title: ÐÑÑ Ð¾Ð´Ð½Ð¾Ð¹ ÑÑÐ°ÐºÑ Ð´Ð²ÑÑ Ð²Ð°Ð»ÑÐ½Ð¾Ð¹ Ð³Ð°Ð·Ð¾ÑÑÑÐ±Ð¸Ð½Ð½Ð¾Ð¹ ÑÑÑÐ°Ð½Ð¾Ð²ÐºÐ¸, Ð¿ÑÐµÐ´Ð½Ð°Ð·Ð½Ð°ÑÐµÐ½Ð½Ð¾Ð¹ Ð´Ð»Ñ ÑÐ°Ð±Ð¾ÑÑ Ð² ÑÐ¾ÑÑÐ°Ð²Ðµ Ð³Ð°Ð·Ð¾Ð¿Ð°ÑÐ¾Ð²Ð¾Ð¹ ÑÑÑÐ°Ð½Ð¾Ð²ÐºÐ¸
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: The output path of a two-shaft gas turbine unit designed to operate as part of a gas-steam unit
Creators: name: Ð¯Ð½ Ð§ÑÐ½ÑÑ Ð°Ð¾
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: 2023
Subjects: ÐºÐ»ÑÑÐµÐ²ÑÐµ ÑÐ»Ð¾Ð²Ð°: Ð³Ð°Ð·Ð¾Ð²Ð°Ñ ÑÑÑÐ±Ð¸Ð½Ð°
Ð³Ð°Ð·Ð¾Ð¿ÐµÑÐºÐ°ÑÐ¸Ð²Ð°ÑÑÐ°Ñ ÑÑÐ°Ð½ÑÐ¸Ñ
Ð´Ð¸ÑÑÑÐ·Ð¾Ñ
Ð²ÑÑ Ð¾Ð´Ð½Ð¾Ð¹ ÑÑÐ°ÐºÑ
Ð¿Ð¾ÑÐµÑÐ¸ Ð¿Ð¾Ð»Ð½Ð¾Ð³Ð¾ Ð´Ð°Ð²Ð»ÐµÐ½Ð¸Ñ
ÑÐ¸ÑÐ»ÐµÐ½Ð½Ð¾Ðµ Ð¼Ð¾Ð´ÐµÐ»Ð¸ÑÐ¾Ð²Ð°Ð½Ð¸Ðµ
key words: gas turbine
power turbine
exhaust arrangement
diffuser
exhaust duct
combined cycle

description: Ð¢ÐµÐ¼Ð° Ð²ÑÐ¿ÑÑÐºÐ½Ð¾Ð¹ ÐºÐ²Ð°Ð»Ð¸ÑÐ¸ÐºÐ°ÑÐ¸Ð¾Ð½Ð½Ð¾Ð¹ ÑÐ°Ð±Ð¾ÑÑ: Â«ÐÑÑÐ¾Ð´Ð½Ð¾Ð¹ ÑÑÐ°ÐºÑ Ð´Ð²ÑÑÐ²Ð°Ð»ÑÐ½Ð¾Ð¹ ÐÐ¢Ð£, Ð¿ÑÐµÐ´Ð½Ð°Ð·Ð½Ð°ÑÐµÐ½Ð½Ð¾Ð¹ Ð´Ð»Ñ ÑÐ°Ð±Ð¾ÑÑ ÑÐ¾ÑÑÐ°Ð²Ðµ ÐÐÐ£Â». Ð¦ÐµÐ»ÑÑ ÑÐ°Ð±Ð¾ÑÑ ÑÐ²Ð»ÑÐµÑÑÑ ÑÐ¸ÑÐ»ÐµÐ½Ð½Ð¾Ðµ Ð¼Ð¾Ð´ÐµÐ»Ð¸ÑÐ¾Ð²Ð°Ð½Ð¸Ðµ Ð²ÑÑÐ¾Ð´Ð½Ð¾Ð³Ð¾ ÑÑÐ°ÐºÑÐ° ÐÐ¢Ð£ Ð´Ð»Ñ Ð¾Ð¿ÑÐ¸Ð¼Ð¸Ð·Ð°ÑÐ¸Ð¸ Ð¿ÑÐ¾ÑÐ¾ÑÐ½Ð¾Ð¹ ÑÐ°ÑÑÐ¸. Ð Ð°ÑÑÐ¼Ð¾ÑÑÐµÐ½Ñ ÐºÐ¾Ð½ÑÑÑÑÐºÑÐ¸Ð¸ Ð³Ð°Ð·Ð¾ÑÑÑÐ±Ð¸Ð½Ð½ÑÑ ÑÑÑÐ°Ð½Ð¾Ð²Ð¾Ðº, Ð¸ÑÐ¿Ð¾Ð»ÑÐ·ÑÐµÐ¼ÑÑ Ð´Ð»Ñ Ð¿ÑÐ¸Ð²Ð¾Ð´Ð° Ð½Ð°Ð³Ð½ÐµÑÐ°ÑÐµÐ»Ñ Ð¿ÑÐ¸ÑÐ¾Ð´Ð½Ð¾Ð³Ð¾ Ð³Ð°Ð·Ð°, ÑÐºÑÐ¿Ð»ÑÐ°ÑÐ¸ÑÑÑÑÐ¸ÑÑÑ Ð½Ð° ÑÐµÑÑÐ¸ÑÐ¾ÑÐ¸Ð¸ Ð Ð¤. ÐÑÐ¸Ð²ÐµÐ´ÐµÐ½Ñ Ð¼ÐµÑÐ¾Ð´Ñ ÑÐ¸ÑÐ»ÐµÐ½Ð½Ð¾Ð³Ð¾ Ð¼Ð¾Ð´ÐµÐ»Ð¸ÑÐ¾Ð²Ð°Ð½Ð¸Ñ, ÑÐ°ÑÑÐ¼Ð¾ÑÑÐµÐ½Ñ ÑÐµÐ·ÑÐ»ÑÑÐ°ÑÑ Ð¿Ð¾Ð»ÑÑÐµÐ½Ð½ÑÐµ, Ð¿ÑÐ¸ ÑÐºÑÐ¿ÐµÑÐ¸Ð¼ÐµÐ½ÑÐ°Ð»ÑÐ½Ð¾Ð¼ Ð¼Ð¾Ð´ÐµÐ»Ð¸ÑÐ¾Ð²Ð°Ð½Ð¸Ð¸ Ð²ÑÑÐ¾Ð´Ð½Ð¾Ð³Ð¾ ÑÑÐ°ÐºÑÐ° Â«ÐÐ¸ÑÑÑÐ·Ð¾Ñ â ÐÐ°ÑÑÑÐ±Ð¾ÐºÂ». ÐÑÐ¾Ð²ÐµÐ´ÐµÐ½Ð¾ ÑÐ¸ÑÐ»ÐµÐ½Ð½Ð¾Ðµ Ð¼Ð¾Ð´ÐµÐ»Ð¸ÑÐ¾Ð²Ð°Ð½Ð¸Ðµ ÑÑÐµÑ Ð²Ð°ÑÐ¸Ð°Ð½ÑÐ¾Ð² ÑÐ°ÑÑÐµÑÐ½Ð¾Ð¹ Ð¼Ð¾Ð´ÐµÐ»Ð¸ Ð²ÑÑÐ¾Ð´Ð½Ð¾Ð³Ð¾ ÑÑÐ°ÐºÑÐ° Ð³Ð°Ð·Ð¾Ð²Ð¾Ð¹ ÑÑÑÐ±Ð¸Ð½Ñ. ÐÑÐ¾Ð²ÐµÐ´ÐµÐ½ Ð°Ð½Ð°Ð»Ð¸Ð· Ð¿Ð¾Ð»ÑÑÐµÐ½Ð½ÑÑ ÑÐµÐ·ÑÐ»ÑÑÐ°ÑÐ¾Ð² ÑÐ¸ÑÐ»ÐµÐ½Ð½Ð¾Ð³Ð¾ ÑÐºÑÐ¿ÐµÑÐ¸Ð¼ÐµÐ½ÑÐ°, Ð¿ÑÐµÐ´Ð»Ð¾Ð¶ÐµÐ½Ñ Ð²Ð°ÑÐ¸Ð°Ð½ÑÑ ÑÐ»ÑÑÑÐµÐ½Ð¸Ñ ÐºÐ¾Ð½ÑÑÑÑÐºÑÐ¸Ð¸ Ð²ÑÑÐ¾Ð´Ð½Ð¾Ð³Ð¾ ÑÑÐ°ÐºÑÐ° Ñ ÑÐµÐ»ÑÑ ÑÐ»ÑÑÑÐµÐ½Ð¸Ñ ÐµÐ³Ð¾ Ð°ÑÑÐ¾Ð´Ð¸Ð½Ð°Ð¼Ð¸ÑÐµÑÐºÐ¸Ñ ÐºÐ°ÑÐµÑÑÐ².
description: The topic of the final qualifying work: " Exhaust duct of two-shaft gas turbine designed for working in combined cycle power plant ". The aim of the work is numerical simulation of the output path of the gas turbine engine to optimize the flow part. The designs of gas turbine installations used to drive a natural gas supercharger operating in the territory of the Russian Federation are considered. Numerical modeling methods are presented, the results obtained during experimental modeling of the output path "Diffuser â Pipe" are considered. Numerical modeling of three variants of the computational model of the gas turbine output path is carried out. The analysis of the obtained results of the numerical experiment is carried out, options for improving the design of the output path in order to improve its aerodynamic qualities are proposed.