US Patent 11066996 Gas turbine engine with inertial particle separator
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Patent abstract
There is disclosed an inertial particle separator communicating with an engine inlet. The inertial particle separator has: a main duct body; a bypass duct; and a splitter defined by an intersection of the main duct and the bypass duct. The main duct and the bypass duct having particular geometric characteristics. A method of separating particles via inertia in an aircraft engine inlet is also provided.
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Patent Inventor Names
Francois Bisson0
Roberto Marrano0
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Patent Jurisdiction
Patent Number
110669960
Date of Patent
July 20, 2021
0Patent Application Number
162028270
Date Filed
November 28, 2018
0Official Website
Patent Citations
Patent Primary Examiner
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US Patent 11066996 Gas turbine engine with inertial particle separator
Infobox
Is a
Patent jurisdiction
Patent number
11066996
Date of patent
July 20, 2021
Patent application number
16202827
Date Filed
November 28, 2018
Patent citations
Patent primary examiner
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