The patent badge is an abbreviated version of the USPTO patent document. The patent badge does contain a link to the full patent document.

The patent badge is an abbreviated version of the USPTO patent document. The patent badge covers the following: Patent number, Date patent was issued, Date patent was filed, Title of the patent, Applicant, Inventor, Assignee, Attorney firm, Primary examiner, Assistant examiner, CPCs, and Abstract. The patent badge does contain a link to the full patent document (in Adobe Acrobat format, aka pdf). To download or print any patent click here.

Date of Patent:
Jan. 02, 2024

Filed:

Dec. 27, 2021
Applicant:

Parallel Flight Technologies, Inc., Ben Lomond, CA (US);

Inventors:

Joshua Resnick, Ben Lomond, CA (US);

David Adams, Ben Lomond, CA (US);

Robert Hulter, Ben Lomond, CA (US);

Seth McGann, Ben Lomond, CA (US);

Brian Eiseman, Ben Lomond, CA (US);

Assignee:

Parallel Flight Technologies, Inc., Ben Lomond, CA (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64D 31/06 (2006.01); B60L 58/12 (2019.01); B60L 7/10 (2006.01); B60L 15/20 (2006.01); B64C 27/32 (2006.01); B64D 27/24 (2006.01); B64D 27/26 (2006.01); B64D 33/08 (2006.01); B64D 27/02 (2006.01);
U.S. Cl.
CPC ...
B64D 31/06 (2013.01); B60L 7/10 (2013.01); B60L 15/20 (2013.01); B60L 58/12 (2019.02); B64C 27/32 (2013.01); B64D 27/24 (2013.01); B64D 27/26 (2013.01); B64D 33/08 (2013.01); B60L 2200/10 (2013.01); B64D 2027/026 (2013.01);
Abstract

One variation of a system for generating thrust at an aerial vehicle includes: a primary electric motor; a rotor coupled to the motor; an internal-combustion engine; a clutch interposed between the motor and an output shaft of the internal-combustion engine; an engine shroud defining a shroud inlet between the rotor and the internal-combustion engine, extending over the internal-combustion engine, and defining a shroud outlet opposite the rotor; a cooling fan coupled and configured to displace air through the engine shroud; and a local controller configured to receive a rotor speed command specifying a target rotor speed, adjust a throttle setpoint of the internal-combustion engine according to the target rotor speed and a state of charge of a battery in the aerial vehicle, and drive the primary electric motor to selectively output torque to the rotor and to regeneratively brake the rotor according to the target rotor speed.


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