A Review of Materials for Gas Turbines Firing Syngas Fuels

Gibbons, Thomas¹  Wright, Ian G¹ 

[1] ORNL

关键词: COAL;    COATINGS;    COMBUSTION;    EFFICIENCY;    ENGINES;    GAS TURBINES;    GREENHOUSE GASES;    IMPURITIES;    MODIFICATIONS;    NATURAL GAS;    PARTICULATES;    POWER GENERATION;    PRICES;    RELIABILITY;    SULFUR;    THERMAL BARRIERS;    TURBINES;    WATER VAPOR advanced gas turbines;    gas turbine materials;    syngas turbines;    hydrogen turbines;   

DOI  :  10.2172/970884
RP-ID  :  ORNL/TM-2009/137
PID  :  OSTI ID: 970884
Others  :  Other: AA2045000
Others  :  FEAA070
Others  :  TRN: US201003%%743

美国|英语

来源: SciTech Connect

【 摘 要 】

Following the extensive development work carried out in the 1990's, gas turbine combined-cycle (GTCC) systems burning natural gas represent a reliable and efficient power generation technology widely used in many parts of the world. A critical factor was that, in order to operate at the high turbine entry temperatures required for high efficiency operation, aero-engine technology, i.e., single-crystal blades, thermal barrier coatings, and sophisticated cooling techniques had to be rapidly scaled up and introduced into these large gas turbines. The problems with reliability that resulted have been largely overcome, so that the high-efficiency GTCC power generation system is now a mature technology, capable of achieving high levels of availability. The high price of natural gas and concern about emission of greenhouse gases has focused attention on the desirability of replacing natural gas with gas derived from coal (syngas) in these gas turbine systems, since typical systems analyses indicate that IGCC plants have some potential to fulfil the requirement for a zero-emissions power generation system. In this review, the current status of materials for the critical hot gas path parts in large gas turbines is briefly considered in the context of the need to burn syngas. A critical factor is that the syngas is a low-Btu fuel, and the higher mass flow compared to natural gas will tend to increase the power output of the engine. However, modifications to the turbine and to the combustion system also will be necessary. It will be shown that many of the materials used in current engines will also be applicable to units burning syngas but, since the combustion environment will contain a greater level of impurities (especially sulfur, water vapor, and particulates), the durability of some components may be prejudiced. Consequently, some effort will be needed to develop improved coatings to resist attack by sulfur-containing compounds, and also erosion.