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

Z Sun, X Jiang, C Qiu, S Cheng, X Liu, H Li… - Journal of Alloys and …, 2023 - Elsevier
Directionally solidified gas turbine blades are wildly used in land-based industrial gas
turbines for power generation. During long-term service, the harsh service environment …

[PDF][PDF] Failure mechanisms in turbine blades of a gas turbine Engine—An overview

N Rao, N Kumar, B Prasad, N Madhulata… - Int. J. Eng. Res …, 2014 - researchgate.net
For the past few decades, the gas turbines have been operated at elevated temperatures to
have the advantage of achieving higher and higher power output and engine efficiency. The …

Effect of thermal exposure on the microstructure and creep properties of a fourth-generation Ni-based single crystal superalloy

Y Huang, X Wang, C Cui, Z Tan, J Li, Y Yang… - Journal of Materials …, 2021 - Elsevier
The effect of thermal exposure on microstructure and creep properties of a fourth-generation
nickel-based single crystal superalloy was investigated. The thermal exposure of samples …

The effect of stress on primary MC carbides degeneration of Waspaloy during long term thermal exposure

X Chen, Z Yao, J Dong, H Shen, Y Wang - Journal of Alloys and …, 2018 - Elsevier
Microstructure evolution during long-term thermal exposure and stress rupture in Waspaloy
was investigated in detail. During thermal and stress exposure, γ′ phase and grain …

Assessment of service induced degradation of microstructure and properties in turbine blades made of GH4037 alloy

J Tong, X Ding, M Wang, K Yagi, Y Zheng… - Journal of Alloys and …, 2016 - Elsevier
Abstract Service lives of turbine blades are closely related to microstructural degradation
introduced by normal and overheating service exposures. However, comparative …

The effect of thermal exposure on the properties of a Ni-base superalloy

M Aghaie-Khafri, M Hajjavady - Materials Science and Engineering: A, 2008 - Elsevier
The effect of 1000h thermal exposure on the microstructural instability and mechanical
properties degradation of IN738C at 850° C were investigated by means of TEM, SEM and …

Failure analysis of gas turbine blades in a gas turbine engine used for marine applications

VNB Rao, INN Kumar, KB Prasad - International Journal of Engineering …, 2014 - ajol.info
High pressure temperature (HPT) turbine blade is the most important component of the gas
turbine and failures in this turbine blade can have dramatic effect on the safety and …

Microstructure and wear resistance of one-step in-situ synthesized TiN/Al composite coatings on Ti6Al4V alloy by a laser nitriding process

Y Fu, XC Zhang, JF Sui, ST Tu, FZ Xuan… - Optics & Laser …, 2015 - Elsevier
The aim of this paper was to develop a one-step in situ method to synthesize the TiN
reinforced Al metallic matrix composite coatings on Ti6Al4V alloy. In this method, the Al …

On the failure behavior of fifth stage gas turbine blade

AF Sheykhlari, SK Moghanaki, M Moattari… - Engineering Failure …, 2020 - Elsevier
In the present study, the failure of a fifth stage blade of a gas turbine after 500 equivalent
operation hours is investigated. After hot gas path inspection, it was found that an airfoil of a …

CM88Y superalloy blade metallurgical degradation in a gas turbine

M Najmi, SMH Mirbagheri - Engineering Failure Analysis, 2023 - Elsevier
The failure of first-stage blades in a 25 MW gas turbine, made of CM88Y nickel-based
superalloy were studied by metallurgical approaches. The blades were examined visually …