title: ÐÑÐ¾ÐµÐºÑÐ¸ÑÐ¾Ð²Ð°Ð½Ð¸Ðµ Ð¾ÑÐµÐ²Ð¾Ð³Ð¾ ÐºÐ¾Ð¼Ð¿ÑÐµÑÑÐ¾ÑÐ° ÐÐ¢Ð­ 65
title: Ð²ÑÐ¿ÑÑÐºÐ½Ð°Ñ ÐºÐ²Ð°Ð»Ð¸ÑÐ¸ÐºÐ°ÑÐ¸Ð¾Ð½Ð½Ð°Ñ ÑÐ°Ð±Ð¾ÑÐ° Ð±Ð°ÐºÐ°Ð»Ð°Ð²ÑÐ°
titleType: Subtitle
title: Design of axial compressor GTE-65
Creators: name: Ð¥Ð°ÑÑÑÐ¸Ð½, ÐÐ²Ð°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: 2022
Subjects: ÐÐ¢Ð­
Ð¾ÑÐµÐ²ÑÐµ ÐºÐ¾Ð¼Ð¿ÑÐµÑÑÐ¾ÑÑ
Ð¦ÐÐÐ
Ð¦ÐÐ¢Ð
GTE
axial compressors
CIAM
CKTI

description: Ð Ð´Ð°Ð½Ð½Ð¾Ð¹ ÑÐ°Ð±Ð¾ÑÐµ Ð¾Ð¿Ð¸ÑÐ°Ð½Ð° Ð¼ÐµÑÐ¾Ð´Ð¸ÐºÐ° Ð¿ÑÐ¾ÐµÐºÑÐ¸ÑÐ¾Ð²Ð°Ð½Ð¸Ñ Ð¾ÑÐµÐ²Ð¾Ð³Ð¾ ÐºÐ¾Ð¼Ð¿ÑÐµÑÑÐ¾ÑÐ° Ð³Ð°Ð·Ð¾ÑÑÑÐ±Ð¸Ð½Ð½Ð¾Ð¹ ÑÑÑÐ°Ð½Ð¾Ð²ÐºÐ¸ ÐÐ¢Ð­â65 ÐºÐ°Ðº Ð¿Ð¾ Ð¼ÐµÑÐ¾Ð´Ð¸ÐºÐ°Ð¼ Ð¦ÐÐÐâÐ¦ÐÐ¢Ð, ÑÐ°Ðº Ð¸ Ñ Ð¸ÑÐ¿Ð¾Ð»ÑÐ·Ð¾Ð²Ð°Ð½Ð¸ÐµÐ¼ Ð¿ÑÐ¾Ð³ÑÐ°Ð¼Ð¼Ñ Concepts NREC AXIAL.ÐÑÐ»Ð¸ Ð¾Ð¿ÑÐµÐ´ÐµÐ»ÐµÐ½Ñ Ð¾ÑÐ½Ð¾Ð²Ð½ÑÐµ ÑÐ°ÑÐ°ÐºÑÐµÑÐ¸ÑÑÐ¸ÐºÐ¸ Ð¾ÑÐµÐ²Ð¾Ð³Ð¾ ÐºÐ¾Ð¼Ð¿ÑÐµÑÑÐ¾ÑÐ°, Ð° ÑÐ°ÐºÐ¶Ðµ Ð¿Ð°ÑÐ°Ð¼ÐµÑÑÑ ÑÐ°Ð±Ð¾ÑÐµÐ³Ð¾ Ð¿ÑÐ¾ÑÐµÑÑÐ° ÑÐµÑÐµÐ½Ð¸ÑÑ Ð¿ÑÐ¾ÑÐ¾ÑÐ½Ð¾Ð¹ ÑÐ°ÑÑÐ¸ Ð¾ÑÐµÐ²Ð¾Ð³Ð¾ ÐºÐ¾Ð¼Ð¿ÑÐµÑÑÐ¾ÑÐ°, ÑÐ°ÑÑÐ¼Ð¾ÑÑÐµÐ½ Ð¾Ð´Ð½Ð¾Ð¼ÐµÑÐ½ÑÐ¹ Ð¸ Ð²ÑÐ·ÐºÐ¸Ð¹ ÐºÐ²Ð°Ð·Ð¸ÑÑÑÑÐ¼ÐµÑÐ½ÑÐ¹ ÑÐ°ÑÑÑÑ ÑÑÑÐ°Ð½Ð¾Ð²ÐºÐ¸. ÐÑÐ¿Ð¾Ð»Ð½ÐµÐ½ ÑÐ°ÑÑÑÑ Ð¸ Ð¿ÑÐ¾ÐµÐºÑÐ¸ÑÐ¾Ð²Ð°Ð½Ð¸Ðµ Ð¾ÑÐµÐ²Ð¾Ð³Ð¾ ÐºÐ¾Ð¼Ð¿ÑÐµÑÑÐ¾ÑÐ° Ð½Ð° Ð¾ÑÐ½Ð¾Ð²Ðµ Ð¸Ð¼ÐµÑÑÐ¸ÑÑÑ Ð´Ð°Ð½Ð½ÑÑ ÑÑÑÐµÑÑÐ²ÑÑÑÐµÐ³Ð¾ Ð¿ÑÐ¾ÑÐ¾ÑÐ¸Ð¿Ð°.Â ÐÑÐ¾Ð²ÐµÐ´ÑÐ½ ÑÐ°ÑÑÑÑ Ð¿ÐµÑÐ²Ð¾Ð³Ð¾ ÐºÐ°ÑÐºÐ°Ð´Ð° Ð¿Ð¾ Ð¼ÐµÑÐ¾Ð´Ð¸ÐºÐµ Ð¦ÐÐÐ, ÑÐ°ÑÑÑÑ Ð²ÑÐ¾ÑÐ¾Ð³Ð¾ ÐºÐ°ÑÐºÐ°Ð´Ð° Ð¿Ð¾ Ð¼ÐµÑÐ¾Ð´Ð¸ÐºÐµ Ð¦ÐÐ¢Ð Ñ Ð¾Ð±Ð¾ÑÐ½Ð¾Ð²Ð°Ð½Ð¸ÐµÐ¼ Ð¿ÐµÑÐµÑÐ¾Ð´Ð° Ð² Ð¿ÑÐ¾Ð³ÑÐ°Ð¼Ð¼Ñ Concepts NREC AXIAL, ÑÐ°ÑÑÑÑ Ð² Ð¿ÑÐ¾Ð³ÑÐ°Ð¼Ð¼Ðµ Concepts NREC AXIAL Ñ Ð¸ÑÐ¿Ð¾Ð»ÑÐ·Ð¾Ð²Ð°Ð½Ð¸ÐµÐ¼ Ð·Ð°ÑÑÐ±ÐµÐ¶Ð½ÑÑ Ð¼Ð¾Ð´ÐµÐ»ÑÐ½ÑÑ Ð¿ÑÐ¾ÑÐ¸Ð»ÐµÐ¹, Ð¿Ð¾Ð»ÑÑÐµÐ½Ñ Ð¸ ÑÑÐ°Ð²Ð½ÐµÐ½Ñ Ð³Ð°Ð·Ð¾Ð´Ð¸Ð½Ð°Ð¼Ð¸ÑÐµÑÐºÐ¸Ðµ Ð¸ Ð³ÐµÐ¾Ð¼ÐµÑÑÐ¸ÑÐµÑÐºÐ¸Ðµ Ð¿Ð°ÑÐ°Ð¼ÐµÑÑÑ Ð´Ð»Ñ Ð¾Ð±Ð¾Ð¸Ñ Ð¼ÐµÑÐ¾Ð´Ð¾Ð² Ð¿ÑÐ¾ÐµÐºÑÐ¸ÑÐ¾Ð²Ð°Ð½Ð¸Ñ.