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Journal articles on the topic 'Газотурбінний двигун gas turbine engine'

Author: Grafiati

Published: 30 May 2022

Last updated: 31 July 2025

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1

Tovkach, Serhii. "Закони керування авіаційним газотурбінним двигуном з турбовентиляторною приставкою". Aerospace Technic and Technology, № 4sup1 (24 серпня 2023): 70–74. http://dx.doi.org/10.32620/aktt.2023.4sup1.10.

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The main aspects of the general task of integrating an aviation engine (AE) with a turbofan additional unit (TAU) of a multi-mode aircraft are the selection of the scheme and design parameters of the AE with the TAU (including parameters of the work process), as well as methods and means of automatic control of the AE with the TAU for better matching its characteristics with certain flight modes. These two tasks are closely interrelated: on the one hand, when determining the appearance of the aircraft and its power plant (PP), it is necessary to consider what means will ensure the adaptation o

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2

Nerubaskyi, Vadym. "Ринок та перспективи газотурбінних двигунів для надважких транспортних гелікоптерів". Aerospace Technic and Technology, № 4sup1 (29 серпня 2024): 5–11. http://dx.doi.org/10.32620/aktt.2024.4sup1.01.

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The introductory part of the article provides brief information about the main activity of Element JSC – the development and production of electronic control systems for aircraft engines, in particular, the RDC-450M ECU family for turboshaft gas turbine engines AI-450M, MS-500V, TV3-117VMA-SBM-1V, and others, created by SE Ivchenko-Progres and Motor Sich JSC. Element JSC, with its partners, has been involved in Ukrainian helicopter industry for more than 25 years. In the next section, the classification of helicopters is given, and the segment of super-heavy helicopters with gas turbine engine

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3

Nerubaskyi, Vadym. "Ринок та перспективи газотурбінних двигунів для важких транспортних гелікоптерів". Aerospace Technic and Technology, № 4sup1 (24 серпня 2023): 5–11. http://dx.doi.org/10.32620/aktt.2023.4sup1.01.

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The subject of this study is the current state of the market and prospects for the development of heavy transport helicopters and their power plants. This article provides a classification of helicopters and a segment of medium-heavy and heavy helicopters with gas turbine engines. The field of application of such helicopters is briefly described. The purpose of this article is to evaluate the activities of Element JSC in the field of developing electronic control systems for gas turbine engines for heavy class helicopters. Such systems for Element JSC, in particular, are RDTs-2500 and RDTs-450

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4

Kvasha, Yu A. "Calculation of a 3D turbulent flow in aircraft gas turbine engine ducts." Technical mechanics 2020, no. 4 (2020): 65–71. http://dx.doi.org/10.15407/itm2020.04.065.

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This work is devoted to the development of approaches to the numerical simulation of 3D turbulent gas flows in different ducts of aircraft gas turbine engines, in particular in inlet device ducts. Inlet devices must provide large values of the total pressure recovery factor and flow uniformity at the engine compressor inlet. The aim of this work is the verification of the operability of a technique developed earlier for the calculation of the parameters of a 3D turbulent flow in complex-shape ducts. The basic approach is a numerical simulation of 3D turbulent gas flows on the basis of the comp

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5

Katrenko, M. O., H. O. Strelnikov, and N. S. Pryadko. "Experience in the design of small-size gas-turbine engines for unmanned aerial vehicles." Technical mechanics 2025, no. 2 (2025): 35–49. https://doi.org/10.15407/itm2025.02.035.

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This paper is concerned with low-thrust air-feed jet engines, which are used in unmanned and manned aerial vehicles, power plants, etc. The paper presents an overview of existing aerial vehicles that use low-thrust air-feed jet engines of various types. Consideration is given to the basic construction and schematic diagrams of gas-turbine engines of thrust 100 to 3,000 N. Experience in the design, making, and operation of air-feed jet engines as a part of unmanned aerial vehicles for various purposes is overviewed. The features of existing low-thrust engines are identified. It is shown that pa

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6

Yepifanov, Sergiy, та Oleksii Bondarenko. "Формування динамічних моделей газотурбінних двигунів для використання в системах автоматичного керування та контролю". Aerospace Technic and Technology, № 4 (24 серпня 2023): 50–61. http://dx.doi.org/10.32620/aktt.2023.4.06.

