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:
May. 09, 2023

Filed:

May. 06, 2020
Applicant:

Eve Uam, Llc, Wilmington, DE (US);

Inventors:

Adilson Melo, São José dos Campos—SP, BR;

Alberto Dei Castelli, São José dos Campos—SP, BR;

Fabio Zaroni, São José dos Campos—SP, BR;

Felipe Nahime Cursino, São José dos Campos—SP, BR;

Fernando Rodrigues Vianna, São José dos Campos—SP, BR;

Flavia Renata Dantas Alves Silva, São José dos Campos—SP, BR;

Geraldo Carvalho, São José dos Campos—SP, BR;

Igor Miranda Rodrigues, São José dos Campos—SP, BR;

Julio Cesar Graves, São José dos Campos—SP, BR;

Luiz Antonio Madeira, Jr., São José dos Campos—SP, BR;

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

Rafael Desideri de Freitas, São José dos Campos—SP, BR;

Rafael Estefano Reis Cleto, São José dos Campos—SP, BR;

Ricardo Takeshi Demizu, São José dos Campos—SP, BR;

Rodrigo Takashi Lourenco Kawasaki, São José dos Campos—SP, BR;

Thalerson Augusto Mortari Alves, São José dos Campos—SP, BR;

Vinicius Magalhaes Cunha, São José dos Campos—SP, BR;

Yasser Mahmud Abdallah, São José dos Campos—SP, BR;

Assignee:

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

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64C 29/00 (2006.01); B64C 27/26 (2006.01); B64C 3/16 (2006.01); B64C 25/52 (2006.01);
U.S. Cl.
CPC ...
B64C 29/0025 (2013.01); B64C 3/16 (2013.01); B64C 25/52 (2013.01); B64C 27/26 (2013.01);
Abstract

Vertical takeoff and landing (VTOL) aircraft, especially electric VTOL (e-VTOL) aircraft include a fuselage (which may include a pair of ground-engaging skids) defining a longitudinal axis of the aircraft, forward and aft pairs of port and starboard aerodynamic wings extending laterally outwardly from the fuselage and forward and aft pairs of port and starboard rotor pods each being in substantial alignment with the longitudinal axis of the fuselage. In specific embodiments, each of the forward and aft pairs of port and starboard rotor pods comprises a forward and aft pair of rotor assemblies.


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