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:
Oct. 10, 2023

Filed:

Oct. 09, 2020
Applicant:

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

Inventors:

Jacob S. Izraelevitz, Pasadena, CA (US);

Brett A. Kennedy, Altadena, CA (US);

Amanda R. Bouman, Pasadena, CA (US);

Daniel Pastor Moreno, Pasadena, CA (US);

Matthew James Lindsay Anderson, Pasadena, CA (US);

Paul M. Nadan, San Carlos, CA (US);

Joel W. Burdick, Pasadena, CA (US);

Assignee:
Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64C 1/30 (2006.01); B64U 10/13 (2023.01); B64U 30/12 (2023.01); B64U 30/20 (2023.01); B64U 70/00 (2023.01); B64C 39/02 (2023.01); B64U 50/19 (2023.01);
U.S. Cl.
CPC ...
B64C 39/024 (2013.01); B64C 1/30 (2013.01); B64U 10/13 (2023.01); B64U 30/12 (2023.01); B64U 30/20 (2023.01); B64U 50/19 (2023.01); B64U 70/00 (2023.01);
Abstract

A ballistically launched foldable multirotor vehicle has a central body frame. A battery is located in an upper vertical location of the vehicle and positions a center of mass of the vehicle to provide aerodynamic stability during a launch. Fins are attached to the central body frame such that aerodynamic forces on the fins shift an aerodynamic center (AC) of the vehicle downward below the center of mass of the vehicle. Three or more foldable arms are attached to the central body frame via a hinge and exist in two states—a closed state where the foldable arms are parallel to a central body axis, and an open state (after launch) where the foldable arms extend radially outward perpendicular to the central body axis. Rotors mounted to each foldable arm are controlled by a motor to enable flight.


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