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US Patent 10759545 Hybrid electric aircraft system with distributed propulsion

OverviewStructured DataIssuesContributorsActivity
Is a
Patent
Patent
Date Filed
June 19, 2018
Date of Patent
September 1, 2020
Patent Application Number
16012040
Patent Citations
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US Patent 10107500 Gas turbine engine with selective flow path
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US Patent 10112696 Stabilizer sacrificial surfaces
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US Patent 10267263 Exhaust duct for turbine forward of fan
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US Patent 10435163 Aircraft propelled by a turbojet engine with contrarotating fans
0
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US Patent 10287991 Gas turbine engine with paired distributed fan sets
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US Patent 10450079 Propulsive wing of an aircraft
0
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US Patent 10071801 Tri-rotor aircraft capable of vertical takeoff and landing and transitioning to forward flight
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US Patent 10106265 Stabilizer assembly for an aircraft AFT engine
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Patent Citations Received
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US Patent 11312502 Gas-electric propulsion system for an aircraft
0
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US Patent 11673678 Gas-electric propulsion system for an aircraft
0
Patent Jurisdiction
United States Patent and Trademark Office
United States Patent and Trademark Office
Patent Number
10759545
Patent Primary Examiner
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Aaron L Troost

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