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. 11, 2024

Filed:

Sep. 15, 2023
Applicant:

Archer Aviation, Inc., San Jose, CA (US);

Inventors:

Fernanda Aline Matta De Paiva, Los altos Hills, CA (US);

Scott Furman, Menlo Park, CA (US);

Sergio Henrique Soares Ferreira, San Jose, CA (US);

Damien Bardon, San Jose, CA (US);

Assignee:

ARCHER AVIATION, INC., San Jose, CA (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64C 29/00 (2006.01); B64C 11/46 (2006.01); B64C 13/50 (2006.01);
U.S. Cl.
CPC ...
B64C 29/0033 (2013.01); B64C 11/46 (2013.01); B64C 13/50 (2013.01); B64D 2221/00 (2013.01);
Abstract

Aspects of this present disclosure relate to flight control of electric aircrafts and other vehicles. In one embodiment, an aircraft is disclosed comprising: a fuselage; two wings; a plurality of lift propellers, the lift propellers disposed aft of the wings during forward flight; plurality of tilt propellers that are tiltable between vertical lift and forward propulsion configurations, the tilt propellers disposed forward of the wings during forward flight; a plurality of tilt propellor actuators that tilt propellers between vertical lift and forward propulsion configurations, the tilt propellor actuators on opposite sides of the fuselage; and a plurality of electrical buses coupled to a flight control computer; wherein the flight control computer is configured to provide control signals for at least one of the lift propellers mounted to one of the wings and one of the tilt propellers mounted to the other wing via the same electrical bus.


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