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:
Nov. 25, 2025

Filed:

Nov. 15, 2023
Applicant:

Airbus Helicopters, Marignane, FR;

Inventor:

Nayibe Gomez, Aix En Provence, FR;

Assignee:

AIRBUS HELICOPTERS, Marignane, FR;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64D 35/025 (2025.01); B64C 27/04 (2006.01); B64D 27/02 (2006.01); B64D 27/10 (2006.01); B64D 27/24 (2024.01); B64D 27/32 (2024.01); B64D 27/33 (2024.01); B64D 27/34 (2024.01); B64D 31/00 (2024.01); B64D 31/06 (2024.01); B64D 31/18 (2024.01); F01N 1/00 (2006.01); F02D 35/00 (2006.01);
U.S. Cl.
CPC ...
B64D 35/025 (2024.01); B64C 27/04 (2013.01); B64D 27/02 (2013.01); B64D 27/10 (2013.01); B64D 27/24 (2013.01); B64D 27/32 (2024.01); B64D 27/33 (2024.01); B64D 27/34 (2024.01); B64D 31/00 (2013.01); B64D 31/06 (2013.01); B64D 31/18 (2024.01); F01N 1/00 (2013.01); F02D 35/0007 (2013.01); B64D 27/026 (2024.01); F05D 2270/333 (2013.01);
Abstract

A method of optimizing the noise generated by a hybrid power plant of a rotorcraft in flight, the hybrid power plant driving a main rotor of the rotorcraft in rotation and being provided with at least one engine, with at least one electric machine, and with at least one electrical energy source that electrically powers the electric machine. The method includes a determination step for determining a required power delivered by the hybrid power plant and that is required for the flight phase, and a distribution step for distributing the required power between the at least one engine and the electric machine as a function of a target noise level and of the required power for the flight phase, as well as of a model for the noise generated by the at least one engine as a function of one of its parameters.


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