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Frontiers in Energy

ISSN 2095-1701

ISSN 2095-1698(Online)

CN 11-6017/TK

Postal Subscription Code 80-972

2018 Impact Factor: 1.701

Front. Energy    2020, Vol. 14 Issue (4) : 790-800    https://doi.org/10.1007/s11708-020-0691-2
RESEARCH ARTICLE
Experimental investigation of a novel micro gas turbine with flexible switching function for distributed power system
Xiaojing LV1(), Weilun ZENG1, Xiaoyi DING2, Yiwu WENG2(), Shilie WENG2
1. Research Center for Low Carbon Combustion and Engine System, China-UK Low Carbon College, Shanghai Jiao Tong University, Shanghai 200240, China
2. Gas Turbine Research Institute, School of Mechanical Engineering, Shanghai Jiao Tong University, Shanghai 200240, China
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Abstract

Micro gas turbine (MGT) is widely used in small-scale distributed power systems because of its low emissions and fuel flexibility. However, the under-utilization of its exhaust heat and the low electric efficiency are the main bottlenecks that restrict its application. Additionally, the flexible switching between the power generated by the MGT and the power grid is also a key factor for keeping the secure operation of a distributed power station. Therefore, this paper conducted some experimental investigations of a 30 kW MGT to provide reference solutions for the above issues. This MGT is located at Shanghai Jiao Tong University (SJTU), which is designed by the Gas Turbine Research Institute of SJTU, and is manufactured by a turbo-machinery factory in Chongqing, China. The demonstration prototype is mainly composed of a single stage centrifugal compressor, a radial turbine, a combustor, a high-speed permanent magnet generator, and a control system. The results show that the MGT can achieve steady operation at a low rotational speed from 10000 r/min to 34000 r/min in the case of using oil lubricated bearings, which can greatly reduce the economic cost compared with the use of air bearings. At the same time, the ignition success rate of combustion chamber (CC) reaches 98% at a low rotational speed, and a wide range of stable combustion area can be obtained, because of the novel design method of combustor by referencing the way applied in an axial flow aero-engine. The MGT generating set can achieve functions, such as starting up, ignition, stable operation, loaded operation, grid-connection and stopping. This system also can realize flexibly switching from the start motor mode to the generator mode, and from grid-connected mode to off-grid mode, because the innovative multi-state switching control system is adopted. The above research work can make our state master independent intellectual property rights of micro gas turbine, rather than continue to be subject to the technological monopoly of the developed states, which can provide theoretical and experimental support for the industrialization of MGT in China.

Keywords gas turbine      flexible switching system      control system      distributed power system      emission test     
Corresponding Author(s): Xiaojing LV,Yiwu WENG   
Online First Date: 04 September 2020    Issue Date: 21 December 2020
 Cite this article:   
Xiaojing LV,Weilun ZENG,Xiaoyi DING, et al. Experimental investigation of a novel micro gas turbine with flexible switching function for distributed power system[J]. Front. Energy, 2020, 14(4): 790-800.
 URL:  
https://academic.hep.com.cn/fie/EN/10.1007/s11708-020-0691-2
https://academic.hep.com.cn/fie/EN/Y2020/V14/I4/790
Fig.1  Generating set driven by MGT.
Design parameter Structural parameter
Inlet total pressure/Pa 259379 Inlet radius/mm 125
Inlet temperature/°C 850 Inlet blade high/mm 8
Outlet static pressure/Pa 101325 Export hub radius/mm 27
Mass flow rate/(kg·s–1) 0.587 Export blade High/mm 46.5
Expansion ratio 2.487 Axial length/mm 73.5
Rotation speed/(r·min–1) 34000 Blade number 11
Tab.1  Turbine design and structural parameters
Fig.2  3-D turbine.
Fig.3  Stress nephogram of turbine.
Design parameter Structural parameter
Inlet total pressure/Pa 101325 Inlet hub radius/mm 28
Inlet temperature/°C 27 Inlet blade high/mm 29.4
Outlet static pressure/Pa 236875 Outlet radius/mm 111
Mass flow rate/(kg·s–1) 0.5618 Outlet blade high/mm 5.8
Pressure ratio 2.8 Axial length/mm 58
Rotation speed/(r·min–1) 34000 Blade number 9
Tab.2  Compressor design and structural parameters
Fig.4  3-D compressor.
Fig.5  Stress nephogram of compressor.
Fig.6  3-D assembled compressor and turbine.
Fig.7  Prototype of assembled compressor and turbine.
Fig.8  Prototype of combustor.
Fig.9  Control scheme of MGT generating set.
No ma/(kg? s 1) T2/ °C P2/ MPa mf/(kg?s1) T3/ °C NOx/ppm Comment
1 0.150 135 0.167 0.0042–0.0029 855 30.9 Ignition
2 0.130 135 0.175 0.0039 815 Ignited
3 0.244 135 0.200 0.0078–0.0077 882–913 33.7 WS 1
4 0.245 135 0.200 0.0077 855 33.7 WS 2
5 0.249 135 0.220 0.0086 953 Refueling
6 0.248 135 0.220 0.0080 884 33.3 WS 4
7 0.250 135 0.240 0.0078–0.0079 893 33.7 WS 5
8 0.249 135 0.240 0.0072 843 30.4 WS 6
9 0.488 135 0.261 0.0149 872 33.4 WS 7
10 0.502 175 0.265 0.0150 873 31.5 WS 8
Tab.3  Emissions of micro gas turbine
Fig.10  30 kW-class MGT power generation system.
Fig.11  Diagram of experimental data for speed, temperature, and fuel flow rate of MGT.
Fig.12  Micro gas turbine generator control panel.
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