Results 31 to 40 of about 55 (51)
Experimental studies of a plasma enhancer for a dual-fuel gas turbine combustion chamber
Авіаційно-космічна техніка та технологіяPurpose. This study investigates the characteristics of a low-current plasma intensifier operating with air as the plasma-forming medium and the supply of a liquid phase simulating fuel, for potential application in dual-fuel gas turbine combustion ...
Serhiy Serbin +3 more
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CURRENT STATE OF THE PROBLEM OF THE DEVELOPMENT OF ACOUSTIC LINERS FOR GAS-TURBINE ENGINES
Авіаційно-космічна техніка та технологія, 2020 A review of current international aviation noise requirements is provided. It is shown that international requirements for aircraft noise levels are constantly increasing.
Євген Олександрович Римаренко
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PREDICTION OF THE INTER-ELEMENT INTERACTION IN THE AUTOMATIC CONTROL SYSTEMS OF AVIATION ENGINES
Авіаційно-космічна техніка та технологія, 2018 The article is devoted to the development of modern models and algorithms for information processing for the prediction, diagnosing and maintenance tasks of inter-element interaction in automatic control systems of aviation gas turbine engines ...
Сергій Сергійович Товкач
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Авіаційно-космічна техніка та технологіяThe energy independence problem of Ukraine is an urgent modern problem. Despite the full-scale war, Ukraine has managed to maintain a stable natural gas production level.
Valerii Kuznetsov +2 more
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Identification of dynamic characteristics of two-shaft turbofan engine
Авіаційно-космічна техніка та технологіяMathematical models are an important tool for designing engines and their automatic control systems. The models are used in the simulation modeling of the control object, in the analysis, synthesis, semi-realistic modeling, and in the synthesis of the ...
Oleksii Bondarenko
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INTERPRETATION OF VIBRATION SIGNALS OF COMPLEX ROTOR SYSTEM BASED ON FRACTAL ANALYSIS
Авіаційно-космічна техніка та технологія, 2019 The work analyzes vibration signals obtained by simulating a turbine of a complex rotor system, for example, an aviation gas turbine engine, under conditions of stationary and non-stationary excitations. Four modes of vibration excitation are considered:
Надія Іванівна Бурау +1 more
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LAWS OF MULTIPHASE FLOW BEHAVIOR IN THE HELICOPTER GAS TURBINE ENGINE INLET DUCT
Авіаційно-космічна техніка та технологія, 2017 The results of finite element modeling of the airflow contains dust particles of various sizes in the helicopter gas turbine engine air inlet duck with mounted and dismounted dust protective device are given.
Я. В. Двирник +1 more
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Авіаційно-космічна техніка та технологіяThis study presents an approach to the formalized construction of a diagnostic model for the TV3-117V gas turbine engine, aimed at post-flight analysis of operational data.
Andrii Dunai
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Topological optimization of the axial compressor blade of aircraft gas turbine engine
Авіаційно-космічна техніка та технологіяThe requirements for the efficiency, reliability, and environmental friendliness of technical systems in modern mechanical engineering are constantly increasing.
Maryna Pikul +3 more
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ПІДВИЩЕННЯ ХАРАКТЕРИСТИК НАДІЙНОСТІ ПІДШИПНИКІВ РОТОРІВ АВІАЦІЙНИХ ГАЗОТУРБІННИХ ДВИГУНІВ
Наука і техніка Повітряних Сил Збройних Сил УкраїниПроведено аналіз причин виникнення дефектів підшипників (ПШ) роторів авіаційних газотурбінних двигунів (ГТД), головних причин їх пошкоджень та руйнування.
І.Б. Ковтонюк +4 more
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