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https://dx.doi.org/10.18720/sp...

Other literature type . 2020

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Ð“Ð°Ð·Ð¾Ñ‚ÑƒÑ€Ð±Ð¸Ð½Ð½Ð°Ñ ÑƒÑÑ‚Ð°Ð½Ð¾Ð²ÐºÐ° Ð¼Ð¾Ñ‰Ð½Ð¾ÑÑ‚ÑŒÑŽ 16,8 ÐœÐ’Ñ‚

descriptionPublicationkeyboard_double_arrow_right Other literature type 01 Jan 2020 Russian Publisher:Ð¡Ð°Ð½ÐºÑ-ÐÐµÑÐµÑÐ±ÑÑÐ³ÑÐºÐ¸Ð¹ Ð¿Ð¾Ð»Ð¸ÑÐµÑÐ½Ð¸ÑÐµÑÐºÐ¸Ð¹ ÑÐ½Ð¸Ð²ÐµÑÑÐ¸ÑÐµÑ ÐÐµÑÑÐ° ÐÐµÐ»Ð¸ÐºÐ¾Ð³Ð¾

doi: 10.18720/spbpu/3/2020/vr/vr20-5465

Ð“Ð°Ð·Ð¾Ñ‚ÑƒÑ€Ð±Ð¸Ð½Ð½Ð°Ñ ÑƒÑÑ‚Ð°Ð½Ð¾Ð²ÐºÐ° Ð¼Ð¾Ñ‰Ð½Ð¾ÑÑ‚ÑŒÑŽ 16,8 ÐœÐ’Ñ‚

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Abstract

This paper includes the methods of designing a gas turbine unit (GTU) with a capacity of 16.8 MW based on the previously developed gas turbine unit of the al-31ST prototype are analyzed. it also provides a General description of the developed installation and its design features. Calculated thermal scheme, an approximate calculation of the low-pressure compressor (KND) and a high pressure compressor (HPC), the calculation of the combustion chamber (CC), detailed the calculation flow of the high-pressure turbine (HPT), low pressure turbine (LPT) and power turbine (PT), the calculation of the spin flow in the last stage PT, the calculation of the strength of the rotor of PT.

Keywords

ÐºÐ°Ð¼ÐµÑÐ° ÑÐ³Ð¾ÑÐ°Ð½Ð¸Ñ, turbine, combustion chamber, ÐºÐ¾Ð¼Ð¿ÑÐµÑÑÐ¾Ñ, compressor, ÑÑÑÐ±Ð¸Ð½Ð°

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	citations This is an alternative to the "Influence" indicator, which also reflects the overall/total impact of an article in the research community at large, based on the underlying citation network (diachronically).	0
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	influence This indicator reflects the overall/total impact of an article in the research community at large, based on the underlying citation network (diachronically).	Average
	impulse This indicator reflects the initial momentum of an article directly after its publication, based on the underlying citation network.	Average