Academic literature on the topic 'Thermogasdynamic compression'
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Journal articles on the topic "Thermogasdynamic compression"
Kobalava, H., and D. Konovalov. "Numerical simulation of the regime and geometric characteristics influence on the pressure loss of a low-flow aerothermopressor." Refrigeration Engineering and Technology 55, no. 2 (April 30, 2019): 66–76. http://dx.doi.org/10.15673/ret.v55i2.1355.
Full textКоновалов, Дмитро Вікторович, and Галина Олександрівна Кобалава. "ПРОМІЖНЕ ОХОЛОДЖЕННЯ ЦИКЛОВОГО ПОВІТРЯ В ГАЗОТУРБІННИХ УСТАНОВКАХ АЕРОТЕРМОПРЕСОРАМИ." Aerospace technic and technology, no. 1 (February 25, 2018): 29–36. http://dx.doi.org/10.32620/aktt.2018.1.02.
Full textКоновалов, Дмитро Вікторович, and Галина Олександрівна Кобалава. "ЧИСЕЛЬНЕ МОДЕЛЮВАННЯ ПРОТОЧНОЇ ЧАСТИНИ МАЛОВИТРАТНОГО АЕРОТЕРМОПРЕСОРА ДЛЯ ПРОМІЖНОГО ОХОЛОДЖЕННЯ ЦИКЛОВОГО ПОВІТРЯ ГАЗОТУРБІННОГО ДВИГУНА." Aerospace technic and technology, no. 4 (August 31, 2019): 31–38. http://dx.doi.org/10.32620/aktt.2019.4.06.
Full textКоновалов, Дмитро Вікторович. "АНАЛІЗ ЕФЕКТИВНОСТІ ТЕПЛОВИКОРИСТОВУЮЧОЇ ТЕРМОПРЕСОРНО-ЕЖЕКТОРНОЇ ХОЛОДИЛЬНОЇ МАШИНИ." Aerospace technic and technology, no. 8 (August 31, 2019): 59–67. http://dx.doi.org/10.32620/aktt.2019.8.09.
Full textКоновалов, Дмитро Вікторович, Роман Миколайович Радченко, Сергій Георгійович Фордуй, Віктор Павлович Халдобін, Олексій Олегович Зєліков, and Олександр Анатолійович Різун. "ВДОСКОНАЛЕННЯ ТЕПЛОВИКОРИСТОВУЮЧИХ ЕЖЕКТОРНИХ ХОЛОДИЛЬНИХ МАШИН ЗАСТОСУВАННЯМ АЕРОТЕРМОПРЕСОРНИХ ТЕХНОЛОГІЙ." Aerospace technic and technology, no. 1 (February 26, 2021): 60–66. http://dx.doi.org/10.32620/aktt.2021.1.06.
Full textКобалава, Галина Олександрівна. "ВИЗНАЧЕННЯ КОНСТРУКТИВНИХ ПАРАМЕТРІВ ПРОТОЧНОЇ ЧАСТИНИ АЕРОТЕРМОПРЕСОРА СИСТЕМИ ОХОЛОДЖЕННЯ ЦИКЛОВОГО ПОВІТРЯ МІКРОТУРБІН." Aerospace technic and technology, no. 2 (April 22, 2019): 44–50. http://dx.doi.org/10.32620/aktt.2019.2.05.
Full textBoyko, Ludmila, Vadym Datsenko, Aleksandr Dyomin, and Nataliya Pizhankova. "Devising a method for calculating the turboshaft gas turbine engine performance involving a blade-by-blade description of the multi-stage compressor in a two-dimensional setting." Eastern-European Journal of Enterprise Technologies 4, no. 8(112) (August 31, 2021): 59–66. http://dx.doi.org/10.15587/1729-4061.2021.238538.
Full textBlinov, V. L., and G. A. Deryabin. "Technical Condition Estimation of the Gas Turbine Axial Compressor." IOP Conference Series: Earth and Environmental Science 990, no. 1 (February 1, 2022): 012037. http://dx.doi.org/10.1088/1755-1315/990/1/012037.
