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:
Jul. 25, 2023

Filed:

Sep. 09, 2019
Applicant:

Embraer S.a., São José dos Campos, BR;

Inventors:

Júlio Cesar Graves, São José dos Campos, BR;

Yasser Mahmud Abdallah, São José dos Campos, BR;

Leandro Guimarães Maia, São José dos Campos, BR;

Carlos Eduardo Vieira De Souza, São José dos Campos, BR;

Luiz Felipe Ribeiro Valentini, São José dos Campos, BR;

Assignee:

EVE UAM, LLC, Wilmington, DE (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64C 27/57 (2006.01); B64C 5/02 (2006.01); B64C 11/00 (2006.01); B64C 27/26 (2006.01); B64C 27/30 (2006.01); B64C 27/68 (2006.01); B64C 29/00 (2006.01); B64C 9/00 (2006.01); B64D 35/02 (2006.01);
U.S. Cl.
CPC ...
B64C 27/57 (2013.01); B64C 5/02 (2013.01); B64C 9/00 (2013.01); B64C 11/00 (2013.01); B64C 27/26 (2013.01); B64C 27/30 (2013.01); B64C 27/68 (2013.01); B64C 29/0025 (2013.01); B64D 35/02 (2013.01);
Abstract

Vertical takeoff and landing (VTOL) aircraft are provided with fixed-position port and starboard wings extending laterally from an elongate fuselage having an empennage at an aft end of the fuselage and a propeller to provide horizontal thrust to the aircraft in a direction of the longitudinal axis thereof. A series of port and starboard rotor units are provided, each of which includes axially opposed rotor blades, and a motor to rotate the rotor blades and provide vertical thrust to the aircraft. A logic control unit (LCU) controllably sets an angular position of the opposed rotor blades along a position axis relative to the longitudinal axis of the aircraft in response to determining an optimal position of the rotor blades during cruise flight operation to thereby minimize airflow disruption over the fixed-position wings.


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