Results 231 to 240 of about 19,260 (264)
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Microstructural evolution in damaged IN738LC alloy during various steps of rejuvenation heat treatments

Journal of Alloys and Compounds, 2012
Abstract IN738LC is one of the superior nickel base superalloys utilized at high temperatures in aggressive environments. However, experiencing high temperatures and stresses during service causes microstructure deterioration and degradation of mechanical properties in this alloy.
Sayyed Shahabeddin Hosseini   +2 more
exaly   +2 more sources

Effect of Double-Step Solution Treatment on Rejuvenation Heat Treated Microstructure of IN-738 Superalloy

Key Engineering Materials, 2020
This work investigates the effect of rejuvenation heat treatment, with double-step solution treatment at the temperature from 1150 °C to 1200 °C, on the recovered microstructure of IN-738 cast superalloy. The superalloy has been long-term exposed as a turbine blade in a gas turbine prior to this study.
exaly   +2 more sources

Effect of rejuvenation heat treatments on gamma prime distributions in a Ni based superalloy for power plant applications

Materials Science and Technology, 2013
The gamma prime ( γ′) distribution in the Ni based superalloy, CMSX-4, has been examined in detail using a field emission gun scanning electron microscope and a transmission electron microscope after high temperature degradation and the subsequent application of a number of rejuvenation heat treatments.
Rachel C Thomson
exaly   +2 more sources

The investigations of rejuvenation heat treatment on the microstructure and mechanical properties of a serviced gas turbine blade

Journal of Alloys and Compounds, 2023
Zishu Sun   +9 more
exaly   +2 more sources

Effect of rejuvenation heat treatment on the microstructure and stress relaxation behavior of nickel-based superalloy with excess hardness

Materials Characterization, 2023
Jiajian Wang   +5 more
exaly   +2 more sources

Rejuvenation Heat Treatment Development to Extend the Service Life of René N4 Single Crystal Gas Turbine Blades

Volume 9: Manufacturing Materials and Metallurgy; Microturbines, Turbochargers, and Small Turbomachines; Oil & Gas Applications; Steam Turbine
Abstract Single crystal superalloys are widely used for gas turbine blades exposed to high stresses, high temperatures in aggressive environments. When these components reach their serviceable limit, they must be replaced by new ones, with an important impact in terms of maintenance costs.
Cristina Motta   +3 more
exaly   +2 more sources

Full Rejuvenation Heat Treatment of GTD 111DS

Volume 7: Industrial and Cogeneration; Manufacturing Materials and Metallurgy; Microturbines, Turbochargers, and Small Turbomachines; Oil & Gas Applications, 2022
Abstract Previous studies performed by TEServices, Sulzer and EPRI showed that GTD111 DS metallurgical and mechanical [stress rupture (SR) and low cycle fatigue (LCF)] properties can be restored close to new with and without hot isostatic pressing (HIP) followed by full solution heat treatment (FSHT).
Hans van Esch   +4 more
openaire   +1 more source

Full Rejuvenation Heat Treatment of MGA 1400DS

Volume 8: Industrial and Cogeneration; Manufacturing Materials and Metallurgy, 2023
Abstract Directionally Solidified (DS) nickel-base superalloys have been extensively used for power generation turbine blades. These blades are exposed to high stresses and temperatures for extended periods of time and aging the microstructural and reducing the mechanical properties.
Hans van Esch   +4 more
openaire   +1 more source

Microstructural and mechanical investigations on the heat treatment rejuvenation of a long-term service-exposed GTD-111 Ni-based superalloy

Materials Science & Engineering A: Structural Materials: Properties, Microstructure and Processing, 2023
Ali Geranmayeh   +2 more
exaly   +2 more sources

Study on the microstructural degradation and rejuvenation heat treatment of directionally solidified turbine blades

Journal of Alloys and Compounds, 2020
Abstract The directionally solidified Ni-based superalloy is used in gas turbine blades for advanced aircraft engines because of its high stability and favorable properties at elevated temperatures. The microstructures of superalloys degrade when they are exposed to long-term services, and the recovery of these damaged microstructures in a real ...
Peiyu Zhang   +5 more
openaire   +1 more source

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