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:
Mar. 05, 2024

Filed:

Dec. 17, 2020
Applicant:

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

Inventors:

Riccardo Bianco Mengotti, Samarate, IT;

Carlo Cassinelli, Samarate, IT;

Alessandro Scandroglio, Samarate, IT;

Andrea Bavetta, Samarate, IT;

Paolo Brughera, Samarate, IT;

Luca Sampugnaro, Samarate, IT;

Assignee:

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

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64C 29/00 (2006.01); B64C 1/20 (2006.01); B64C 1/22 (2006.01); B64C 3/52 (2006.01); B64C 9/14 (2006.01); B64C 27/22 (2006.01); B64C 39/12 (2006.01); B64D 27/24 (2006.01); B64D 29/00 (2006.01); B64D 35/04 (2006.01); B64D 35/08 (2006.01); B64D 27/02 (2006.01);
U.S. Cl.
CPC ...
B64C 29/0033 (2013.01); B64C 1/20 (2013.01); B64C 1/22 (2013.01); B64C 3/52 (2013.01); B64C 9/14 (2013.01); B64C 27/22 (2013.01); B64C 39/12 (2013.01); B64D 27/24 (2013.01); B64D 29/00 (2013.01); B64D 35/04 (2013.01); B64D 35/08 (2013.01); B64D 2027/026 (2013.01);
Abstract

A convertiplane is described that comprises a fuselage, having a first longitudinal axis, with a nose and a tail portion; a pair of wings arranged on respective opposite sides of said fuselage, carrying respective rotors; a pair of engines operatively connected to respective said rotors; at least one first lifting surface arranged on said tail portion; and a pair of canards arranged on said nose of said fuselage and defining respective second lifting surfaces adapted to generate a third lift/negative lift value; each rotor comprising a mast rotatable about a second axis and about an relative third axis transversal to said second axis and with respect to the fuselage, so as to set said convertiplane between a helicopter configuration and an aeroplane configuration; each second axis, in use, being transversal to the first axis of said convertiplane in said helicopter configuration and being parallel to said first axis in said aeroplane configuration.


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