Experimental and numerical investigation of an innovative non-combustion impulse gas turbine for micro-scale electricity generation

被引:1
|
作者
Liaw, Kim Leong [1 ]
Ong, Khai Chuin [1 ]
Zar, Muhammad Aliff B. Mohd Ali [1 ]
Lai, Wen Kang [1 ]
Muhammad, M. Fadhli B. [1 ,2 ]
Firmansyah [2 ]
Kurnia, Jundika C. [1 ]
机构
[1] Univ Teknol PETRONAS, Dept Mech Engn, Bandar Seri Iskandar 32610, Perak Darul Rid, Malaysia
[2] PETRONAS Res Sdn Bhd, Bandar Baru Bangi, Selangor, Malaysia
关键词
Computational fluid dynamics; Sliding mesh and six degrees of freedom (sDOF); Performance and operating envelope; Remote offshore oil platform; ORGANIC RANKINE-CYCLE; AXIAL TURBINE; DESIGN; OPTIMIZATION; PERFORMANCE; OIL;
D O I
10.1016/j.energy.2022.126433
中图分类号
O414.1 [热力学];
学科分类号
摘要
Fulfilling electricity demand in a remote platform has been a great challenge for oil and gas industry. With only pressurized gas line available, the choice of technology that can be implemented is limited; one of it is impulse gas turbine. At the moment, no studies investigating the performance of a compact impulse gas turbine which utilizes pressurized gas line has been reported, hindering the wide adoption of this technology. This study is therefore conducted with the main objective to investigate the performance of small scale impulse gas turbine for electricity generation by using computational fluid dynamics (CFD) approach in tandem with experimental validation. Three-dimensional computational model for the turbine is developed. Concurrently, an experimental set-up, consisting of micro impulse gas turbine, electric generator, flow loop and control system, is prepared to validate the model prediction. The effect of several key parameters, such as working fluid, rotational speed, mass flow rate and input pressure are evaluated to obtain operating envelope of the turbine. Overall, good agreement is achieved between numerical model prediction and experimental measured value. On the effect of working fluid, the results indicate that the impulse gas turbine driven by natural gas at 69 bar produce maximum power output of 1743.81 W at lower speed of 4500 RPM while maximum power of 1084.04 W can be achieved when driven by compressed air at 19 bar at rotational speed of 7000 RPM. In addition, a complete operating envelope for the turbine operating with either compressed air or natural gas has been developed. Furthermore, the effect of distance between nozzle outlet and turbine blade has been evaluated for which the optimum distance within studied range is obtained: 49.62 mm for one with compressed air and 54.62 mm for one with natural gas. The result from this study is expected to serve as a guideline in designing micro impulse gas turbine for electricity generation especially for remote offshore platform.
引用
收藏
页数:15
相关论文
共 44 条
  • [31] EXPERIMENTAL INVESTIGATION OF COMBUSTION INSTABILITIES IN A LABORATORY-SCALE, MULTI-CAN GAS TURBINE COMBUSTOR
    Beita, Jadeed
    Talibi, Midhat
    Rocha, Nuno
    Ezenwajiaku, Chinonso
    Sadasivuni, Suresh
    Balachandran, Ramanarayanan
    PROCEEDINGS OF ASME TURBO EXPO 2023: TURBOMACHINERY TECHNICAL CONFERENCE AND EXPOSITION, GT2023, VOL 3B, 2023,
  • [32] EXPERIMENTAL AND NUMERICAL DESIGN STUDY FOR A SMALL SCALE JET-STABILIZED MICRO GAS TURBINE COMBUSTOR
    Hasemann, Stefan
    Seliger, Hannah
    Kutne, Peter
    Aigner, Manfred
    PROCEEDINGS OF THE ASME TURBO EXPO: TURBOMACHINERY TECHNICAL CONFERENCE AND EXPOSITION, 2018, VOL 4A, 2018,
  • [33] Numerical investigation on combustion flow characteristics of a micro gas turbine swirl combustor with different protruded bluff body structures
    Liu, Hong
    Zeng, Zhuoxiong
    Guo, Kaifang
    PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART A-JOURNAL OF POWER AND ENERGY, 2023, 237 (07) : 1493 - 1508
  • [34] Experimental and numerical investigation of blade height effects on micro-scale axial turbines performance using compressed air open cycle
    Khalil, Khalil M.
    Mahmoud, S.
    Al-Dadah, R. K.
    ENERGY, 2020, 211
  • [35] EXPERIMENTAL INVESTIGATION OF THE COMBUSTION CHARACTERISTICS OF A DOUBLE-STAGED FLOX®-BASED COMBUSTOR ON AN ATMOSPHERIC AND A MICRO GAS TURBINE TEST RIG
    Zanger, Jan
    Monz, Thomas
    Aigner, Manfred
    ASME TURBO EXPO: TURBINE TECHNICAL CONFERENCE AND EXPOSITION, 2015, VOL 4A, 2015,
  • [36] Experimental investigation of a biomass-fuelled micro-scale tri-generation system with an organic Rankine cycle and liquid desiccant cooling unit
    Jradi, M.
    Riffat, S.
    ENERGY, 2014, 71 : 80 - 93
  • [37] Experimental and numerical investigation on non-premixed CH4/air combustion in a micro Swiss-roll combustor
    Li, Jiaxin
    Yang, Guangyao
    Wang, Shixuan
    Fan, Aiwu
    FUEL, 2023, 349
  • [38] Numerical Investigation of NOx Emission Reduction in Non-Premixed Lean Reverse-Flow Combustor in a Micro Gas Turbine Engine
    Joy, Jesline
    Wang, Peng Cheng
    Panisilvam, Jeggathishwaran
    Yu, Simon Ching Man
    EMISSION CONTROL SCIENCE AND TECHNOLOGY, 2020, 6 (02) : 285 - 300
  • [39] Numerical Investigation of NOx Emission Reduction in Non-Premixed Lean Reverse-Flow Combustor in a Micro Gas Turbine Engine
    Jesline Joy
    Peng Cheng Wang
    Jeggathishwaran Panisilvam
    Simon Ching Man Yu
    Emission Control Science and Technology, 2020, 6 : 285 - 300
  • [40] Experimental and Numerical Investigation of Wall Heat Fluxes in a Gas Fired Furnace: Practicable Models for Swirling Non-Premixed Combustion
    Broukal, Jakub
    Vondal, Jiri
    Hajek, Jiri
    PRES 2012: 15TH INTERNATIONAL CONFERENCE ON PROCESS INTEGRATION, MODELLING AND OPTIMISATION FOR ENERGY SAVING AND POLLUTION REDUCTION, 2012, 29 : 1399 - 1404