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.
Patent No.:
Date of Patent:
Dec. 19, 2017
Filed:
Feb. 14, 2014
Applicant:
Airbus Helicopters, Marignane, FR;
Inventor:
Jean Nicola, Aix En Provence, FR;
Assignee:
AIRBUS HELICOPTERS, Marignane, FR;
Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64C 27/26 (2006.01); B64D 47/08 (2006.01); B64C 1/00 (2006.01); B64C 25/04 (2006.01); B64C 39/04 (2006.01); B64D 1/22 (2006.01); B64C 25/32 (2006.01);
U.S. Cl.
CPC ...
B64C 27/26 (2013.01); B64C 1/00 (2013.01); B64C 25/04 (2013.01); B64C 39/04 (2013.01); B64D 1/22 (2013.01); B64D 47/08 (2013.01); B64C 2025/325 (2013.01);
Abstract
A rotorcraft () having: a lift rotor (); a wing () extending from a first end () carrying a first propulsive propeller () to a second end () carrying a second propeller (); landing gear (); and a tail (). The rotorcraft () is provided with two fuselages () secured to said wing () between said first and second propulsive propellers () in such a manner as to present an inter-fuselage space () having no propeller between said fuselages (), each fuselage () including at least one undercarriage of said landing gear ().