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. 16, 2021

Filed:

Dec. 29, 2017
Applicant:

Leonardo S.p.a., Rome, IT;

Inventor:

Massimo Brunetti, Samarate, IT;

Assignee:

LEONARDO S.P.A., Rome, IT;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64C 27/12 (2006.01); B64C 27/68 (2006.01); H02K 16/02 (2006.01);
U.S. Cl.
CPC ...
B64C 27/12 (2013.01); B64C 27/68 (2013.01); H02K 16/02 (2013.01); B64C 2201/042 (2013.01);
Abstract

There is disclosed a rotor for an aircraft capable of hovering, comprising: a stator; a rotatable element, which is rotatable about an axis with respect to stator; a blade, which is connected with element; a support element, which supports a source of a magnetic field and is either stationary or driven in rotation at a first rotational speed; and a first electric circuit, which is angularly integral with element and can be driven in rotation at a second rotational speed different from first rotational speed; first electric circuit being electromagnetically coupled with source so that an electromotive force is magnetically induced in first electric circuit and an first electric current flows in first electric circuit; rotor further comprises a second electric circuit which is either stationary or driven in rotation at a first rotational speed, and a sensor generating a signal associated to a back electromotive force induced on second electric circuit.


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