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. 30, 2024

Filed:

Feb. 03, 2022
Applicant:

Volocopter Gmbh, Bruchsal, DE;

Inventors:

Martin Stobbe, Inning, DE;

Krishna Pal Rajput, Munich, DE;

Sebastian Mores, Munich, DE;

Assignee:

Volocopter GmbH, Bruchsal, DE;

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64C 29/00 (2006.01); B64C 3/16 (2006.01); B64C 3/32 (2006.01); B64C 39/06 (2006.01); B64D 27/24 (2024.01);
U.S. Cl.
CPC ...
B64C 29/0025 (2013.01); B64C 3/16 (2013.01); B64C 3/32 (2013.01); B64C 39/068 (2013.01); B64D 27/24 (2013.01);
Abstract

A VTOL aircraft () having a fuselage () for transporting passengers and/or load, front and rear wings () attached to the fuselage, a right connecting beam () and a left connecting beam (), which connecting beams structurally connect the front wing and the rear wing, and which connecting beams are spaced apart from the fuselage, and at least two lifting units (M-M) on each one of the connecting beams. The lifting units each include at least one propeller () and at least one motor () driving the propeller, preferably an electric motor, and are arranged with their respective propeller axis in an essentially vertical orientation. The front wing, at least in portions thereof, has a sweep angle γ between γ=45° and γ=135°, and the rear wing, at least in portions thereof, has a forward sweep with sweep angle β≥30°.


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