title: ÐÑÐ¾ÐµÐºÑÐ¸ÑÐ¾Ð²Ð°Ð½Ð¸Ðµ 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: Designing an axial compressor of natural gas based on the model stage K-100-2L
Creators: name: ÐÐ¾Ð¶ÐµÐºÐ¸Ð½, ÐÐ°Ð²ÐµÐ»
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
ÑÐµÐ½ÑÑÐ¾Ð±ÐµÐ¶Ð½ÑÐ¹ ÐºÐ¾Ð¼Ð¿ÑÐµÑÑÐ¾Ñ
Ð¿ÑÐ¸ÑÐ¾Ð´Ð½ÑÐ¹ Ð³Ð°Ð·
ÑÑÑÐ¿ÐµÐ½Ñ Ð-50
ÑÑÑÐ¿ÐµÐ½Ñ Ð-100
axial compressor
centrifugal compressor
natural gas
stage K-50
stage K-100

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° Ð´Ð»Ñ Ð¿ÑÐ¸Ð¼ÐµÐ½ÐµÐ½Ð¸Ñ Ð² Ð³Ð°Ð·Ð¾Ð¿ÐµÑÐµÐºÐ°ÑÐ¸Ð²Ð°ÑÑÐ¸Ñ Ð°Ð³ÑÐµÐ³Ð°ÑÐ°Ñ 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ÑÑÐ¿ÐµÐ½ÑÐ¼Ð¸ Ð³Ð°Ð±Ð°ÑÐ¸ÑÑ Ð¾Ð¿Ð¾ÑÐ½ÑÑ Ð¸ ÑÐ¿Ð¾ÑÐ½Ð¾Ð³Ð¾ 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 work the calculation and design engineering of a flow channel of an axial compressor are presented. The axial compressor is destined for renewal of a flow channel of an original radial-flow compressor of a gas-compressor plant with a capacity of 16 Mega Watts for a straight-line gas-compressor station. 
In the dissertation the gasdynamic solving of a flow channel of an axial compressor by two numbers of revolutions of rotary n = 9000 rounds per minute and n = 10000 rounds per minute is accomplished.
Moreover, the calculation of axial load which works upon a rotary of an axial compressor and the calculation of external leakage through labyrinth packing of balance cylinder are executed.
In the setting of substitution of a flow channel with centrifugal working stages for a flow channel with axial flow stages, the limiting dimensions of thrust bearing and axial magnetic bearing and the limiting dimensions of end dry gas closure remain unchanged.