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  1. 21

    INNOVATIVE APPROACH TO ENSURING THE QUALITY OF GAS TURBINE ENGINE PARTS PRODUCED BY SELECTIVE LASER SINTERING FOR UAV by Yevhen VYSHNEPOLSKYI, Dmytro PAVLENKO, Larysa TUMARCHENKO

    Published 2024-09-01
    “…The research objects are gas turbine engines parts, manufactured using an innovative method of additive manufacturing – selective laser sintering. …”
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    Article
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    Characterization of the stress-strain state in a gas turbine engine compressor disc taking into account damage accumulation by Natalia Boychenko, Ivan Ishtyryakov

    Published 2019-10-01
    “…A stress-strain state analysis of a gas turbine engine compressor disc was conducted with consideration to the accumulation of damages under various loading conditions in the temperature range. …”
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    Article
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    Numerical simulation of thermal barrier coating in gas turbine combustion chamber liner: a comparative study of YSZ and PSZ by S M Taseen Wahid, Rashidun Nessa Chowdhury, Jurana Monjur, Muammer Din Arif

    Published 2025-01-01
    “…This study investigates the potential of Yttria-Stabilized Zirconia (YSZ) and Partially Stabilized Zirconia (PSZ) thermal barrier coatings (TBCs) in improving gas turbine performance through a theoretical simulation. …”
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    Article
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    Simulation of Impinging Cooling Performance with Pin Fins and Mist Cooling Adopted in a Simplified Gas Turbine Transition Piece by Tao Xu, Hang Xiu, Junlou Li, Haichao Ge, Qing Shao, Guang Yang, Zhenglei Yu

    Published 2014-01-01
    “…The gas turbine transition piece was simplified to a one-four cylinder double chamber model with a single row of impinging holes in the outer wall. …”
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    Article
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    Accurate Reconstruction of Gas Turbine Blade Geometry Using 3D/2D Rigid-Registration and CT View Optimization by Hristo Valtchanov, Nicolas Piché, Vladimir Brailovski, Justin Byers, Catherine Desrosiers, François Guibault

    Published 2025-02-01
    “…In our study, we utilize a gas turbine blade as a case study, highlighting the significance of its internal flow channels. …”
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    Article
  12. 32

    Detailed Film Cooling Measurements over a Gas Turbine Blade Using a Transient Liquid Crystal Image Technique by Hui Du, Srinath V. Ekkad, Je-Chin Han, C. Pang Lee

    Published 2001-01-01
    “…Detailed heat transfer coefficient and film effectiveness distributions over a gas turbine blade with film cooling are obtained using a transient liquid crystal image technique. …”
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    Article
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    Effect of Turbulence Intensity on Cross-Injection Film Cooling at a Stepped or Smooth Endwall of a Gas Turbine Vane Passage by Pey-Shey Wu, Shen-Ta Tsai, Yue-Hua Jhuo

    Published 2014-01-01
    “…This study is concerned with a film cooling technique applicable to the protection of the endwalls of a gas turbine vane. In the experiments, cross-injection coolant flow from two-row, paired, inclined holes with nonintersecting centerlines was utilized. …”
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    Article
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    Deep Multiscale Soft-Threshold Support Vector Data Description for Enhanced Heavy-Duty Gas Turbine Generator Sets’ Anomaly Detection by Zhang Kun, Li Hongren, Wang Xin, Xie Daxing, Sun Xiaokai

    Published 2024-01-01
    “…The study concludes that DMS-SVDD presents a robust and efficient solution for gas turbine anomaly detection, with practical advantages for decision support in turbine maintenance. …”
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    Article
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    Influence of Compressor Station Waste-Heat Recovery Section on Operational Efficiency of Gas Turbine Drive with Isobaric Heat Supply and Regenerative Heat Utilization by A. P. Nesenchuk, V. N. Romaniuk, A. A. Abrazovsky, A. V. Begliak, T. V. Ryzhova, V. V. Begliak, R. O. Kuzmin

    Published 2013-08-01
    “…The paper considers an influence of waste heat recovery section on operational efficiency of gas turbine drive with regenerative heat utilization.…”
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    Article
  19. 39

    An example of use of gas turbine engine compressor, which has been mastered in production and has good characteristics in a new product project by A. V. Grekhnev

    Published 2022-12-01
    “…The development of a new gas turbine engine requires a lot of time and money spent on the design and testing its compressor, which has been shown as the most complex and time-consuming assembly unit of the engine. …”
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    Article
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