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:
Jun. 08, 2021

Filed:

Jul. 13, 2018
Applicant:

The Boeing Company, Chicago, IL (US);

Inventors:

Roger W. Lacy, West Chester, PA (US);

Michael J. Duffy, Lansing, NY (US);

David H. Mason, Glenmoore, PA (US);

Assignee:

The Boeing Company, Chicago, IL (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64C 27/52 (2006.01); B64C 27/10 (2006.01); G05D 1/08 (2006.01); B64C 39/02 (2006.01); B64C 27/82 (2006.01);
U.S. Cl.
CPC ...
B64C 27/52 (2013.01); B64C 27/10 (2013.01); G05D 1/0808 (2013.01); B64C 39/024 (2013.01); B64C 2027/8227 (2013.01); B64C 2201/024 (2013.01); B64C 2201/108 (2013.01);
Abstract

A rotorcraft has a frame and a plurality of rotors connected to the frame. The frame has a roll axis and a pitch axis. Each of the rotors includes a rotor shaft. The rotor shaft of each of the rotors is canted with respect to at least one of the roll axis and the pitch axis. The rotor shaft of each of the rotors may be canted between 3 and 15 degrees. Each of the rotors may be a co-axial co-rotating rotor. The rotors may be oriented in opposing pairs across the frame. Both rotors in each opposing pair rotate in the same direction. The rotorcraft may include at least two additional rotors, each having a forward cant. Each of the additional rotors may be a co-axial contra-rotating rotor.


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