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:
Aug. 30, 2022

Filed:

Mar. 20, 2019
Applicant:

The Boeing Company, Chicago, IL (US);

Inventors:

Roger D. Bernhardt, O'Fallon, MO (US);

Dan J. Clingman, Milton, WA (US);

Assignee:

The Boeing Company, Chicago, IL (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64C 29/00 (2006.01); B64C 15/02 (2006.01); B64C 29/04 (2006.01); B64C 39/02 (2006.01); F04D 13/06 (2006.01); F04D 13/12 (2006.01); F04D 15/00 (2006.01); B64D 27/18 (2006.01);
U.S. Cl.
CPC ...
B64C 15/02 (2013.01); B64C 29/0091 (2013.01); B64C 29/04 (2013.01); B64C 39/024 (2013.01); B64D 27/18 (2013.01); F04D 13/06 (2013.01); F04D 13/12 (2013.01); F04D 15/00 (2013.01); B64C 2201/104 (2013.01); B64C 2201/108 (2013.01);
Abstract

A ducted-fan unmanned aerial vehicle (UAV) capable of low-energy high-rate maneuvers for both vertical roll control and horizontal pitch control. The UAV includes ducted fans which are with respective piezoelectric-actuated thrust vectoring flaps. Thrust vector control is achieved by controlling the angular positions of a plurality of thrust vector flaps pivotably coupled at respective outlets of a plurality of ducts having fan rotors at the inlets. Each thrust vectoring flap has only one degree of freedom in the frame of reference of the UAV, namely, rotation about a single axis that is perpendicular to the axis of the duct. The angular position of the flap is controlled by sending electrical signals to a piezoelectric actuator (e.g., a piezoelectric bimorph actuator) having a voltage sufficient to cause the piezoelectric actuator to bend.


Find Patent Forward Citations

Loading…