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1. Failure Analysis of Compressor IGV in 9F Gas Turbine Generator Unit

   Several compressor inlet guide vanes (IGV) with cracks of 9F gas turbine generator unit have been found fractured during the inspection process. The...

   Shuchao Gu, Dong An, ... Yuzhe Liu in Journal of Failure Analysis and Prevention

   Article 13 July 2022
   

2. Structural and Mechanical Properties of the Nickel Alloy of Gas-Turbine Engine Blades

   We analyze the influence of structure on the physicomechanical properties of a refractory corrosionresistant alloy doped with rhenium and tantalum...

   Y. H. Kvasnytska, L. M. Ivaskevich, ... H. P. Mialnitsa in Materials Science

   Article 01 March 2022
   

3. Fatigue Life Analysis Based on Transition State Parameters of Turbine Blades

   ANSYS finite element analysis software is used to calculate the fatigue life of a certain turbine blade during the thermal shock process in this...

   Yingtao Chen, **nlong Yang, ... Wanlin Zhang in Journal of Failure Analysis and Prevention

   Article 02 July 2024
   

4. Materials for Gas Turbine Engines: Present Status, Future Trends and Indigenous Efforts

   Gas turbine engines ingest air from the ambient atmosphere and produce power using the energy of the combustion products of the highly compressed air...

   Swati Biswas, S. Ramachandra, ... S. P. Suresh Kumar in Journal of the Indian Institute of Science

   Article 01 January 2022
   

5. Fatigue Fracture of the Blades of Gas-Turbine Engines Made of a New Refractory Nickel Alloy

   We perform experimental investigations of the fatigue fracture of turbine blades in the second stage of power gas-turbine engines. The blades were...

   O. I. Balitskii, Yu. H. Kvasnytska, ... K. H. Kvasnytska in Materials Science

   Article 01 January 2022
   

6. Failure Analysis of a V94.2 Gas Turbine Inner Casing

   During operation, hot combustion products are passed through the inner casing from combustion chamber to gas turbine. Therefore, this part is exposed...

   Mohsen Mehdizadeh, Masumeh Rayatpour, Zahra Lalegani in Journal of Failure Analysis and Prevention

   Article 23 August 2021
   

7. Improving the Microstructure and Wear Behavior of Gas Turbine Compressor Parts Through the Application of FeCoNiCuAl–WC High Entropy Composite Coating by Laser Cladding

   To improve the wear resistance properties of gas turbine compressor parts, a high entropy alloy (HEA) coating of FeCoNiCuAl with 60% WC ceramic...

   **guo Zhao, Morteza Taheri, ... Mohammad Ali Palay in Metals and Materials International

   Article 07 October 2023
   

8. Influence of Thermal Barrier Coatings on the Dam** of GTE Turbine Blade Vibrations

   Abstract —The characteristics that confirm the positive effect of thermal barrier coatings on the rotor blades of gas turbine engines, which are made...

   N. V. Abraimov in Russian Metallurgy (Metally)

   Article 01 June 2023
   

9. Heat Transfer, Thermal Stress and Failure Inspection of a Gas Turbine Compressor Stator Blade Made of Five Different Conventional Superalloys and Ultra-High-Temperature Ceramic Material: A Direct Numerical Investigation

   Probing the efficiency of Brayton cycle is of great importance to harbor maximum output from gas turbines. The efficiency of Brayton cycle largely...

   Abyaz Abid, Md Tanbir Sarowar in Journal of Failure Analysis and Prevention

   Article 24 May 2022
   

10. A Review on Coating and Finite Element Analysis for Optimization Gas Turbine

    The efficiency of gas turbines plays a big role in power generation for electricity. The operating hours for a general gas turbine are non-stop...

