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. 16, 2024

Filed:

Apr. 15, 2021
Applicant:

Airbus Helicopters Technik Gmbh, Calden, DE;

Inventors:

Jan Haar, Ahnatal, DE;

Uwe Arnold, Kassel, DE;

Martin Meunier, Kassel, DE;

Carsten Wintjen, Grebenstein, DE;

Matthias Müller, Kassel, DE;

Werner Pflüger, Ahnatal, DE;

Assignee:
Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64C 27/68 (2006.01); B64C 27/04 (2006.01);
U.S. Cl.
CPC ...
B64C 27/68 (2013.01); B64C 27/04 (2013.01);
Abstract

An actuator for aviation applications, in particular for adjusting rotor blades in a helicopter, may include an electromechanical drive assembly connected to an output drive via a downstream transmission, where the drive assembly is divided into sub-drives that can be operated independently, and where at least two sub-drives are spatially separated from one another in that the transmission is placed between these sub-drives. The transmission may include at least two harmonic gearings coupled to one another by at least one first coupling element, where a first harmonic gearing is located inside a non-rotating first housing, where a second harmonic gearing is located inside a rotating second housing, and where the second housing is connected to the output drive.


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