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US Patent 10611477 Closed wing aircraft having a distributed propulsion system

Patent 10611477 was granted and assigned to Textron on April, 2020 by the United States Patent and Trademark Office.

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Patent attributes

Patent Applicant

Current Assignee

Patent Jurisdiction

United States Patent and Trademark Office

Patent Number

Date of Patent

April 7, 2020

Patent Application Number

16526841

Date Filed

July 30, 2019

Patent Citations

US Patent 10227133 Transportation method for selectively attachable pod assemblies

US Patent 10336450 Enhanced net pitching moment multi-wing VTOL compact personal aircraft

US Patent 10232950 Aircraft having a fault tolerant distributed propulsion system

US Patent 10011351 Passenger pod assembly transportation system

US Patent 10124890 Modular nacelles to provide vertical takeoff and landing (VTOL) capabilities to fixed wing aerial vehicles, and associated systems and methods

US Patent 10183746 Aircraft with independently controllable propulsion assemblies

US Patent 10214285 Aircraft having autonomous and remote flight control capabilities

US Patent 10220944 Aircraft having manned and unmanned flight modes

Patent Citations Received

US Patent 12110105 Aircraft having rotor assemblies rotating in parallel planes

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US Patent 11932387 Adaptive transition systems for VTOL aircraft

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US Patent 12084200 Ground state determination systems for aircraft

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US Patent 12103673 Payload saddle assemblies for use on aircraft

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US Patent 11603194 Aircraft having a high efficiency forward flight mode

US Patent 11608173 Aerial delivery systems using unmanned aircraft

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US Patent 11643207 Aircraft for transporting and deploying UAVs

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US Patent 11673662 Telescoping tail assemblies for use on aircraft

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