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. 27, 2024

Filed:

Oct. 02, 2018
Applicant:

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

Inventors:

Luiz Fernando Tedeschi Oliveira, São José dos Campos—SP, BR;

Carlos Eduardo de Carvalho, São José dos Campos—SP, BR;

Jay Beever, São José dos Campos—SP, BR;

Assignee:

EMBRAER S.A., São José dos Campos—SP, BR;

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64C 29/00 (2006.01); B64C 23/06 (2006.01); B64C 5/06 (2006.01); B64C 37/02 (2006.01); B64C 39/06 (2006.01);
U.S. Cl.
CPC ...
B64C 29/0033 (2013.01); B64C 5/06 (2013.01); B64C 23/069 (2017.05); B64C 37/02 (2013.01); B64C 39/068 (2013.01);
Abstract

Vertical short takeoff and landing (VSTOL) aircraft include primary airfoils extending outwardly from a forward region of the aircraft fuselage, and secondary empennage airfoils extending outwardly from an aft region of the aircraft fuselage so as to be separated from the forward primary airfoils and thereby define a space therebetween which accommodates non-cyclic controllable propellers operably driven by a respective engine of a propulsion unit. The propulsion units are mounted for pivotal movement within the defined space between the primary airfoil and the secondary empennage airfoils so as to achieve a first operational position wherein the thrust line of the propellers is orientated substantially parallel to the longitudinal axis of the fuselage and a second operational position wherein the thrust line of the propellers is oriented substantially perpendicular to the longitudinal axis of the aircraft. The propulsion units may be mounted aft of the aircraft center of gravity (CG).


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