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The subject of the study is the process of forming a mathematical model (MM) of an aviation gas turbine engine, which provides the calculation of parameters of the work process in stable and transient operating modes for use in the evaluation of dynamic characteristics, in the analysis and synthesis of automatic engine and aircraft control systems, as part of aviation simulators, and in on-board control and diagnostics algorithms. The goal is to substantiate the structure and methodology of MM formation, intended for use in real and accelerated time scale systems. Task: formulation of requirem

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7

Зданевич, Володимир, Олег Маслій, Сергій Янюк, Валерій Маліков та Олександр Фролов. "ОСОБЛИВОСТІ ЗАСТОСУВАННЯ РЕАКТИВНИХ ПАЛИВ ДЛЯ АВІАЦІЙНИХ ГАЗОТУРБІННИХ ДВИГУНІВ". Collection of scientific works of Odesa Military Academy, № 18 (3 березня 2023): 55–60. http://dx.doi.org/10.37129/2313-7509.2022.18.55-60.

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The purpose of this article is to study the features of the usage of jet fuels for aviation gas turbine engines and the importance of the chymotology for the study of aviation kerosene and technical fluids usage in the of modern aviation technology. The role of practical aviation chymotology in ensuring reliable operation of aviation equipment and functional application of fuel and lubricants and technical fluids in existing and future aviation equipment is revealed in the work. In the present time jet fuels of both domestic and foreign production are supplied to meet the needs of the Air Forc

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8

Kvasha, Yu A., N. A. Zinevych, and N. V. Petrushenko. "Features of blade shape variation in the aerodynamic improvement of aircraft gas-turbine engine compressors." Technical mechanics 2022, no. 2 (2022): 17–24. http://dx.doi.org/10.15407/itm2022.02.017.

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This work is devoted to the development of procedures for the aerodynamic improvement of gas-turbine engine axial-flow compressor blade rows. The aim of the work is to compare the efficiency of two methods for impeller blade shape variation in the aerodynamic improvement of an aircraft gas-turbine engine two-stage fan. The first method consists only in varying the blade profile angle along the blade height, while the second consists in varying the blade profile angle and geometrical parameters. The features of the approach used in the solution of this problem are as follows: formulating qualit

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9

Yepifanov, Sergiy, та Oleksii Bondarenko. "Метод визначення невимірюваних параметрів газотурбінних двигунів з урахуванням зміни технічного стану". Aerospace Technic and Technology, № 2 (21 березня 2025): 25–37. https://doi.org/10.32620/aktt.2025.2.03.

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The subject of this study is the estimation of non-measurable parameters of a gas turbine engine's operating process based on a limited set of measured parameters. The relevance of this research arises from the practical impossibility of measuring several critical engine parameters under operating conditions, such as thrust, turbine inlet gas temperature, among others, which are essential for control and diagnostics tasks. These parameters must be continuously estimated using only limited available data. This requires the use of a mathematical model of the engine's operating process, with cons

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10

Миргород, В. Ф., та И. М. Гвоздева. "ПІДВИЩЕННЯ ЕФЕКТИВНОСТІ МЕТОДІВ ТРЕНДОВОГО АНАЛІЗУ І КОНТРОЛЮ ПРИ АНАЛІЗІ ТЕХНІЧНОГО СТАНУ ГАЗОТУРБІННИХ ДВИГУНІВ". Aerospace Technic and Technology, № 7 (7 липня 2017): 151–56. http://dx.doi.org/10.32620/aktt.2017.7.21.

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The paper suggests an approach to joint trend analysis and trend monitoring of time series formed by the parameters of gas-turbine engines technical conditions in their long-term operation. The proposed approach is based on forming the diagnostic model in the form of a polynomial approximation of the throttle characteristics for the reference motor and selecting the deviations from this model. For the obtained multidimensional time series of deviations from the diagnostic model, the known methods of trend analysis and trend monitoring are consistently applied. The proposed approach makes it po

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11

Kvasnytska, K. H. "WAYS TO ELIMINATE THE SHORTCOMINGS OF THE TECHNOLOGY OF CASTING PARTS OF GAS TURBINE ENGINES." Casting processes 159, no. 1 (2025): 22–33. https://doi.org/10.15407/plit2025.01.022.

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12

Калініна, Наталія Євграфівна, Олександр Васильович Калінін, Тетяна Валеріївна Носова, Стелла Ігорівна Мамчур та Наталія Іванівна Цокур. "Розробка технології дисперсного модифікування жароміцних нікелевих сплавів для лопаток газотурбінних двигунів". Aerospace technic and technology, № 3 (27 травня 2021): 49–53. http://dx.doi.org/10.32620/aktt.2021.3.06.

