Air inlet filter for gas turbine engine
Номер патента: CA1266382A
Опубликовано: 06-03-1990
Автор(ы): William M. O'connor
Принадлежит: Avco Corp
Опубликовано: 06-03-1990
Автор(ы): William M. O'connor
Принадлежит: Avco Corp
Реферат: ABSTRACT OF THE DISCLOSURE An annular air filter is rotationally mounted within a plenurn box, which in turn is securely mounted to the inlet end of a gas turbine engine. At least a portion of the annular air filter surrounds the inlet end of the engine. A motor is provided to rotationally drive the air filter relative to both the plenum box and the engine. An air pressure nozzle is disposed adjacent the inner circumfer-ential surface of the air filter, and a vacuum nozzle is disposed adjacent the outer circumferential surface thereof. The air pressure and vacuum nozzles clean the air filter as the air filter is rotated relative thereto.
Filtering chamber for gas turbines and method for maintenance thereof
Номер патента: RU2664097C2. Автор: Марко САНТИНИ,Джордже МАРЧЕТТИ. Владелец: Нуово Пиньоне СРЛ. Дата публикации: 2018-08-15.