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. 15, 2016

Filed:

May. 30, 2014
Applicant:

Airbus Helicopters, Marignane, FR;

Inventor:

Pierre Prud'Homme-Lacroix, Vitrolles, FR;

Assignee:

Airbus Helicopters, Marignane, FR;

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64C 27/26 (2006.01); B64D 31/00 (2006.01); B64C 27/82 (2006.01); B64C 27/22 (2006.01); B64D 27/02 (2006.01); B64D 27/22 (2006.01);
U.S. Cl.
CPC ...
B64D 31/00 (2013.01); B64C 27/22 (2013.01); B64C 27/26 (2013.01); B64C 27/82 (2013.01); B64D 27/02 (2013.01); B64D 27/22 (2013.01);
Abstract

A hybrid aircraft () having a fuselage () extending longitudinally along an anteroposterior plane of symmetry (PSYM) from the rear () of the aircraft () towards the front () of the aircraft (). The aircraft () has a rotary wing () carried by the fuselage () of a lift surface () fastened to the fuselage () and constituted by a first half-wing () and a second half-wing (). The aircraft () has a first propulsion unit () carried by the first half-wing () and a second propulsion unit () carried by the second half-wing (). Each propulsion unit () includes at least one tractor propeller (), and at least one propulsion unit has two propellers (--) on the same axis, each of said propellers rotating about an axis of rotation (AX) that is offset transversely from said anteroposterior plane of symmetry (PSYM).


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