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US Patent 11859516 Gas turbine engine with third stream

Patent 11859516 was granted and assigned to General Electric on January, 2024 by the United States Patent and Trademark Office.

OverviewStructured DataIssuesContributorsActivity
Is a
Patent
Patent
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Current Assignee
General Electric
General Electric
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Date Filed
August 26, 2022
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Date of Patent
January 2, 2024
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Patent Applicant
General Electric
General Electric
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Patent Application Number
17896579
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Patent Citations
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US Patent 8382430 Aeroengine
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US Patent 8438832 High turning fan exit stator
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US Patent 8459035 Gas turbine engine with low fan pressure ratio
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US Patent 8689538 Ultra-efficient propulsor with an augmentor fan circumscribing a turbofan
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US Patent 8762766 Distributed fault tolerant architecture for a healthcare communication system
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US Patent 7559191 Ducted spinner for engine cooling
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US Patent 7658063 Gas turbine having a single shaft bypass configuration
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US Patent 7762766 Cantilevered framework support for turbine vane
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US Patent 7765786 Aircraft engine with separate auxiliary rotor and fan rotor
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US Patent 8276392 Turboprop engine with an apparatus for the generation of a cooling airflow
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•••
Patent Inventor Names
David Marion Ostdiek
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Patent Jurisdiction
United States Patent and Trademark Office
United States Patent and Trademark Office
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Patent Number
11859516
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Patent Primary Examiner
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Brian Christopher Delrue
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CPC Code
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F05D 2220/36
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F05D 2260/20
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F01D 9/041
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F01D 25/24
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F01D 1/26
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F01D 7/00
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F02C 7/04
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F02K 3/077
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F05D 2200/12
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F05D 2200/14
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•••

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