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:
May. 07, 2024

Filed:

Apr. 21, 2021
Applicants:

California Institute of Technology, Pasadena, CA (US);

Toofon, Inc., Pasadena, CA (US);

Inventors:

Morteza Gharib, Altadena, CA (US);

Michael V. Ol, Pasadena, CA (US);

Christopher J. Dougherty, Pasadena, CA (US);

Assignees:

California Institute of Technology, Pasadena, CA (US);

TooFon, Inc., Pasadena, CA (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64C 27/22 (2006.01); B64C 27/08 (2023.01); B64C 27/82 (2006.01); B64C 39/02 (2023.01); B64U 10/13 (2023.01);
U.S. Cl.
CPC ...
B64C 27/08 (2013.01); B64C 27/22 (2013.01); B64C 27/82 (2013.01); B64C 39/024 (2013.01); B64U 10/13 (2023.01);
Abstract

A system and method for controlling a multi-rotor aircraft that implements the unconventional use of an odd number of rotors. The odd or auxiliary rotor is designed to be smaller in diameter than the remaining main rotors and accordingly generates a smaller unbalanced torque and pitch on the aircraft. Additional configurations implement the use of smaller thrust rotors that can be used to generate thrust as well as control yaw and thus counteract any remaining unbalanced torque from the odd auxiliary rotor.


Find Patent Forward Citations

Loading…