초록 ▼

A system for cooling hot section components of a gas turbine engine. The cooling system includes a plurality of compressors, or compression train, and an intercooler disposed between each adjacent pair of compressors so as to achieve the desired pressure and temperature of the cooling air at reduced

A system for cooling hot section components of a gas turbine engine. The cooling system includes a plurality of compressors, or compression train, and an intercooler disposed between each adjacent pair of compressors so as to achieve the desired pressure and temperature of the cooling air at reduced shaft power requirements. The first stage of compression may be provided by the booster, or low pressure compressor, of the engine, with the first intercooler receiving all of the air discharging from the booster. After exiting the first intercooler, a first portion of the booster discharge air is routed to the engine high pressure compressor and a second portion is routed to an inlet of the second compressor of the cooling air compression train. The compressed, cooled air exiting the last, downstream one of the compressors is used for cooling at least a first hot section component of the engine.

대표청구항 ▼

[ What is claimed is:] [1.] A system for cooling at least a first portion of a gas turbine engine having a high pressure compressor and a core gas stream, said cooling system comprising:a plurality of compressors disposed in serial flow relationship with one another and effective for compressing air

[ What is claimed is:] [1.] A system for cooling at least a first portion of a gas turbine engine having a high pressure compressor and a core gas stream, said cooling system comprising:a plurality of compressors disposed in serial flow relationship with one another and effective for compressing air, each of said compressors having an inlet and an outlet, wherein said inlet of a first, upstream one of said compressors receives air having a pressure which is less than or equal to a pressure of the core gas stream at an entrance to the high pressure compressor of the engine, said upstream compressor producing a first compressed airflow, said upstream compressor comprising a low pressure compressor of the engine, and a second compressor comprising a first auxiliary compressor producing a second compressed airflow;a first intercooler effective for reducing a temperature of said first compressed airflow, said first intercooler having a first inlet and a first outlet for said first compressed airflow receiving cooling from said first intercooler, said first inlet in fluid flow communication with said outlet of said upstream compressor and said first outlet in fluid flow communication with said inlet of said second compressor, said first intercooler further including a second inlet and a second outlet for a first coolant fluid providing cooling to said first intercooler, said first compressed airflow received by said first inlet of said first intercooler comprising an entire portion of the airflow discharging through said outlet of said low pressure compressor of the engine, said first compressed airflow discharging from said first outlet of said first intercooler split into a first portion in fluid flow communication with the high pressure compressor of the engine and a second portion in fluid flow communication with said inlet of said first auxiliary compressor;wherein an airflow discharging from a last, downstream one of said compressors is used for cooling said at least a first portion of the engine.