Full textShabarov, Alexander B., Alexander M. Moiseev, Mikhail S. Belov, and Andrey A. Achimov. "INFORMATION SYSTEM OF THE TEST BENCH FOR DRIVING GAS TURBINE ENGINES." Tyumen State University Herald. Physical and Mathematical Modeling. Oil, Gas, Energy 6, no. 4 (2020): 28–47. http://dx.doi.org/10.21684/2411-7978-2020-6-4-28-47.
Full textБойко, Людмила Георгиевна, Олег Владимирович Кислов, and Наталия Владимировна Пижанкова. "МЕТОД РАСЧЕТА ТЕРМОГАЗОДИНАМИЧЕСКИХ ПАРАМЕТРОВ ТУРБОВАЛЬНОГО ГТД НА ОСНОВЕ ПОВЕНЦОВОГО ОПИСАНИЯ ЛОПАТОЧНЫХ МАШИН. ЧАСТЬ 1. ОСНОВНЫЕ УРАВНЕНИЯ." Aerospace technic and technology, no. 1 (February 25, 2018): 48–58. http://dx.doi.org/10.32620/aktt.2018.1.05.
Full textDissertations / Theses on the topic "Thermogasdynamic compression"
Сорін, В. Д. "Вихровий компресор для наддуву повітря в топку згорання на ТЕЦ." Master's thesis, Сумський державний університет, 2021. https://essuir.sumdu.edu.ua/handle/123456789/86615.
Full textВ работе выполнен расчет одноступенчатого вихревого компрессора и определен диаметр рабочего колеса. С целью уменьшения габаритных размеров выполнен расчет двухступенчатого вихревого компрессора с разными диаметрами рабочих колес первой и второй ступеней. Выполнен анализ полученных результатов и выбрана оптимальная конструкция для предлагаемых исходных данных. В разделе охраны труда выполнен анализ вредных и опасных факторов при эксплуатации вихревых компрессоров и расчет шумоглушителя.
In this work, the calculation of a single-stage vortex compressor is carried out and the diameter of the impeller is determined. In order to reduce the overall dimensions, a calculation was made for a two-stage vortex compressor with different diameters of the impellers of the first and second stages. The analysis of the obtained results is carried out and the optimal design for the proposed initial data is selected. In the labor protection section, the analysis of harmful and hazardous factors during the operation of vortex compressors and the calculation of the silencer are carried out.
Konovalov, Dmytro, Eugeniy Trushliakov, Mykola Radchenko, Halina Kobalava, and Vitaliy Maksymov. "Research of the Aerothermopressor Cooling System of Charge Air of a Marine Internal Combustion Engine Under Variable Climatic Conditions of Operation." Thesis, 2020. https://doi.org/10.1007/978-3-030-40724-7_53.
Full textAbstract. Principle of charge air cooling of the internal combustion engine with an aerothermopressor is proposed. It is implemented on the transport ship regular line. Arising thermogasdynamic compression allows increasing the air pressure. The aerothermopressor application in the charge air cooling systems makes it possible to reduce the power consumed by compressors, Nc by 3–10 %, thereby the engine power is increased by 1–3 % and the specific fuel consumption is decreased by 2–4 %. It is established that in case of increasing the ambient air temperature tamb at the turbocharger input the effect from the aerothermopressor used for cooling of the charge air is increased: the turbocharger power reduction DNC is increased with a corresponding increase in engine power and a decrease in specific fuel consumption. The relative (related to air flow) water mass flow is determined, which has to be injected at completely evaporated in a thermal overpressure: 0.02–0.05 (2–5 %).
Conference papers on the topic "Thermogasdynamic compression"
Baturin, Oleg, Andrei Tkachenko, Ilia Krupenich, Grigorii Popov, and Eugene Goryachkin. "Identifying the Approach to Significantly Improve the Performance of NK-36ST Gas Turbine Power Plant." In ASME Turbo Expo 2017: Turbomachinery Technical Conference and Exposition. American Society of Mechanical Engineers, 2017. http://dx.doi.org/10.1115/gt2017-64836.
Full textVinogradov, Alexandr S., and Renat R. Badykov. "Influence of Labyrinth Seal Leakage on the Turbine Support Cooling." In ASME 2014 Gas Turbine India Conference. American Society of Mechanical Engineers, 2014. http://dx.doi.org/10.1115/gtindia2014-8172.
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