Â ÐÑÐ» Ð¿ÑÐ¾Ð²ÐµÐ´ÑÐ½ Ð³Ð°Ð·Ð¾Ð´Ð¸Ð½Ð°Ð¼Ð¸ÑÐµÑÐºÐ¸Ð¹ ÑÐ°ÑÑÑÑ Ð¿ÑÐ¾ÑÐ¾ÑÐ½Ð¾Ð¹ ÑÐ°ÑÑÐ¸ Ð² Ð¿ÑÐ¾Ð³ÑÐ°Ð¼Ð¼Ðµ ANSYS CFX, Ð½Ð° Ð¾ÑÐ½Ð¾Ð²Ð°Ð½Ð¸Ð¸ ÐºÐ¾ÑÐ¾ÑÐ¾Ð³Ð¾ ÑÐ´ÐµÐ»Ð°Ð½Ñ Ð²ÑÐ²Ð¾Ð´Ñ Ð¾ ÑÐ¾ÑÐ½Ð¾ÑÑÐ¸ Ð¿ÑÐ¸Ð¼ÐµÐ½Ð¸Ð¼Ð¾ÑÑÐ¸ Ð¿Ð¾Ð´Ð¾Ð±Ð½ÑÑ Ð¼ÐµÑÐ¾Ð´Ð¾Ð² Ð¿ÑÐ¾ÐµÐºÑÐ¸ÑÐ¾Ð²Ð°Ð½Ð¸Ñ Ð´Ð»Ñ Ð´Ð°Ð½Ð½ÑÑ ÑÑÑÐ°Ð½Ð¾Ð²Ð¾Ðº Ð¸ ÐºÐ¾Ð¼Ð¿ÑÐµÑÑÐ¾ÑÐ¾Ð² Ð² ÑÐµÐ»Ð¾Ð¼.
description: This paper describes the methodology for designing an axial compressor for a GTEâ65 gas turbine plant, both according to the CIAMâCKTI methods and using the Concepts NREC AXIAL program.Â The main characteristics of the axial compressor were determined, as well as the parameters of the working process in the cross sections of the flow path of the axial compressor, oneâdimensional and viscous quasiâthreeâdimensional calculation of the installation was considered. The calculation and design of an axial compressor based on the available data of the existing prototype has been carried out.Â The calculation of the first cascade was carried out according to the CIAM method, the calculation of the second cascade was carried out according to the CKTI method with the rationale for switching to the Concepts NREC AXIAL program, the calculation in the Concepts NREC AXIAL program using foreign model profiles, the gasâdynamic and geometric parameters for both design methods were obtained and compared. A gasâdynamic calculation of the flow path was carried out in the ANSYS CFX program, on the basis of which conclusions were drawn about the accuracy of the applicability of such design methods for these units and compressors as a whole.