Modelling the characteristics of axial compressor of variable flow passage geometry, working in the gas turbine engine system

被引:5
|
作者
Wirkowski, Pawel [1 ]
机构
[1] Polish Naval Univ, Mech Elect Fac, PL-81103 Gdynia, Poland
关键词
marine gas turbine engine; compressor; modelling of characteristics;
D O I
10.2478/v10012-007-0015-z
中图分类号
U6 [水路运输]; P75 [海洋工程];
学科分类号
0814 ; 081505 ; 0824 ; 082401 ;
摘要
This paper concerns application of mathematical modelling methods to analyzing gas-dynamic processes in marine gas turbines. Influence of geometry changes in axial compressor flow passage on kinematical airflow characteristics, are presented. The elaborated mathematical model will make it possible to realize - in the future - simulative investigations of gas-dynamic processes taking place in a compressor fitted with controllable guide vanes.
引用
收藏
页码:27 / 32
页数:6
相关论文
共 50 条
  • [31] TIP LEAKAGE FLOW AND HEAT TRANSFER CHARACTERISTICS ON ROTOR CASING AND BLADE TIP IN AN AXIAL GAS TURBINE ENGINE: STEADY ANALYSIS
    Rahman, Md Hamidur
    Kim, Sung In
    Hassan, Ibrahim
    [J]. HT2008: PROCEEDINGS OF THE ASME SUMMER HEAT TRANSFER CONFERENCE - 2008, VOL 2, 2009, : 635 - 644
  • [32] Gas turbine gas-path fault diagnosis in power plant under transient operating condition with variable geometry compressor
    Li, Jingchao
    Ying, Yulong
    Wu, Zhong
    [J]. ENERGY SCIENCE & ENGINEERING, 2022, 10 (09) : 3423 - 3442
  • [33] A Study on Flow Instability in an Axial Compressor of Gas Turbine for Power Generation at Partial-Load Conditions
    Yokoji, Katsuhiro
    Nakayama, Kentaro
    Miura, Toshimasa
    [J]. International Journal of Gas Turbine, Propulsion and Power Systems, 2024, 15 (04): : 25 - 32
  • [34] CALCULATION OF AXIAL DRIVE CENTRIFUGAL BREATHERS OF GAS-TURBINE ENGINE OIL SYSTEM
    PETROV, PG
    POVAROV, OA
    [J]. IZVESTIYA VYSSHIKH UCHEBNYKH ZAVEDENII AVIATSIONAYA TEKHNIKA, 1979, (03): : 108 - 110
  • [35] Off-design performance improvement of twin-shaft gas turbine by variable geometry turbine and compressor besides fuel control
    Sanaye, Sepehr
    Hosseini, Salahadin
    [J]. PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART A-JOURNAL OF POWER AND ENERGY, 2020, 234 (07) : 957 - 980
  • [36] Development of a Throughflow-Based Simulation Tool for Preliminary Compressor Design Considering Blade Geometry in Gas Turbine Engine
    Liu, Xiaoheng
    Wan, Ke
    Jin, Donghai
    Gui, Xingmin
    [J]. APPLIED SCIENCES-BASEL, 2021, 11 (01): : 1 - 22
  • [37] Joint prediction of aircraft gas turbine engine axial flow compressor off-design performance and surge line based on the expanded method of generalized functions
    Mikhailova A.B.
    Akhmedzyanov D.A.
    Akhmetov Y.M.
    Mikhailov A.E.
    [J]. Russian Aeronautics, 2014, 57 (03): : 291 - 296
  • [38] Analysis of Performance Characteristics under Variable Inlet Conditions of Gas Turbine Compressor based on Physical Model
    Park, Gyu Sang
    Bang, Myeong Hwan
    Gwak, You Ra
    Kang, Hae Su
    Chang, Sung Ho
    Choi, Woo Sung
    [J]. TRANSACTIONS OF THE KOREAN SOCIETY OF MECHANICAL ENGINEERS A, 2021, 45 (01) : 67 - 74
  • [39] Numerical investigations of performance optimization using variable guide vanes in a multistage compressor of a 6 MW gas turbine engine
    White, NM
    Tourlidakis, A
    Elder, RL
    [J]. PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART A-JOURNAL OF POWER AND ENERGY, 2003, 217 (A6) : 593 - 603
  • [40] NUMERICAL INVESTIGATION ON AERODYNAMIC CHARACTERISTICS OF VARIABLE GEOMETRY TURBINE VANE CASCADE FOR MARINE GAS TURBINES
    Gao, Jie
    Huo, Dongchen
    [J]. PROCEEDINGS OF THE ASME TURBO EXPO: TURBOMACHINERY TECHNICAL CONFERENCE AND EXPOSITION, VOL 8, 2020,