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. 25, 2015

Filed:

Jul. 30, 2013
Applicant:

Aurora Flight Sciences Corporation, Manassas, VA (US);

Inventors:

Adam John Woodworth, Melrose, MA (US);

James Peverill, Canton, MA (US);

Greg Vulikh, Manassas, VA (US);

Jeremy Scott Hollman, Manassas, VA (US);

Assignee:
Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64D 27/00 (2006.01); B64C 1/30 (2006.01); B64D 27/26 (2006.01); B64D 9/00 (2006.01); B64C 19/00 (2006.01); B64D 1/14 (2006.01); B64C 15/00 (2006.01); B64C 39/02 (2006.01); A63H 27/00 (2006.01);
U.S. Cl.
CPC ...
B64C 1/30 (2013.01); A63H 27/001 (2013.01); A63H 27/02 (2013.01); B64C 15/00 (2013.01); B64C 19/00 (2013.01); B64C 39/028 (2013.01); B64D 1/14 (2013.01); B64D 9/00 (2013.01); B64D 27/26 (2013.01); B64C 2201/028 (2013.01); B64C 2201/042 (2013.01); B64C 2201/104 (2013.01); B64C 2201/127 (2013.01); B64C 2201/165 (2013.01); B64C 2201/18 (2013.01); B64C 2201/187 (2013.01); B64C 2201/201 (2013.01);
Abstract

An aircraft for unmanned aviation is described. The aircraft includes an airframe, a pair of fins attached to a rear portion of the airframe, a pair of dihedral braces attached to a bottom portion of the airframe, a first thrust-vectoring ('T/V') module and a second T/V module, and an electronics module. The electronics module provides commands to the two T/V modules. The two T/V modules are configured to provide lateral and longitudinal control to the aircraft by directly controlling a thrust vector for each of the pitch, the roll, and the yaw of the aircraft. The use of directly articulated electrical motors as T/V modules enables the aircraft to execute tight-radius turns over a wide range of airspeeds.


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