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:
Mar. 04, 2025

Filed:

May. 11, 2022
Applicant:

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

Inventors:

Joshua Alan Resnick, Ben Lomond, CA (US);

Robert Hulter, Ben Lomond, CA (US);

David Adams, Ben Lomond, CA (US);

Paul Allen Kele, Soquel, CA (US);

Maxwell Lewis Kauker, Soquel, CA (US);

Assignee:

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

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64D 35/08 (2006.01); B64C 39/02 (2023.01); B64D 27/02 (2006.01); B64D 27/04 (2006.01); B64D 27/24 (2024.01); B64D 33/02 (2006.01); B64D 33/08 (2006.01); B64D 35/02 (2024.01); B64U 30/20 (2023.01); B64U 50/19 (2023.01); B64U 50/11 (2023.01);
U.S. Cl.
CPC ...
B64D 35/08 (2013.01); B64C 39/024 (2013.01); B64D 27/04 (2013.01); B64D 27/24 (2013.01); B64D 33/08 (2013.01); B64D 35/02 (2013.01); B64D 27/026 (2024.01); B64D 2033/024 (2013.01); B64U 30/20 (2023.01); B64U 50/11 (2023.01); B64U 50/19 (2023.01);
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 disengagement mechanism interposed between the motor and an output shaft of the internal-combustion engine; an cooling shroud defining a shroud inlet between the rotor and the internal-combustion engine, extending over the internal-combustion engine, and defining a cooling shroud outlet opposite the rotor; a cooling fan coupled and configured to displace air through the cooling 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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