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.:

US 10737786 B1

PDF
Full Text
Expired
Date of Patent:
Aug. 11, 2020

Filed:

May. 12, 2017
Applicant:

Bell Helicopter Textron Inc., Fort Worth, TX (US);

Inventors:

Carlos Alexander Fenny, Fort Worth, TX (US);

Rohn Lee Olson, Hurst, TX (US);

Andrew James Zahasky, North Richland Hills, TX (US);

Assignee:

BELL HELICOPTER TEXTRON INC., Fort Worth, TX (US);

Attorneys:
Primary Examiner:
Int. Cl.
CPC ...
B64C 39/06 (2006.01); B64C 29/02 (2006.01); B64D 27/02 (2006.01); B64C 11/28 (2006.01); B64C 27/50 (2006.01); B64C 29/00 (2006.01); B64C 3/10 (2006.01); B64C 27/08 (2006.01); B64C 27/12 (2006.01); B64D 27/24 (2006.01); B64D 31/00 (2006.01); B64C 1/06 (2006.01); B64C 39/02 (2006.01); B64C 1/00 (2006.01);
U.S. Cl.
CPC ...
B64C 39/062 (2013.01); B64C 1/068 (2013.01); B64C 3/10 (2013.01); B64C 11/28 (2013.01); B64C 27/08 (2013.01); B64C 27/12 (2013.01); B64C 27/50 (2013.01); B64C 29/0025 (2013.01); B64C 29/02 (2013.01); B64C 39/024 (2013.01); B64C 39/06 (2013.01); B64D 27/24 (2013.01); B64D 31/00 (2013.01); B64C 2001/0045 (2013.01); B64D 2027/026 (2013.01);
Abstract

An aircraft includes a closed wing, a fuselage at least partially disposed within a perimeter of the closed wing, and one or more spokes coupling the closed wing to the fuselage. A plurality of hydraulic or electric motors are disposed within or attached to the closed wing, fuselage or spokes in a distributed configuration. A propeller is proximate to a leading edge of the closed wing or spokes and operably connected to each hydraulic or electric motor. A source of hydraulic or electric power is disposed within or attached to the closed wing, fuselage or spokes and coupled to each hydraulic or electric motor disposed within or attached to the closed wing, fuselage or spokes. A controller is coupled to each hydraulic or electric motor, and one or more processors communicably coupled to each controller that control an operation and speed of the plurality of hydraulic or electric motors.


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