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US Patent 11713722 Gas turbine engine compressor particulate offtake

OverviewStructured DataIssuesContributorsActivity
Is a
Patent
Patent
0
Date Filed
May 8, 2020
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Date of Patent
August 1, 2023
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Patent Application Number
16870269
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Patent Citations
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US Patent 9046056 Inlet particle separator system for a gas turbine engine
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US Patent 9623354 System for extracting matter through variable bleed valves in turbines
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US Patent 9945260 Hub of an intermediate casing for an aircraft turbojet engine comprising doors with contoured geometry
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US Patent 11035372 Pneumatic controller for controlling a bleed valve
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US Patent 10030539 Gas turbine engine inner case including non-symmetrical bleed slots
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US Patent 11199131 Multistage axial compressor and gas turbine
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US Patent 7624581 Compact booster bleed turbofan
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US Patent 8899050 Compressor for a gas turbine
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Patent Citations Received
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US Patent 11927140 Gas turbine engine with guided bleed air dump
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Patent Jurisdiction
United States Patent and Trademark Office
United States Patent and Trademark Office
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Patent Number
11713722
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Patent Primary Examiner
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Todd E. Manahan
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CPC Code
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F02C 7/06
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F02C 9/18
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F02C 7/055
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B64D 2013/0607
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F02C 7/052
0
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F02C 6/08
0

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