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:
Mar. 02, 2021

Filed:

Feb. 27, 2018
Applicant:

Airbus Helicopters Deutschland Gmbh, Donauworth, DE;

Inventors:

Qinyin Zhang, Augsburg, DE;

Uwe Kiesewetter, Rain am Lech, DE;

Sebastian Mores, Munich, DE;

Marco Schneeberger, Rosenheim, DE;

Marius Bebesel, Augsburg, DE;

Assignee:
Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64C 27/52 (2006.01); B64C 27/08 (2006.01); B64C 27/20 (2006.01); B64C 27/00 (2006.01); B64C 27/28 (2006.01); B64C 29/00 (2006.01);
U.S. Cl.
CPC ...
B64C 27/52 (2013.01); B64C 27/00 (2013.01); B64C 27/08 (2013.01); B64C 27/20 (2013.01); B64C 27/28 (2013.01); B64C 29/00 (2013.01); B64C 29/0033 (2013.01); B64C 2201/024 (2013.01); B64C 2201/108 (2013.01); B64C 2201/162 (2013.01);
Abstract

A multirotor aircraft with an airframe and a thrust producing units arrangement, wherein the thrust producing units arrangement comprises a predetermined number of thrust producing units for producing thrust in a predetermined direction, and wherein a flexible suspension unit is rigidly mounted to the airframe, wherein the flexible suspension unit comprises at least one bearing that mechanically couples the thrust producing units arrangement to the airframe such that the thrust producing units of the predetermined number of thrust producing units are inclinable in relation to the airframe.


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