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:
Apr. 07, 2026

Filed:

Apr. 11, 2024
Applicant:

Airbus Helicopters Deutschland Gmbh, Donauwörth, DE;

Inventors:

Sascha Schneider, Meitingen, DE;

Daniel Reber, Gröbenzell, DE;

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64D 31/09 (2024.01); B64C 27/00 (2006.01); B64F 5/60 (2017.01);
U.S. Cl.
CPC ...
B64D 31/09 (2024.01); B64F 5/60 (2017.01); B64C 27/00 (2013.01);
Abstract

A method of operating a rotorcraft with at least one main rotor and at least two engines, comprising: determining whether the rotorcraft is operated in an AEO mode wherein the at least two engines are powering the at least one main rotor, or in a SEO mode wherein only a first engine of the at least two engines is powering the at least one main rotor while a second engine of the at least two engines is inactive; if the rotorcraft is operated in the SEO mode, monitoring the first engine to enable detection of engine failures; and if during monitoring of the first engine an engine failure of the first engine is detected, entering into autorotation of the at least one main rotor upon detection of the engine failure by adjusting main rotor actuators of the at least one main rotor.


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