초록 ▼

A gas turbine engine that includes a steam driven variable speed booster compressor is described. In one embodiment, the engine includes a low pressure turbine and a booster compressor rotatable on a low pressure shaft. The engine further includes a high pressure compressor, a high pressure combusto

A gas turbine engine that includes a steam driven variable speed booster compressor is described. In one embodiment, the engine includes a low pressure turbine and a booster compressor rotatable on a low pressure shaft. The engine further includes a high pressure compressor, a high pressure combustor, and a high pressure turbine rotatable on a high pressure (HP) shaft and forming the core engine. The output of the low pressure compressor is supplied to an intercooler, and the output of the intercooler is supplied to the high pressure compressor. The engine further includes a power turbine downstream of the high pressure turbine, and the power turbine is coupled to a generator by a shaft. The output exhaust of the power turbine is supplied to an exhaust heat boiler, and steam output by the boiler is supplied to, and drives, the low pressure turbine. Steam from the boiler may also be supplied to the high pressure combustor and to the power turbine. Since the steam is generated from the power turbine exhaust heat, the amount of steam flow can be independently varied from the gas turbine engine primary conditions, consistent of course with the gas turbine exhaust flow/temperature limitations.

대표청구항 ▼

[ I claim:] [1.] A gas turbine engine comprising:a low pressure turbine;a booster compressor coupled to said low pressure turbine by a first shaft;a high pressure compressor for receiving airflow from said booster compressor;a high pressure turbine coupled to said high pressure compressor by a secon

[ I claim:] [1.] A gas turbine engine comprising:a low pressure turbine;a booster compressor coupled to said low pressure turbine by a first shaft;a high pressure compressor for receiving airflow from said booster compressor;a high pressure turbine coupled to said high pressure compressor by a second shaft;a combustor located intermediate said high pressure compressor and said high pressure turbine;a power turbine downstream of said high pressure turbine;an exhaust heat boiler coupled to receive exhaust from said power turbine, an outlet of said exhaust heat boiler coupled to an inlet of said low pressure turbine; anda control valve for controlling flow of steam from said exhaust heat boiler to said pressure turbine, wherein a speed of said booster compressor is controllable substantially independently of a speed of said high pressure compressor.