, and the influence of turning parameters on fatigue life was analyzed with a mathematical relationship. Drawing a conclusion, the effects of turning parameters on fatigue life at normal temperature are as follows: Feed > Cutting depth > Cutting speed. The fatigue life of vc = 30 m/min, f = 0.25 mm/r, ap = 0.3 mm is only 40,586 cycles per week, the fatigue life of vc = 30 m/min, f = 0.05 mm/r, ap = 0.1 mm has 539,400 cycles per week, that is, the longest fatigue life is 16.6 times the smallest. Small cutting speed, feed, and large cut depth can be chosen based on ensuring practical processing efficiency. The fatigue fracture of the TC17 sample occurred after a certain cycle, and the fatigue fracture mechanism was revealed in this paper

Research on Surface Integrity and Fatigue Properties in the Turning of TC17 Titanium Alloy Based on the Response Surface Method

Titanium alloy parts are more and more widely used in the field of aerospace. In order to improve the service life of titanium alloy parts, the response surface method was used to study surface residual stress and roughness under different turning parameters. In addition, a mathematical model was established through multiple linear regression to determine the relationship between surface integrity parameters and fatigue life. The test results indicate that the turning parameters have an effect on surface residual stress in the order of feed rate > depth of cut > cutting speed and on surface roughness in the order of feed rate > cutting speed > depth of cut. The analysis results of surface integrity show that the residual compressive stress on the surface has the greatest impact on fatigue life, followed by surface roughness. The fatigue life increases with the increase in residual compressive stress and decreases linearly with the increase in surface roughness. The feed rate has a significant impact on residual stress and surface roughness. Therefore, under the experimental conditions of this paper, the appropriate feed rate can be selected to ensure that the  Ra < 2 μm and a large residual compressive stress is obtained