title: ÐÑÑÐ»ÐµÐ´Ð¾Ð²Ð°Ð½Ð¸Ðµ ÑÐµÑÐ¼Ð¾Ð´Ð¸Ð½Ð°Ð¼Ð¸ÑÐµÑÐºÐ¸Ñ Ñ Ð°ÑÐ°ÐºÑÐµÑÐ¸ÑÑÐ¸Ðº Ð¾ÑÐµÐ²Ð¾Ð³Ð¾ ÐºÐ¾Ð¼Ð¿ÑÐµÑÑÐ¾ÑÐ° Ð¿ÑÐ¸ÑÐ¾Ð´Ð½Ð¾Ð³Ð¾ Ð³Ð°Ð·Ð° Ð½Ð° Ð¾ÑÐ½Ð¾Ð²Ðµ Ð¼Ð¾Ð´ÐµÐ»ÑÐ½Ð¾Ð¹ ÑÑÑÐ¿ÐµÐ½Ð¸ Ð-100-2Ð»
title: Ð²ÑÐ¿ÑÑÐºÐ½Ð°Ñ ÐºÐ²Ð°Ð»Ð¸ÑÐ¸ÐºÐ°ÑÐ¸Ð¾Ð½Ð½Ð°Ñ ÑÐ°Ð±Ð¾ÑÐ° Ð¼Ð°Ð³Ð¸ÑÑÑÐ°
titleType: Subtitle
title: Study of thermodynamic characteristics of axial natural gas compressors based on the K-100-2l stage model
Creators: name: ÐÐ¾ÑÑÐ¸Ð½, ÐÐ¾Ð½ÑÑÐ°Ð½ÑÐ¸Ð½
Publisher: name: Ð¡Ð°Ð½ÐºÑ-ÐÐµÑÐµÑÐ±ÑÑÐ³ÑÐºÐ¸Ð¹ Ð¿Ð¾Ð»Ð¸ÑÐµÑÐ½Ð¸ÑÐµÑÐºÐ¸Ð¹ ÑÐ½Ð¸Ð²ÐµÑÑÐ¸ÑÐµÑ ÐÐµÑÑÐ° ÐÐµÐ»Ð¸ÐºÐ¾Ð³Ð¾
Year: 2019
Subjects: Ð¾ÑÐµÐ²Ð¾Ð¹ ÐºÐ¾Ð¼Ð¿ÑÐµÑÑÐ¾Ñ
Ð¸ÑÑÐ»ÐµÐ´Ð¾Ð²Ð°Ð½Ð¸Ðµ
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Ð¼Ð¾Ð´ÐµÐ»ÑÐ½Ð°Ñ ÑÑÑÐ¿ÐµÐ½Ñ
Ð´ÑÐ¼Ð¼Ð¸Ñ
Ð½Ð°Ð³Ð½ÐµÑÐ°ÑÐµÐ»Ñ
Ð¿Ð°ÑÑÑÐ±ÐºÐ¸
Ð¾ÑÐµÐ²Ð¾Ðµ ÑÑÐ¸Ð»Ð¸Ðµ
axial compressor
research
natural gas
model stage
dummies
supercharger
nozzles
axial force

description: Ð Ð´Ð¸Ð¿Ð»Ð¾Ð¼Ð½Ð¾Ð¼ Ð¿ÑÐ¾ÐµÐºÑÐµ Ð±ÑÐ»Ð¸ Ð¿ÑÐ¾Ð²ÐµÐ´ÐµÐ½Ñ ÑÐ°ÑÑÐµÑÑ Ð¸ Ð¿ÑÐ¾ÐµÐºÑÐ¸ÑÐ¾Ð²Ð°Ð½Ð¸Ðµ Ð¿ÑÐ¾ÑÐ¾ÑÐ½Ð¾Ð¹ ÑÐ°ÑÑÐ¸ Ð¾ÑÐµÐ²Ð¾Ð³Ð¾ ÐºÐ¾Ð¼Ð¿ÑÐµÑÑÐ¾ÑÐ°, Ð¿ÑÐµÐ´Ð½Ð°Ð·Ð½Ð°ÑÐµÐ½Ð½Ð¾Ð³Ð¾ Ð´Ð»Ñ Ð·Ð°Ð¼ÐµÐ½Ñ Ð¿ÑÐ¾ÑÐ¾ÑÐ½Ð¾Ð¹ ÑÐ°ÑÑÐ¸ Ð¸ÑÑÐ¾Ð´Ð½Ð¾Ð³Ð¾ ÑÐµÐ½ÑÑÐ¾Ð±ÐµÐ¶Ð½Ð¾Ð³Ð¾ ÐºÐ¾Ð¼Ð¿ÑÐµÑÑÐ¾ÑÐ° Ð³Ð°Ð·Ð¾Ð¿ÐµÑÐµÐºÐ°ÑÐ¸Ð²Ð°ÑÑÐµÐ³Ð¾ Ð°Ð³ÑÐµÐ³Ð°ÑÐ° Ð¼Ð¾ÑÐ½Ð¾ÑÑÑÑ 16 ÐÐÑ Ð´Ð»Ñ Ð»Ð¸Ð½ÐµÐ¹Ð½Ð¾Ð¹ ÐºÐ¾Ð¼Ð¿ÑÐµÑÑÐ¾ÑÐ½Ð¾Ð¹ ÑÑÐ°Ð½ÑÐ¸Ð¸. Ð Ð´Ð¸ÑÑÐµÑÑÐ°ÑÐ¸Ð¸ Ð±ÑÐ»Ð¸ Ð²ÑÐ¿Ð¾Ð»Ð½ÐµÐ½Ñ Ð³Ð°Ð·Ð¾Ð´Ð¸Ð½Ð°Ð¼Ð¸ÑÐµÑÐºÐ¸Ðµ ÑÐ°ÑÑÐµÑÑ Ð¿ÑÐ¾ÑÐ¾ÑÐ½Ð¾Ð¹ ÑÐ°ÑÑÐ¸ Ð¾ÑÐµÐ²Ð¾Ð³Ð¾ ÐºÐ¾Ð¼Ð¿ÑÐµÑÑÐ¾ÑÐ°, Ð¿ÑÐ¸ Ð´Ð²ÑÑ Ð·Ð½Ð°ÑÐµÐ½Ð¸ÑÑ ÑÐ¸ÑÐµÐ» Ð¾Ð±Ð¾ÑÐ¾ÑÐ¾Ð² ÑÐ¾ÑÐ¾ÑÐ° n = 9000 Ð¾Ð±/Ð¼Ð¸Ð½. Ð¸ n = 10000 Ð¾Ð±/Ð¼Ð¸Ð½., Ð° ÑÐ°ÐºÐ¶Ðµ ÑÐ°ÑÑÐµÑÑ Ð¾ÑÐµÐ²Ð¾Ð³Ð¾ ÑÑÐ¸Ð»Ð¸Ñ, Ð´ÐµÐ¹ÑÑÐ²ÑÑÑÐµÐ³Ð¾ Ð½Ð° ÑÐ¾ÑÐ¾Ñ Ð¾ÑÐµÐ²Ð¾Ð³Ð¾ ÐºÐ¾Ð¼Ð¿ÑÐµÑÑÐ¾ÑÐ°, Ð¸ Ð²Ð½ÐµÑÐ½Ð¸Ñ ÑÑÐµÑÐµÐº ÑÐµÑÐµÐ· Ð»Ð°Ð±Ð¸ÑÐ¸Ð½ÑÐ½ÑÐµ ÑÐ¿Ð»Ð¾ÑÐ½ÐµÐ½Ð¸Ñ Ð´ÑÐ¼Ð¼Ð¸ÑÐ°. ÐÑÐ¸ Ð·Ð°Ð¼ÐµÐ½Ðµ Ð¿ÑÐ¾ÑÐ¾ÑÐ½Ð¾Ð¹ ÑÐ°ÑÑÐ¸ Ñ ÑÐµÐ½ÑÑÐ¾Ð±ÐµÐ¶Ð½ÑÐ¼Ð¸ ÑÐ°Ð±Ð¾ÑÐ¸Ð¼Ð¸ ÑÑÑÐ¿ÐµÐ½ÑÐ¼Ð¸ Ð½Ð° Ð¿ÑÐ¾ÑÐ¾ÑÐ½ÑÑ ÑÐ°ÑÑÑ Ñ Ð¾ÑÐµÐ²ÑÐ¼Ð¸ ÑÐ°Ð±Ð¾ÑÐ¸Ð¼Ð¸ ÑÑÑÐ¿ÐµÐ½ÑÐ¼Ð¸ Ð³Ð°Ð±Ð°ÑÐ¸ÑÑ ÑÐ¿Ð¾ÑÐ½Ð¾Ð³Ð¾ Ð¿Ð¾Ð´ÑÐ¸Ð¿Ð½Ð¸ÐºÐ°, Ð¾Ð¿Ð¾ÑÐ½ÑÑ Ð¼Ð°Ð³Ð½Ð¸ÑÐ½ÑÑ Ð¿Ð¾Ð´ÑÐ¸Ð¿Ð½Ð¸ÐºÐ¾Ð² Ð¸ ÐºÐ¾Ð½ÑÐµÐ²ÑÑ ÑÑÑÐ¸Ñ Ð³Ð°Ð·Ð¾Ð´Ð¸Ð½Ð°Ð¼Ð¸ÑÐµÑÐºÐ¸Ñ ÑÐ¿Ð»Ð¾ÑÐ½ÐµÐ½Ð¸Ð¹ ÑÐ¾ÑÑÐ°Ð½ÑÑÑÑÑ.
description: In the diploma project, calculations and design of the flow part of the axial compressor designed to replace the flow part of the initial centrifugal compressor of the gas compressor unit with a capacity of 16 MW for the linear compressor station were carried out. In the dissertation, gas-dynamic calculations of the flow part of the axial compressor were performed, at two values of the rotor speed n = 9000 rpm and n = 10000 rpm, as well as calculations of the axial force acting on the rotor of the axial compressor and external leaks through the labyrinth seals of dummies. When replacing the flow part with centrifugal operating stages with the flow part with axial operating stages, the dimensions of the thrust bearing, magnetic support bearings and dry gas-dynamic end seals are preserved.