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:
Dec. 02, 2025

Filed:

Dec. 10, 2021
Applicant:

Gérard Tavin, Angers, FR;

Inventor:

Gérard Tavin, Angers, FR;

Assignee:
Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64C 29/00 (2006.01); B64C 1/30 (2006.01); B64C 3/56 (2006.01); B64C 27/12 (2006.01); B64C 27/30 (2006.01); B64D 35/024 (2025.01);
U.S. Cl.
CPC ...
B64C 29/0025 (2013.01); B64C 1/30 (2013.01); B64C 3/56 (2013.01); B64C 27/30 (2013.01); B64C 27/12 (2013.01); B64D 35/024 (2024.01);
Abstract

Disclosed is a vertical take-off and landing aerodyne, including a fuselage, two wings, horizontal flight propulsion unit and at least one pair of rotors intended to provide propulsion and lift in the take-off and landing phases. The rotors are retractable and the horizontal flight propulsion unit includes a counter-rotating propeller, situated at the tail of the aerodyne, and a drive unit for rotating the counter-rotating propeller, the counter-rotating propeller being capable of being oriented by a control unit about two axes, one parallel to the yaw axis and the other parallel to the pitch axis of the aerodyne, such that the counter-rotating propeller is used for controlling the attitude of the aerodyne, the latter therefore not having a tail unit.


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