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:
Sep. 10, 2024

Filed:

Jul. 16, 2021
Applicant:

Airbus Helicopters Deutschland Gmbh, Donauworth, DE;

Inventors:

Rupert Pfaller, Riemerling, DE;

Tobias Ries, Nordendorf, DE;

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64C 39/00 (2023.01); B64C 1/00 (2006.01); B64C 27/22 (2006.01);
U.S. Cl.
CPC ...
B64C 39/029 (2020.01); B64C 1/0009 (2013.01); B64C 27/22 (2013.01);
Abstract

A rotary wing aircraft that extends along an associated roll axis between a nose region and an aft region and that comprises a fuselage with a front section and a rear section, wherein the rear section extends between the front section and the aft region, the rotary wing aircraft comprising: a propeller that is rotatably mounted at the rear section in the aft region, a main rotor that is rotatably mounted at the front section, and a source of asymmetry that is connected to the front section such that the front section comprises at least in sections an asymmetrical cross-sectional profile in direction of the associated roll axis, wherein the source of asymmetry is configured to generate sideward thrust for main rotor anti-torque from main rotor downwash.


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