Results 1 to 10 of about 2,116 (231)

Microstructure degradation of service-exposed turbine blades made of directionally solidified DZ125 superalloy

open access: yesFrontiers in Materials, 2022
The investigation about the degradation behavior of turbine blades exposed to complex and extreme environments for long-term service is of great importance to assess the remaining life of the blades. In our work, the microstructure at different positions
Yadan Xie   +4 more
doaj   +1 more source

Formation Mechanism and Restraining Measures of Burning-on of DZ22B Directionally Solidified Blade

open access: yesJournal of Aeronautical Materials, 2018
The microstructure and chemical composition of the burning-on layer of the directionally solidified blade of the DZ22B superalloy were studied by means of SEM and EDS.
LI Fei   +6 more
doaj   +1 more source

Research progress in effect of static magnetic field on microstructure of directionally solidified Ni-based superalloy

open access: yesCailiao gongcheng, 2019
The current research progress in the influence of static magnetic field on the microstructures of directionally solidified Ni-based superalloy at home and abroad was reviewed, and the effect of different ways, strength of static magnetic fields on the ...
LIU Cheng-lin   +4 more
doaj   +1 more source

Effect of MCrAlY coating on crack formation during thermal fatigue testing of a directionally solidified Nickle based superalloy [PDF]

open access: yesمواد نوین, 2023
Introduction: Nickle based superalloys are widely used in gas turbine components such as blades due to their excellent mechanical properties at high temperatures.
Alimohammad Fazeli Tehrani   +1 more
doaj   +1 more source

Dependence of microstructural evolution on the geometric structure for serviced DZ125 turbine blades

open access: yesFrontiers in Materials, 2023
The turbine blades were directionally solidified by a high-rate solidification process by the Bridgman technique using directional solidified Ni-based master superalloy DZ125 and operated on the engine bench with a high-temperature gas environment of ...
Yadan Xie   +7 more
doaj   +1 more source

Effect of Solid Solution Treatment on Microstructure and Mechanical Properties of DS Superalloy DZ8

open access: yesJournal of Aeronautical Materials, 2016
The microstructure of DZ8 after solid solution treatment at 1260 ℃ and 1240 ℃ was observed, and the tensile and stress rupture properties were compared.
ZHANG Shuaiqi   +6 more
doaj   +1 more source

Creep Damage and Deformation Mechanism of a Directionally Solidified Alloy during Moderate-Temperature Creep

open access: yesCrystals, 2021
Through creep performance tests, microstructural observations, and contrast analysis of the dislocation configuration, the deformation and damage mechanism of the directionally solidified nickel-based superalloy during creep at moderate temperatures was ...
Jiachun Li   +5 more
doaj   +1 more source

Effect of C Content on Microstructure of Second Generation Single Crystal Superalloy

open access: yesJournal of Aeronautical Materials, 2017
The single crystal superalloy with different C contents was casted using master alloy of DD6 in the directionally solidified furnace. The effect of C content on the microstructure of the second generation single crystal superalloy was investigated.
LIU Shizhong, SHI Zhenxue, LI Jiarong
doaj   +1 more source

Effect of Melt Superheating Treatment on the Microstructures and Purity of a Directionally Solidified Superalloy

open access: yesCrystals, 2023
In this paper, the effects and the mechanisms of melt superheating treatment (MST) on a directionally solidified alloy were investigated. The mass loss rate of the superalloy becomes severe as the MST temperature rises.
Yi Li   +3 more
doaj   +1 more source

A Contribution to the Study of the Integrity Surface of the IC10 Ni3Al-Based Alloy After Creep-Feed Grinding with a Focus on High-Temperature Fatigue Life

open access: yesMetals
The IC10 directionally solidified superalloy is a nickel-based alloy with high temperature resistance, and its surface integrity has a significant impact on the fatigue life of critical hot-end components in aerospace engines. This paper investigates the
Shuaiqi Zhang   +7 more
doaj   +1 more source

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