|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||60/39161 ; 60/395 ; 415/148|
|발명자 / 주소|
|출원인 / 주소|
|인용정보||피인용 횟수 : 29 인용 특허 : 0|
An industrial gas turbine engine includes in serial flow relationship a booster compressor, core engine, power turbine, and flow channel, with the power turbine having a first shaft, joined to the booster compressor, and an output shaft, and the flow channel having an outlet. Means for selectively varying flow area of the channel outlet are provided for controlling stall margin of the booster compressor in an exemplary embodiment of the engine and method of operation. The flow area varying means is effective for providing a minimum area of the channel ou...
A gas turbine engine of the marine and land-based industrial (M&I) type for powering a load connected thereto comprising: a booster compressor for providing compressed airflow; a core engine disposed in flow communication with said booster compressor for receiving said compressed airflow and generating combustion gases; a power turbine disposed in flow communication with said core engine for receiving said combustion gases, said power turbine including a first shaft, joined to said booster compressor for rotation therewith, and an output shaft for provid...