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US Patent 12071234 Hybrid power systems for different modes of flight

Patent 12071234 was granted and assigned to Kitty Hawk on August, 2024 by the United States Patent and Trademark Office.

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Contents

Is a
Patent
Patent
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Patent attributes

Patent Applicant
Kitty Hawk
Kitty Hawk
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Current Assignee
Kitty Hawk
Kitty Hawk
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Patent Jurisdiction
United States Patent and Trademark Office
United States Patent and Trademark Office
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Patent Number
120712340
Patent Inventor Names
Pranay Sinha0
Damon Vander Lind0
Date of Patent
August 27, 2024
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Patent Application Number
182447850
Date Filed
September 11, 2023
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Patent Citations
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US Patent 6923404 Apparatus and methods for variable sweep body conformal wing with application to projectiles, missiles, and unmanned air vehicles
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US Patent 6978970 Aircraft with foldable tail assembly
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US Patent 7011274 Aircraft
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US Patent 7049792 Method and apparatus for a hybrid battery configuration for use in an electric or hybrid electric motive power system
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US Patent 7077358 Helicopter with torque-correcting thruster device
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US Patent 7086843 Cooling fan hub assembly
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US Patent 7090164 Method for producing a lift and a horizontal thrust
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US Patent 7159817 Vertical take-off and landing (VTOL) aircraft with distributed thrust and control
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Patent Primary Examiner
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Medhat Badawi
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CPC Code
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B64D 27/02
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B64D 27/24
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B64D 31/06
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G05D 1/101
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Y02T 10/7072
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Y02T 50/40
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Y02T 50/60
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Y02T 10/70
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Patent abstract

During a cruise mode, a cruise-only propeller provides thrust using power from a first power source. During a hovering mode and a transitional mode, the propeller provides no thrust. The first power source includes an internal combustion engine; a second power source includes a high discharge rate battery and a high energy battery. The propeller is electrically connected to the first power source and is electrically disconnected from the second power source. During the hovering mode and the transitional mode, a hover-and-transition-only tiltrotor provides thrust using power from the second power source. During a vertical landing, the tiltrotor switches power sources from the high energy battery to the high discharge rate battery, independent of current draw. The tiltrotor is electrically disconnected from the first power source and is electrically connected to the second power source. During the cruise mode, the tiltrotor provides no thrust.

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