|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||55/306 ; 55/385B ; 415/121G|
|발명자 / 주소|
|출원인 / 주소|
|인용정보||피인용 횟수 : 17 인용 특허 : 3|
A particle separator for a gas turbine engine is described having an inlet passage to the compressor of the gas turbine engine, with the inlet passageway being defined by an inner wall and an outer wall. The inner wall diverges outwardly to form a throat with a diverging outer wall and converges inwardly downstream thereof. A first bypass opening is provided immediately upstream of the diverging inner wall, whereby solid and liquid particles can be diverted and passed overboard. A splitter ring is provided in the inlet passageway downstream of the conver...
In a gas turbine engine compressor inlet, an airflow particle separator having an axis, the inlet having an inner wall and an outer wall of circular cross-section respectively defining an axial annular passageway, said inner wall including an inner wall portion diverging in a downstream direction away from the separator axis, a bypass opening defined in the inner wall immediately upstream of the diverging wall portion, the bypass opening communicating with a bypass conduit which in turn communicates with a collector shroud adapted to dump said particles ...