title: ÐÐ¿ÑÐ¸Ð¼Ð¸Ð·Ð°ÑÐ¸Ñ Ð¿Ð°ÑÐ°Ð¼ÐµÑÑÐ¾Ð² Ð²ÑÑ Ð¾Ð´Ð½Ð¾Ð³Ð¾ ÑÑÐ°ÐºÑÐ° 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 Ð½Ð° Ð³Ð°Ð·Ð¾Ð¿ÐµÑÐµÐºÐ°ÑÐ¸Ð²Ð°ÑÑÐµÐ¹ ÑÑÐ°Ð½ÑÐ¸Ð¸
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: Optimization of the parameters of the output track of a two-shaft GTU designed for GPS
Creators: name: ÐÐ°ÑÑÐºÐ¾Ð², ÐÐ¸ÑÐ¸Ð»Ð»
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: Ð²ÑÑ Ð¾Ð´Ð½Ð¾Ð¹ Ð´Ð¸ÑÑÑÐ·Ð¾Ñ
ÑÐ¸ÑÐ»ÐµÐ½Ð½Ð¾Ðµ Ð¼Ð¾Ð´ÐµÐ»Ð¸ÑÐ¾Ð²Ð°Ð½Ð¸Ñ
Ð´Ð²ÑÑ Ð²Ð°Ð»ÑÐ½Ð°Ñ Ð³ÑÑ
ÐºÐ¿Ð´
Ð¾Ð¿ÑÐ¸Ð¼Ð¸Ð·Ð°ÑÐ¸Ñ
ansys cfx
output diffuser
numerical simulation
two-shaft gtu
efficiency
optimization

description: ÐÐ°Ð½Ð½Ð°Ñ ÑÐ°Ð±Ð¾ÑÐ° Ð¿Ð¾ÑÐ²ÑÑÐµÐ½Ð° Ð¸ÑÑÐ»ÐµÐ´Ð¾Ð²Ð°Ð½Ð¸Ñ Ð²Ð»Ð¸ÑÐ½Ð¸Ñ Ð³ÐµÐ¾Ð¼ÐµÑÑÐ¸Ð¸ Ð²ÑÑÐ¾Ð´Ð½Ð¾Ð³Ð¾ Ð´Ð¸ÑÑÑÐ·Ð¾ÑÐ° Ð½Ð° ÐºÐ¾ÑÑÑÐ¸ÑÐ¸ÐµÐ½Ñ Ð²Ð¾ÑÑÑÐ°Ð½Ð¾Ð²Ð»ÐµÐ½Ð¸Ñ Ð´Ð°Ð²Ð»ÐµÐ½Ð¸Ñ. ÐÐ°Ð´Ð°ÑÐ¸ ÐºÐ¾ÑÐ¾ÑÑÐµ ÑÐµÑÐ°Ð»Ð¸ÑÑ Ð² ÑÐ¾Ð´Ðµ Ð¸ÑÑÐ»ÐµÐ´Ð¾Ð²Ð°Ð½Ð¸Ñ: 1) ÐÐ¾ÑÑÑÐ¾ÐµÐ½Ð¸Ðµ Ð¼Ð¾Ð´ÐµÐ»ÐµÐ¹ Ð´Ð¸ÑÑÑÐ·Ð¾ÑÐ° Ñ ÑÐ°Ð·Ð»Ð¸ÑÐ½ÑÐ¼Ð¸ ÑÐ³Ð»Ð°Ð¼Ð¸ ÑÐ°ÑÐºÑÑÑÐ¸Ñ. 2) ÑÐ°ÑÑÐµÑ ÑÑÐ¸Ñ Ð¼Ð¾Ð´ÐµÐ»ÐµÐ¹ Ð² Ð¿ÑÐ¾Ð³ÑÐ°Ð¼Ð¼Ðµ Ansys. 3) Ð°Ð½Ð°Ð»Ð¸Ð· ÑÐµÐ·ÑÐ»ÑÑÐ°ÑÐ¾Ð². ÐÑÐ¾Ð²ÐµÐ´ÐµÐ½Ð¾ ÑÐ¸ÑÐ»ÐµÐ½Ð½Ð¾Ðµ Ð¼Ð¾Ð´ÐµÐ»Ð¸ÑÐ¾Ð²Ð°Ð½Ð¸Ðµ ÑÐµÑÑÑÑÑ 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·Ð¾ÑÑÑÐ±Ð¸Ð½Ð½Ð¾Ð¹ ÑÑÑÐ°Ð½Ð¾Ð²ÐºÐ¸: Ð±Ð°Ð·Ð¾Ð²Ð¾Ð³Ð¾ Ð²Ð°ÑÐ¸Ð°Ð½ÑÐ° Ð²ÑÑÐ¾Ð´Ð½Ð¾Ð³Ð¾ ÑÑÐ°ÐºÑÐ°, Ð²Ð°ÑÐ¸Ð°Ð½ÑÐ° ÐÐ¢ Ñ Ð´Ð¸ÑÑÑÐ·Ð¾ÑÐ¾Ð¼, Ð¸Ð¼ÐµÑÑÐ¸Ð¼ ÑÐ³Ð¾Ð» ÑÐ°ÑÐºÑÑÑÐ¸Ñ 7, Ð²Ð°ÑÐ¸Ð°Ð½ÑÐ° Ñ Ð´Ð¸ÑÑÑÐ·Ð¾ÑÐ¾Ð¼ Ð¸Ð¼ÐµÑÑÐ¸Ð¹ ÑÐ³Ð¾Ð» ÑÐ°ÑÐºÑÑÑÐ¸Ñ 14 Ð¸ Ð²Ð°ÑÐ¸Ð°Ð½Ñ Ñ ÑÐ³Ð»Ð¾Ð¼ ÑÐ°ÑÐºÑÑÑÐ¸Ñ 24. 