ESTIMATION OF THE HYDRAULIC LOSSES IN THE WORK SHAFT OF A GAS TURBINE ENGINE OF A GAS COMPRESSOR UNIT UNDER VARIOUS OPERATING CONDITIONS

被引:0
|
作者
Baturin, Oleg [1 ]
Krivtsov, Aleksandr [1 ]
Kolmakova, Dania [1 ]
Popov, Grigorii [1 ]
机构
[1] Samara Natl Res Univ, Samara, Russia
关键词
D O I
暂无
中图分类号
TE [石油、天然气工业]; TK [能源与动力工程];
学科分类号
0807 ; 0820 ;
摘要
The paper presents the results of numerical simulation of air flow through a modernized variant of the inlet filter unit (IFU) of the gas compressor unit GPA-Ts-16. A feature of the IFU design is that to reduce the load on the filter unit, it is proposed to be as compact as possible, which determines its complex shape. The goal of the study is to study the hydraulic losses and to develop the measures to reduce them, since it is found that every 100 Pa of losses in the inlet unit increases the consumption of fuel gas by 2.5 kg/h or reduces the engine power by 10.5 kW. Calculations of hydraulic losses in IFU are carried out for cases of absence or presence of wind with a velocity from 0 to 35 m/s, blowing from 5 main directions (0, 45, 90, 135, 180). Studies are also carried out on the effect of the weather shield shape, presence of baffles under it, and the rack in the shaft on the hydraulic losses. As a result of the research, recommendations are provided for designing (changing the shape) of the inlet filter unit that eventually allow to propose a design that will reduce the hydraulic losses in IFU by 15% relative to the originally suggested variant.
引用
收藏
页数:11
相关论文
共 50 条
  • [21] Optimizing the performance of a single-shaft micro gas turbine engine by modifying its centrifugal compressor design
    Hosseinimaab, S. M.
    Tousi, A. M.
    [J]. ENERGY CONVERSION AND MANAGEMENT, 2022, 271
  • [22] OPTICAL PATTERNATION OF GAS TURBINE FUEL SPRAYS DURING SIMULATED ENGINE OPERATING CONDITIONS
    Guy, S. R. D.
    Allan, W. D. E.
    LaViolette, Marc
    Underhill, P. R.
    [J]. PROCEEDINGS OF THE ASME TURBO EXPO 2009, VOL 2, 2009, : 1 - 10
  • [23] Experimental analysis of oxygen-methane combustion inside a gas turbine reactor under various operating conditions
    Habib, Mohamed A.
    Nemitallah, Medhat A.
    Ahmed, Pervez
    Sharqawy, Mostafa H.
    Badr, Hassan M.
    Muhammad, Inam
    Yaqub, Mohamed
    [J]. ENERGY, 2015, 86 : 105 - 114
  • [24] Estimation of corrosion fatigue life by evaluation on corrosion pit damage in gas turbine compressor blades under service conditions
    Hitachi Works, Hitachi Ltd., Saiwai-Cho, Hitachi, 317-8511, Japan
    不详
    不详
    [J]. Zairyo, 2013, 6 (383-389):
  • [25] A universal fault classification for gas turbine diagnosis under variable operating conditions
    Loboda, Igor
    Feldshteyn, Yakov
    [J]. INTERNATIONAL JOURNAL OF TURBO & JET-ENGINES, 2007, 24 (01) : 11 - 27
  • [26] A STUDY OF THE INFLUENCE OF SERVICE OPERATING TIME AND A CORROSIVE MEDIUM ON THE LIFE OF GAS-TURBINE ENGINE COMPRESSOR BLADES
    TROSHCHENKO, VT
    PROKOPENKO, AV
    TORGOV, VN
    BAUMSHTEIN, MV
    GETSOV, LB
    [J]. STRENGTH OF MATERIALS, 1981, 13 (04) : 401 - 407
  • [27] Oxidation Catalysts for Natural Gas Engine Operating under HCCI or SI Conditions
    Williams, Shazam
    Hu, Linjie Robin
    Nakazono, Tohru
    Ohtsubo, Hiroyuki
    Uchida, Miwa
    [J]. SAE INTERNATIONAL JOURNAL OF FUELS AND LUBRICANTS, 2009, 1 (01) : 326 - 337
  • [28] 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
  • [29] Initial tests of emissions of harmful compounds in the exhaust of a marine gas turbine engine in operating conditions
    Wirkowski, P.
    Markowski, J.
    Kniaziewicz, T.
    [J]. INTERNATIONAL AUTOMOTIVE CONFERENCE (KONMOT2018), 2018, 421
  • [30] Hardware-in-the-loop simulation of two-shaft gas turbine engine's electronic control unit
    Montazeri-Gh, Morteza
    Abyaneh, Soroush
    Kazemnejad, Sajjad
    [J]. PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART I-JOURNAL OF SYSTEMS AND CONTROL ENGINEERING, 2016, 230 (06) : 512 - 521