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. 03, 2019

Filed:

Oct. 05, 2017
Applicant:

Aai Corporation, Hunt Valley, MD (US);

Inventors:

Graham Schill, Upperco, MD (US);

Sean Marshall Baity, Westminster, MD (US);

Kyle W. McCool, Baltimore, MD (US);

Leonard T. Katilas, Baltimore, MD (US);

Assignee:

AAI Corporation, Hunt Valley, MD (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64F 1/22 (2006.01); B64C 39/02 (2006.01); B64F 1/10 (2006.01);
U.S. Cl.
CPC ...
B64F 1/22 (2013.01); B64C 39/024 (2013.01); B64F 1/10 (2013.01); B64C 2201/027 (2013.01); B64C 2201/088 (2013.01); B64C 2201/104 (2013.01); B64C 2201/108 (2013.01); B64C 2201/165 (2013.01); B64C 2201/18 (2013.01); B64C 2201/208 (2013.01);
Abstract

An articulated support includes a base and pitch-roll-yaw assembly having a pitch/roll subassembly and a yaw subassembly. The pitch/roll subassembly includes a central member configured for spring-loaded rotation about a pitch/roll axis, and the yaw subassembly has a U-shaped member configured (a) at end portions to engage under-wing connection lugs of an unmanned aircraft system (UAS) and (b) at a central portion to mate to the central member of the pitch/roll subassembly in a rotatable manner providing for rotation of the yaw subassembly about a yaw axis. The pitch/roll subassembly and yaw subassembly are further co-configured to define first and second fixed yaw positions in which a fuselage of the UAS is, respectively, parallel to and perpendicular to the pitch/roll axis, permitting roll motion and pitch motion of the UAS when mounted on the articulated support.


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