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:
Aug. 25, 2020

Filed:

May. 29, 2017
Applicant:

Volocopter Gmbh, Bruchsal, DE;

Inventors:

Thomas Senkel, Berlin, DE;

Stephan Wolf, Karlsruhe, DE;

Alexander Zosel, Rheinstetten, DE;

Assignee:

Volocopter GmbH, Bruchsal, DE;

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64D 31/06 (2006.01); B64D 27/24 (2006.01); B64D 25/00 (2006.01); B64D 17/80 (2006.01); B64D 11/06 (2006.01); B64C 39/02 (2006.01); B64C 27/473 (2006.01); B64C 27/20 (2006.01); B64C 27/14 (2006.01); B64C 27/08 (2006.01); B64C 25/56 (2006.01); B64C 25/52 (2006.01); B64C 25/34 (2006.01); G05D 1/08 (2006.01); B64D 31/04 (2006.01); B64C 29/00 (2006.01);
U.S. Cl.
CPC ...
B64D 31/06 (2013.01); B64C 25/34 (2013.01); B64C 25/52 (2013.01); B64C 25/56 (2013.01); B64C 27/08 (2013.01); B64C 27/14 (2013.01); B64C 27/20 (2013.01); B64C 27/473 (2013.01); B64C 29/0025 (2013.01); B64C 39/024 (2013.01); B64D 11/0689 (2013.01); B64D 17/80 (2013.01); B64D 25/00 (2013.01); B64D 27/24 (2013.01); B64D 31/04 (2013.01); G05D 1/0858 (2013.01); Y02T 50/64 (2013.01);
Abstract

A vertical takeoff and landing aircraft () for transporting persons or loads, including a plurality of preferably equivalent and redundant electric motors () and propellers (), substantially arranged in one surface, wherein each propeller is assigned an individual electric motor to drive the propeller, the aircraft being characterized in that at least one attitude sensor is provided for attitude control of the aircraft () in an active signal connection to at least one signal processing unit which is designed or set up to automatically perform the attitude control based on measurement data from the attitude sensor by regulating the speed of at least some of the electric motors (), preferably with signal actions of the speed controller assigned to each electric motor such that the aircraft () is positioned in space with the surface defined by the propeller () substantially horizontal at all times, without control input by a pilot or a remote control.


Find Patent Forward Citations

Loading…