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:
Oct. 06, 2020

Filed:

Apr. 07, 2017
Applicant:

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

Inventors:

Matteo Redaelli, Samarate, IT;

Luca Riviello, Samarate, IT;

Attilio Colombo, Samarate, IT;

Lorenzo Trainelli, Milan, IT;

Emanuele Zappa, Mandello L., IT;

Alberto Rolando, Milan, IT;

Potito Cordisco, Calolziocorte, IT;

Edoardo Vigoni, Lecco, IT;

Mauro Terraneo, Calolziocorte, IT;

Riccardo Grassetti, Cassina de'Pecchi, IT;

Assignee:

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

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
G01B 11/02 (2006.01); G01B 11/26 (2006.01); H04N 5/225 (2006.01); B64C 27/00 (2006.01); B64C 27/48 (2006.01); B64C 27/78 (2006.01); B64F 5/60 (2017.01); B64C 27/54 (2006.01);
U.S. Cl.
CPC ...
B64C 27/008 (2013.01); B64C 27/48 (2013.01); B64C 27/54 (2013.01); B64C 27/78 (2013.01); B64F 5/60 (2017.01); G01B 11/026 (2013.01); G01B 11/26 (2013.01);
Abstract

A rotor for a hover-capable aircraft is described that comprises: a drive mast; a hub operatively connected to the drive mast and rotatable about a first axis; and at least two blades hinged to the hub, via a rigid or elastically deformable connection, so as to be able to assume an attitude rotated about and/or translated along at least a second axis with respect to said hub; the aircraft further comprising sensor means configured to detect the attitude of at least one said blade with respect to the hub; the sensor means are configured to acquire an optical image associated with the attitude of the blade with respect to the hub.


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