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:
Sep. 25, 2018

Filed:

Oct. 09, 2015
Applicant:

Aerovironment, Inc., Monrovia, CA (US);

Inventors:

Thomas Szarek, Simi Valley, CA (US);

Thomas Omer, Moorpark, CA (US);

Manolis Pavlos Dimotakis, Altedena, CA (US);

Jefferson C. McBride, Simi Valley, CA (US);

Assignee:

AEROVIRONMENT, INC., Monrovia, CA (US);

Attorneys:
Primary Examiner:
Int. Cl.
CPC ...
B64D 47/08 (2006.01); F16M 11/12 (2006.01); F16M 11/18 (2006.01); B64C 39/02 (2006.01); H04N 7/18 (2006.01);
U.S. Cl.
CPC ...
B64D 47/08 (2013.01); B64C 39/024 (2013.01); F16M 11/123 (2013.01); F16M 11/126 (2013.01); F16M 11/18 (2013.01); H04N 7/183 (2013.01); B64C 2201/021 (2013.01); B64C 2201/123 (2013.01); B64C 2201/127 (2013.01);
Abstract

A turret assembly for attachment on the undersurface of an aircraft that reduces performance limitations due to gimbal lock and reduces the cross section profile of the assembly. The assembly includes a roll actuator including a drive shaft. A yoke having a cross member is coupled to the drive shaft and a pair of prongs. The yoke is rotated via the roll actuator and drive shaft along a roll axis oriented substantially parallel to the body of the aircraft. A turret is mounted on the prongs of the yoke. A tilt actuator is contained within the turret. The tilt actuator tilts the turret on a tilt axis relative to the yoke. The tilt axis is perpendicular to the roll axis.


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