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Title:
Gas turbine engine particle separation device
Document Type and Number:
Japanese Patent JP6111040
Kind Code:
B2
Abstract:
Embodiments of the present invention provide an inlet particle separator (100) for a gas turbine engine having an inlet flow path (102), a scavenge flow path (104), a core flow path (106), and a flow splitter (114) disposed between the scavenge and core flow paths. A plurality of grooves (200) may be disposed about an inner surface of a wall of the separator within the inlet flow path (102).

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Inventors:
Jeffrey Meyer
Brian Roberts
Jonathan Anisco
Application Number:
JP2012230387A
Publication Date:
April 05, 2017
Filing Date:
October 18, 2012
Export Citation:
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Assignee:
GENERAL ELECTRIC COMPANY
International Classes:
F02C7/052; B01D45/08
Domestic Patent References:
JP2008169834A
JP5575753A
JP2007315385A
JP2007130747A
JP200996966A
Foreign References:
US5605292
US3885931
Attorney, Agent or Firm:
Arakawa Satoshi
Hirokazu Ogura
Toshihisa Kurokawa
Takuto Tanaka



 
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