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:
Feb. 06, 2024

Filed:

Oct. 22, 2021
Applicant:

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

Inventors:

Ellande Tang, Pasadena, CA (US);

Patrick Spieler, Pasadena, CA (US);

Matthew J Anderson, Pasadena, CA (US);

Soon-Jo Chung, La Cañada, CA (US);

Assignee:
Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64C 29/00 (2006.01); B64C 3/56 (2006.01); B64C 5/06 (2006.01); B64U 10/20 (2023.01); B64U 30/12 (2023.01); B64U 101/58 (2023.01);
U.S. Cl.
CPC ...
B64C 29/0025 (2013.01); B64C 3/56 (2013.01); B64C 5/06 (2013.01); B64U 10/20 (2023.01); B64U 30/12 (2023.01); B64U 2101/58 (2023.01);
Abstract

An air transport vehicle that capitalizes on the strengths and complexities of a fixed and rotary winged aircraft. The air transport vehicle comprises a body aerodynamically designed to avoid substantial drag. The vehicle has a plurality of rotors configured to generate vertical thrust with a rear rotor configured to generate forward thrust. Additionally, each of the rotors are connected to the fixed wing elements and the fixed wing is positioned about the center of mass of the fuselage. Furthermore, each of the rotors are positioned at a fixed tilt angle such that the stability of the vehicle is maintained in a number of different flight configurations.


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