发明授权
US6101983A Modified gas turbine system with advanced pressurized fluidized bed combustor cycle 失效
改进型燃气轮机系统采用先进的加压流化床燃烧器循环

Modified gas turbine system with advanced pressurized fluidized bed
combustor cycle
摘要:
A modified gas turbine system is provided that adapts an advanced pressurized fluidized bed combustor cycle for use with existing combustion turbine technology. To accommodate current combustion turbine technology, the air extracted from the compressor discharge is limited, e.g. to about 20% of the total. The additional air required for the APFBC cycle is provided by an auxiliary source of compressed air. The compressor discharge air that is not extracted is used for combustion of the fuel gas produced by the carbonizer and also provides internal cooling as required by conventional combustion turbine design. A separate expander turbine is used to recover energy from the vitiated air from the PFBC. Energy from the vitiated air may further be recovered by directing the expander exhaust to an HRSG.
公开/授权文献
信息查询
0/0