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:
Dec. 21, 2021

Filed:

Oct. 18, 2019
Applicant:

The Boeing Company, Chicago, IL (US);

Inventors:

Tyler Emerson Berkey, Charleston, SC (US);

Daniel S. Thomas, Summerville, SC (US);

Assignee:

The Boeing Company, Chicago, IL (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64D 27/24 (2006.01); B64C 29/00 (2006.01); B64C 11/00 (2006.01); B64C 39/12 (2006.01); B64C 11/06 (2006.01); B64C 3/32 (2006.01);
U.S. Cl.
CPC ...
B64D 27/24 (2013.01); B64C 11/001 (2013.01); B64C 11/06 (2013.01); B64C 29/0033 (2013.01); B64C 39/12 (2013.01); B64C 3/32 (2013.01);
Abstract

Rotary electric engines, aircraft including the same, and associated methods. A rotary electric engine includes a nacelle, a fan configured to generate thrust, a stator operatively coupled to the nacelle, and a rotor operatively coupled to the fan. The fan includes a plurality of fan blades. The rotor includes a plurality of rotor magnets operatively coupled to respective blade tips of the fan blades. The stator includes a plurality of field coils configured to produce a magnetic interaction between the field coils and the rotor magnets to rotate the fan. In examples, the stator is configured to rotate each field coil relative to the nacelle. In examples, an aircraft includes one or more rotary electric engines pivotally mounted within engine mount regions. In examples, a method of operating an aircraft includes operating one or more rotary electric engines in a vertical lift configuration and in a forward flight configuration.


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