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System And Method With Inlet Particle Separator

Abstract: ABSTRACT A turbine engine system includes an inlet particle separator (36) receiving an inlet fluid flow and having a clean outlet (52) for a first flow of substantially clean fluid, and a scavenge outlet (54) for a second flow of scavenge fluid. A fluid pump (64) communicates with the scavenge outlet (54). The flow of scavenge fluid through the fluid pump (64) is selectively regulated. FIG. 2

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Patent Information

Application #
Filing Date
12 December 2015
Publication Number
33/2016
Publication Type
INA
Invention Field
ELECTRONICS
Status
Email
Parent Application

Applicants

GENERAL ELECTRIC COMPANY
1 River Road Schenectady, New York 12345 USA

Inventors

1. YOUNES, Firas
1000 Western Ave. Lynn, MA 01910 USA
2. KOBAYASHI, Sukeyuki
GE Aviation Systems 1354 Clifford Avenue, P.O. Box 2909 Loves Park, IL 61132 USA

Specification

Claims:As Attached , Description:As Attached

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