    Ahmad Aliff Syakir Azman, Mariyam Jameelah Ghazali, ... Ahmad Afiq Pauzi in Proceedings of the 3rd Malaysian International Tribology Conference

    Conference paper 2022
    

11. Effect of Alloying Elements on the Strength Properties of Nickel Superalloys for Gas Turbine Disks

    Abstract

    More than 150 industrial and experimental nickel superalloys are analyzed to construct analytical composition–property relationships for...

    A. V. Logunov, Yu. N. Shmotin, ... D. V. Danilov in Russian Metallurgy (Metally)

    Article 01 December 2021
    

12. Recent Advances in Alloy Development for Metal Additive Manufacturing in Gas Turbine/Aerospace Applications: A Review

    A dozen or so alloys have been occupying the alloy landscape in metal additive manufacturing (MAM) in terms of addressing all aspects of research,...

    Dheepa Srinivasan, Kiruthika Ananth in Journal of the Indian Institute of Science

    Article 01 January 2022
    

13. High-temperature oxidation-resistant glass–ceramic/YSZ composite coatings for gas turbine engine applications

    Oxidation behavior of a novel double-layered thermal barrier coating (TBC) system consisting of glass–ceramic–25 wt.% yttria-stabilized zirconia...

    K. Parthiban, Sumana Ghosh in Journal of the Korean Ceramic Society

    Article 22 February 2024
    

14. Influence of Microalloying Elements on the Structures and Properties of Thermal Barrier Coatings on Gas Turbine Blades

    Abstract —The mechanisms of alloying with hafnium of protective thermal barrier coatings on nickel superalloys are studied. The mechanism of hafnium...

    N. V. Abraimov, I. G. Petukhov, V. V. Orekhova in Russian Metallurgy (Metally)

    Article 01 June 2023
    

15. Microstructural Investigation and Determining the Optimal Conditions for Nondestructive Testing of Inconel 738LC Superalloy Gas Turbine Blade

    The optimal conditions for nondestructive testing replication of an IN738LC gas turbine blade have determined. Elcoat 37 coating on IN738LC gas...

    Masumeh Rayatpour, Zahra Lalegani in Journal of Failure Analysis and Prevention

    Article 27 July 2021
    

16. Airworthiness Qualification of a High-Pressure Turbine Disk for a Low Bypass Turbofan Engine

    A single stage high-pressure turbine disk has been designed for a low bypass turbofan engine. The turbine disk operates at extreme operating...

    R. K. Mishra, Vinay Kumar, M. Selva Subramanian in Journal of Failure Analysis and Prevention

    Article 31 December 2022
    

17. Effect of Cryogenic Treatment After Full Solution on Rejuvenation of Exposed IN738LC Gas Turbine Blade

    In this research, the samples were exposed to full and partial solution heat treatments and quenched in the air and nitrogen each period. Also, one...

    Mohsen Samiee, Yazdan Shajari, ... Zahra Sadat Seyedraoufi in Metallography, Microstructure, and Analysis

    Article 20 December 2022
    

18. Protective Coatings for the III–IV Generation Turbine Blades

    Abstract

    The properties and methods of forming of β(NiAl)Zr and β(NiAl)SiMo (SHS) aluminide coatings are considered to protect the III–IV generation...

    V. M. Samoilenko, A. N. Aksenov, ... V. G. Opokin in Russian Metallurgy (Metally)

    Article 01 June 2023
    

19. Integrating State of the Art Zirconia Thermal Barriers with Ytterbium Silicate Environmental Barriers for Silicon-Based Ceramic Turbine Components

    As gas turbine firing temperatures continue to increase for the sake of improved operating efficiency, the material's transition from Ni-based...

    Edward J. Gildersleeve V, Emine Bakan, Robert Vaßen in Journal of Thermal Spray Technology

    Article Open access 30 November 2023
    

20. Failure Analysis of Air Tube Inlets in a High-Speed Power Turbine

    The present study was conducted to investigate the root cause failure analysis of 316L stainless steel air tube inlets at the weld joint in a...

    H. R. Lashgari in Journal of Failure Analysis and Prevention

    Article 27 March 2024