Particle separator and separating method for gas turbine engine

F - Mech Eng,Light,Heat,Weapons – 02 – C

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F02C 9/18 (2006.01) F02C 7/052 (2006.01)

Patent

CA 2671718

A system and method for particle separation in a gas turbine engine centrifugal impeller bleed air system using a tangential velocity component of the compressor bleed air to centrifuge the particles radially outwardly and convey the particles circumferentially, away from a clean air outlet and towards a particle outlet where the particles are extracted from the bleed air.

Un système et une méthode permettant la séparation de particules dans un système de prélèvement d'air d'une turbine centrifuge d'une turbine à gaz au moyen d'un composant de vitesse tangentielle du prélèvement d'air de compresseur pour centrifuger les particules de manière radiale vers l'extérieur et les transporter de manière circonférentielle à l'écart d'une sortie d'air pur et vers une sortie de particules où celles-ci sont extraites du prélèvement d'air.

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