financially supported by the Major Projects in Aviation Engines and Gas Turbines (Grant No.2019-VI-0020-0136);the National Key Research and Development Program of China (Grant Nos.2022YFB3705101&2022YFB3705102);the National Natural Science Foundation of China (Grant No.U1708253);the Fundamental Research Funds for the Central Universities,China (Grant No.N2302005)。
The low frequency electromagnetic casting(LFEC)was used to prevent hot cracking during the solidification process of GH4742 superalloy ingot.The effects of LFEC on the solidification macrostructure of the ingot were i...
financially supported by the National Science and Technology Major Project of China (No.J2019-VI-0004-0117);a Laboratory Fund Project (6142903220101)。
The size and shape effect(SSE)of components has become a critical issue for mechanical properties,application reliability,and processing.In this study,the creep rupture life(CRL)of components with different wall thick...
supported by the Shanghai“Explorer Program”Project(Grant No.24TS1414500);the 10th Sino-Hungarian Intergovernmental Scientific and Technological Cooperation Project(Grant No.2024-10-2)。
Nickel-based superalloy(GH4169)is an ideal material for preparing turbine blades.Profile grinding of the fir-treeshaped turbine blade root can easily cause thermal damage to the workpiece specimen.This study aims to e...
financially supported by the National Natural Science Foundation of China(Nos.52306183,12272245,11832007,12172238);the Natural Science Foundation of Zhejiang Province,China(No.LQ23E050022);the Natural Science Foundation of Sichuan Province,China(Nos.2022NSFSC0324,2022JDJQ0011);the Open Project of Failure Mechanics and Engineering Disaster Prevention,Key Laboratory of Sichuan Province,China(No.FMEDP202305)。
In order to accurately evaluate the creep-fatigue lifetime of GH720Li superalloy,a lifetime prediction model was established,reflecting the interaction between creep damage and low-cycle fatigue damage.The creep-fatig...
supported by the National Science and Technology Major Project of China(2017-VI-0018-0090).
Isothermal compression tests were used to establish constitutive models of the hot deformation of GH4742 superalloy. The microstructural evolution of double cone samples with large strain gradients during hot deformat...
financially supported by the National Key Research and Development Project,China(Nos.2018YFA0703300,2022YFB4600019);the National Natural Science Foundation of China(Nos.52275148,52405154);the Innovation Program Phase II of AECC Commercial Aircraft Engine Co.Ltd,China(No.HT-3RJC1053-2020);support by the Postdoctoral Fellowship Program of CPSF,China(No.GZB20240219);the Shanghai Sailing Program,China(No.24YF2708100).
Submerged Abrasive Waterjet Peening(SAWJP)shows great application potential in augmenting the fatigue properties of metallic parts.Thus,the present work aims to investigate the influence of SAWJP on the Surface Integr...
supported by Guizhou Provincial Key Technology R&D Program(No.[2022]052).
Uniaxial tensile testing explored the Portevin-Le Chatelier(PLC)effect in nickel-based superalloys featuring high Mo/Cr mass ratios,focusing on the influence of variations in the initial microstructure on the deformat...
Correction to:Rare Met.https://doi.org/10.1007/s12598-019-01293-4 In the original publication,Fig.12 was published incorrectly.The correct version of Fig.12 is given in this correction.
This study was funded by Key Science and Technology Projects of Gansu Province(Grant No.22ZD6GB019);the Gansu Key Research and Development Project(Grant No.23YFGA0003);Gansu Provincial Joint Research Fund(Grant No.23JRRC0004);the Fundamental Research Funds for the Central Universities(Grant No.lzujbky-2022-ey15);the fund of the State Key Laboratory of Solidification Processing in NPU(Grant No.SKLSP202204).
In order to elucidate the mechanism of the effect of Ta content on the high temperature behaviour of the alloys,the high temperature oxidation and thermal corrosion experiments were carried out on the three alloys wit...
Supported by Beijing Nova Program(Grant No.Z201100006820094);National Natural Science Foundation of China(Grant Nos.51775525,52175369,U2141205)。
GH 3230 superalloy is a solution strengthening nickel-based superalloy and it is commonly used for fabricating hot components with the service temperature of above 900℃.In order to further improve high-temperature pe...