GAS TURBINE POWER GENERATION SYSTEM WITH A HIGH PRESSURE COMPRESSOR AND AN ADDED FORWARD LOW PRESSURE COMPRESSOR

Provided is a gas turbine power generation system, including a core engine and a low pressure compressor. The core engine includes a high pressure compressor, a combustor, and a high pressure turbineconfigured in a serial flow arrangement. The high pressure compressor and the high pressure turbine are coupled together by a first shaft. The low pressure compressor is positioned axially forward ofthe core engine and is coupled to the first shaft. 本发明提供种燃气涡轮发电系统，其包括核心发动机和低压压缩机。所述核心发动机包括被构造成串流布置的高压压缩机、燃烧器和高压涡轮。所述高压压缩机和所述高压涡轮通过第轴联接在起。所述低压压缩机定位在所述核心发动机轴向前方，并联接到所述第轴。