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The paper proposes means of improving the properties of nickel alloys for aircraft gas turbine engines by improving the existing alloys. The efficiency of an aircraft engine depends on the quality of the turbine rotor blades, which are made of heat-resistant alloys. According to the studies, the obtained results of pilot tests of a complex of mechanical properties, high-temperature corrosion of a multicomponent high-temperature nickel alloy ХН59МВТКЮЛ (Ni-Cr-W-Co-Al-Ti-Mo systems). The paper proposes the use of modifiers. An effective means of dispersing the structural components of alloys at

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13

Vyshnepolskyi, E. V., D. V. Pavlenko, M. V. Sidorenko, and A. A. Pysarskyi. "Determination the residual stresses in the surface layer of gas turbine engine parts by small hole drilling." Metaloznavstvo ta obrobka metalìv 95, no. 3 (2020): 69–75. http://dx.doi.org/10.15407/mom2020.03.069.

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14

Donets, S. E., V. F. Klepikov, V. V. Lytvynenko, et al. "Testing of gas-turbine blades engines using the accelerator of high current relativistic electrons." Nuclear Physics and Atomic Energy 21, no. 1 (2020): 95–100. http://dx.doi.org/10.15407/jnpae2020.01.095.

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15

Nemanezhyn, Yevhen, Gennadiy Lvov та Yuriy Torba. "Оцінка впливу анізотропних властивостей монокристалічних лопаток турбін авіаційних газотурбінних двигунів на їх довготривалу міцність". Aerospace Technic and Technology, № 4sup2 (29 серпня 2024): 39–51. http://dx.doi.org/10.32620/aktt.2024.4sup2.06.

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Long-term static strength is one of the most important parameters to be calculated at the life-time design stage of aircraft engine turbine blades. The importance of studying and modeling this parameter is based on many factors. In particular, it should be noted that one of these factors is the peculiarities of the anisotropic characteristics of single-crystal turbine blades made of nickel heat-resistant alloys for a wide temperature and power load range. Another important factor is the different crystallographic orientations of the single crystals. The analysis of the literature has shown tha

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16

Tovkach, Serhii. "Контури керування і обмеження для побудови системи автоматичного керування авіаційним газотурбінним двигуном". Aerospace technic and technology, № 4sup2 (22 серпня 2022): 68–72. http://dx.doi.org/10.32620/aktt.2022.4sup2.10.

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The choice of programs and control algorithms for ACS determines the possibility of implementation in the engine of the expectancy in the construction of thermodynamic and strength characteristics. For the set modes of operation of the engine limit values of frequency of rotation of rotors of gas temperature , air pressure behind the compressor are defined; on transient modes the size and duration of exceedances by parameters of their maximum admissible values on the set operating modes is limited. The parameters of the GTE adjustment should be chosen so that they characterize the optimality a

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17

Borysov, Yu S., N. V. Vihilianska, O. M. Burlachenko, L. P. Olevska, and V. M. Lopata. "Analysis of modern experience in development of sealing coatings for parts of gas turbine engines (Review)." Avtomatičeskaâ svarka (Kiev) 2022, no. 4 (2022): 41–49. http://dx.doi.org/10.37434/as2022.04.06.

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18

Greshta, V. L., D. V. Tkach, Ye H. Sotnikov, O. V. Klymov, and Ye O. Fasol. "The prospect of using nickel-based sealing coatings in the hot tract of gas turbine engines." Metaloznavstvo ta obrobka metalìv 95, no. 3 (2020): 88–94. http://dx.doi.org/10.15407/mom2020.03.088.

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19

Kovalenko, D. V., I. V. Kovalenko, B. O. Zaderii, and G. V. Zvyagintseva. "Application of A-TIG welding for improving the technology of manufacturing and repair of units of gas turbine engines and installations from titanium alloys." Avtomatičeskaâ svarka (Kiev) 2022, no. 10 (2022): 7–16. http://dx.doi.org/10.37434/as2022.10.01.

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20

Rymarenko, Yevhen. "Дослідження акустичних характеристик дослідних зразків звукопоглинаючих конструкцій для газотурбінних двигунів". Aerospace technic and technology, № 4sup2 (22 серпня 2022). http://dx.doi.org/10.32620/aktt.2022.4sup2.05.

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It is shown that the problem of aviation noise affecting the population near airports is still relevant. Pollution from aircraft noise is not a less influential factor than air or water pollution. The international community is paying close attention to tackling aviation noise by introducing requirements and noise limits for aircraft under development or in operation. Among the sources of aircraft noise, one of the main sources that should be singled out - the noise generated by gas turbine engines. Among the sources of noise of gas turbine engines should be noted to highlight the noise of the

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