期刊
ENERGY
卷 222, 期 -, 页码 -出版社
PERGAMON-ELSEVIER SCIENCE LTD
DOI: 10.1016/j.energy.2021.119978
关键词
Adiabatic compressed air energy storage system; High-pressure stage turbine; Sliding pressure mode; Thermodynamics analysis; Exergy destruction
资金
- National Key Research and Development Program of China [2017YFB0903602]
The study compared the performance of high-pressure stage turbines under different inlet pressures in NV-CAES system, demonstrating that turbine B has a wider operating range and higher performance, improving system efficiency. By establishing thermodynamic and exergy efficiency models, the performance of NV-CAES systems can be effectively simulated.
A high-pressure stage turbine will discharge energy under sliding pressure mode in compressed air energy storage system (CAES) if without throttle valve installed upstream the turbine (NV-CAES). In this work, four high-pressure stage turbines A similar to D are designed for NV-CAES with 1-D turbine loss model under four inlet pressures of 5.0 MPa, 7.0 MPa, 9.0 MPa and 11.0 MPa, respectively. Simulation results reveal that Turbine B has relatively wider working operation range and higher performance. Then, another high-pressure stage turbine in NV-CAES is designed with General performance curve (GNV-CAES) under inlet pressure 7.0 MPa. Both thermodynamic model and exergy efficiency model were built to simulation system performance of these NV-CAESs. For comparison, a CAES equipped with throttle valve (V-CAES), in which the turbine train works with constant inlet pressure, is also computed. Compared with V-CAES, GNV-CAES reduces the exergy destruction from 52.25 GJ to 46.29 GJ and improves the exergy efficiency by 3.3%. The thermodynamic comparison among NV-CAESs shows that The CAES with Turbine B shows the best performance with the storage pressure of 4.0-13.0 MPa. Thus, properly choosing design conditions of high-pressure stage turbine plays an important role to enhance performance of CAES with sliding pressure discharging mode. (C) 2021 Elsevier Ltd. All rights reserved.
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