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:
Jun. 18, 2024

Filed:

Jul. 28, 2023
Applicant:

Joby Aero, Inc., Santa Cruz, CA (US);

Inventors:

Gregor Veble Mikic, Santa Cruz, CA (US);

Alex Stoll, Santa Cruz, CA (US);

JoeBen Bevirt, Santa Cruz, CA (US);

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64C 3/38 (2006.01); B64C 7/00 (2006.01); B64C 27/52 (2006.01); B64C 29/00 (2006.01); B64C 1/06 (2006.01);
U.S. Cl.
CPC ...
B64C 29/0033 (2013.01); B64C 3/38 (2013.01); B64C 7/00 (2013.01); B64C 27/52 (2013.01); B64C 1/061 (2013.01); B64C 1/068 (2013.01);
Abstract

The aircraft can include: an airframe, a tilt mechanism, a payload housing, and can optionally include an impact attenuator, a set of ground support members (e.g., struts), a set of power sources, and a set of control elements. The airframe can include: a set of rotors and a set of support members. By utilizing a larger rotor blade area (and/or larger rotor disc area) and adjusting the blade pitch and RPM, the rotors can augment the lift generated by the aerodynamic profile of the aircraft in the forward flight mode in addition to providing forward thrust. Variants generating lift with the rotors can reduce or eliminate additional control surfaces (e.g., wing flaps, ailerons, ruddervators, elevators, rudder, etc.) on the aircraft since the thrust and motor torque is controllable (thereby indirectly controlling lift) at each rotor, thereby enabling pitch, yaw, and/or roll control during forward flight.


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