Results 111 to 120 of about 1,320 (253)

Effect of Deformation Parameters of an Initial Aged GH4169 Superalloy on Its Microstructural Evolution during a New Two-Stage Annealing. [PDF]

Materials (Basel), 2022
Chen M, Chen Q, Lou Y, Lin Y, Li H, Wang G, Cai H.   +6 more
europepmc   +1 more source

Comparison of Additive Technologies for Gradient Aerospace Part Fabrication from Nickel-Based Superalloys [PDF]

, 2015
In our papers, the laser beam-aided control of the self-propagating high-temperature synthesis in Ni–Al systems for the layerwise manufacture of three-dimensional (3D) parts was offered and experimentally realized.
Kakovkina, Nina G., Kotoban, Dmitry V., Nazarov, Aleksey P., Shishkovsky, Igor V.   +3 more
core   +2 more sources

Effects of Double-Stage Annealing Parameters on Tensile Mechanical Properties of Initial Aging Deformed GH4169 Superalloy. [PDF]

Materials (Basel), 2021
Wang G, Chen M, Lin Y, Lou Y, Li H, Ma Y, Zou Z, Chen Q, Xia Y.   +8 more
europepmc   +1 more source

Creep-Fatigue Behavior of Additively Manufactured Inconel 718: Mechanisms and Challenges [PDF]

This review critically examines the creep-fatigue behavior of additively manufactured (AM) Inconel 718, emphasizing distinctions from conventionally processed forms due to unique microstructures and process-induced defects.
Chaudhari, Sujit B., Gite, Ravindra E., Wakchaure, Vishnu D.   +2 more
core   +1 more source

Study on Shear Angle Model for Superalloy GH4169 [PDF]

Proceedings of the 2017 International Conference on Manufacturing Engineering and Intelligent Materials (ICMEIM 2017), 2017
Yue-wei Chen, Lin He, Zhong-fei Zou
openaire   +1 more source

Quasi-in-situ observation and analysis of grain boundary evolution of GH4169 nickel-based superalloy during the micro-strain stage of thermal deformation

, 2023
Min Ling, Yilong Liang
openalex   +1 more source

Research on the residual stress distribution of aircraft engine blades repaired by laser shock peening and laser cladding composite process [PDF]

The traditional laser cladding (LC) repair process for aircraft blades introduces residual tensile stress near the heat affected zone, which causes a decrease in the strength of the joint interface of the repaired part.
Cheng Xiuquan, He Ruhao, Xia Qinxiang, Xiao Gangfeng, Zhang Junhao   +4 more
core   +1 more source

Towards Enhancing Hot Tooling to Form High-γ′ Superalloys [PDF]

, 2023
Ni-superalloys are well-established for use in high temperature applications in aerospace, power generation, and automotive sectors, yet, are seldom considered as materials for hot tooling.
Fischer, E, Galindo-Nava, E, León-Cázares, FD, Rae, C, Vaasudevan, A, Witulski, T   +5 more
core  

An Accurate FEA of Turning Simulation and Parameters Optimization for Slender Shaft Turning [PDF]

, 2018
There is a high demand to conduct high performance machining in industry to produce high quality parts with high efficiency. Thus, physical machining simulation is a must.
Yang, Tianlin
core  

Forming quality, microstructure, and ductility-oriented mechanical performance of laser powder bed fusion processed Ni-based superalloy using different thermal input modes

Journal of Materials Research and Technology
Thermal input modes significantly affect forming quality, microstructure, and mechanical properties of components fabricated by laser powder bed fusion (LPBF).
Jingjia Sun, Dongdong Gu, Guangjing Huang, Jianfeng Sun, Menghuan Yin, Qi Wu   +5 more
doaj   +1 more source