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°, Ð²Ð°Ð»Ð¸Ð´Ð°ÑÐ¸Ñ Ð¸Ð½ÑÐµÐ³ÑÐ°Ð»ÑÐ½ÑÑ Ð°ÑÑÐ¾Ð´Ð¸Ð½Ð°Ð¼Ð¸ÑÐµÑÐºÐ¸Ñ Ð¿Ð°ÑÐ°Ð¼ÐµÑÑÐ¾Ð² Ð¿Ð¾ ÑÐµÐ·ÑÐ»ÑÑÐ°ÑÐ°Ð¼ ÑÐºÑÐ¿ÐµÑÐ¸Ð¼ÐµÐ½ÑÐ°Ð»ÑÐ½Ð¾Ð³Ð¾ Ð¸ÑÑÐ»ÐµÐ´Ð¾Ð²Ð°Ð½Ð¸Ñ Ð²ÑÑÐ¾Ð´Ð½Ð¾Ð³Ð¾ ÑÑÐ°ÐºÑÐ° Ð±Ð°Ð·Ð¾Ð²Ð¾Ð¹ ÐºÐ¾Ð½ÑÑÑÑÐºÑÐ¸Ð¸, Ð° ÑÐ°ÐºÐ¶Ðµ ÑÐ´ÐµÐ»Ð°Ð½ Ð²ÑÐ²Ð¾Ð´ Ð¾ ÑÐµÐ»ÐµÑÐ¾Ð¾Ð±ÑÐ°Ð·Ð½Ð¾ÑÑÐ¸ Ð´Ð°Ð»ÑÐ½ÐµÐ¹ÑÐµÐ³Ð¾ Ð¸ÑÑÐ»ÐµÐ´Ð¾Ð²Ð°Ð½Ð¸Ñ Ð½ÐµÑÑÐ°Ð½Ð´Ð°ÑÑÐ½Ð¾Ð³Ð¾ Ð²Ð°ÑÐ¸Ð°Ð½ÑÐ° ÐºÐ¾Ð½ÑÑÑÑÐºÑÐ¸Ð¸ Ð²ÑÑÐ¾Ð´Ð½Ð¾Ð³Ð¾ ÑÑÐ°ÐºÑÐ°.
description: This work is devoted to the study of the influence of the geometry of the output diffuser on the pressure recovery coefficient. Tasks that were solved during the study: 1) Construction of diffuser models with different opening angles. 2) calculation of these models in the ansys program. 3) analysis of the results. Numerical modeling of four variants of the design model of the output path of a gas turbine installation is carried out: the basic version of the output path, the variant with a diffuser having an opening angle of 7, the variant with a diffuser having an opening angle of 14 and the variant with an opening angle of 24. The analysis of the obtained results of the numerical experiment, validation of integral aerodynamic parameters based on the results of an experimental study of the output path of the basic design, and the conclusion is made about the feasibility of further research of a non-standard version of the output path design.