|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||60/39092 ; 55/306|
|발명자 / 주소|
|출원인 / 주소|
|인용정보||피인용 횟수 : 54 인용 특허 : 11|
A gas turbine engine utilizes a main and at least one auxiliary particle separator for enhancing the separation of foreign particles from a stream of air entering the engine. The engine includes interior walls which collectively define an engine intake passageway and a compressor inlet passageway in flow communication with the intake passageway so as to provide a primary flowpath for air traveling through the engine to the engine compressor. The main and auxiliary particle separators each include a passageway associated with a corresponding interior wall...
A particle separator system for a gas turbine engine including interior walls defining an engine intake passageway including a throat for receiving engine intake air and an annular compressor inlet passageway in flow communication with the engine intake passageway, said system comprising: a main particle separator including an inlet passageway disposed downstream of said throat and in flow communication with the engine intake passageway for receiving a portion of foreign particles carried by the air entering the engine intake passageway, said inlet passa...