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US Patent 10315761 Aircraft propulsion assembly

Patent 10315761 was granted and assigned to Bell Helicopter on June, 2019 by the United States Patent and Trademark Office.

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Contents

Is a
Patent
Patent

Patent attributes

Patent Applicant
Current Assignee
Patent Jurisdiction
United States Patent and Trademark Office
United States Patent and Trademark Office
Patent Number
10315761
Patent Inventor Names
Paul K. Oldroyd0
John Richard McCullough0
Date of Patent
June 11, 2019
Patent Application Number
15200261
Date Filed
July 1, 2016
Patent Citations
‌
US Patent 10124890 Modular nacelles to provide vertical takeoff and landing (VTOL) capabilities to fixed wing aerial vehicles, and associated systems and methods
0
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US Patent 10011351 Passenger pod assembly transportation system
0
Patent Citations Received
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US Patent 12134466 Unmanned aerial vehicles including wing capture devices and related methods
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US Patent 11511854 Variable pitch rotor assembly for electrically driven vectored thrust aircraft applications
0
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US Patent 12084200 Ground state determination systems for aircraft
0
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US Patent 12091173 UAV with distributed propulsion and blown control surfaces
0
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US Patent 12103673 Payload saddle assemblies for use on aircraft
0
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US Patent 12110105 Aircraft having rotor assemblies rotating in parallel planes
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US Patent 11492116 Tiltrotor aircraft having tiltable forward and aft rotors
0
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US Patent 10618656 Tiltrotor aircraft having interchangeable payload modules
0
...
Patent Primary Examiner
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Brian M O'Hara
Patent abstract

In some embodiments, a propulsion assembly for an aircraft includes a nacelle, at least one self-contained fuel tank disposed within the nacelle operable to contain a liquid fuel, an engine disposed within the nacelle operable to run on the liquid fuel, a drive system mechanically coupled to the engine and operable to rotate responsive to rotation of the engine, a rotor hub mechanically coupled to the drive system operable to rotate responsive to rotation of the drive system and a proprotor mechanically coupled to the rotor hub and operable to rotate therewith.

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