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:
May. 22, 2018

Filed:

May. 10, 2016
Applicant:

Northrop Grumman Systems Corporation, Falls Church, VA (US);

Inventors:

Stephen D. Johnson, Laguna Niguel, CA (US);

Barnaby S. Wainfan, Long Beach, CA (US);

Assignee:

Northrop Grumman Systems Corporation, Falls Church, VA (US);

Attorneys:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64C 39/02 (2006.01); B64C 3/00 (2006.01); B64C 7/02 (2006.01); B64C 11/00 (2006.01);
U.S. Cl.
CPC ...
B64C 39/024 (2013.01); B64C 3/00 (2013.01); B64C 7/02 (2013.01); B64C 11/001 (2013.01); B64C 2201/104 (2013.01);
Abstract

A ducted fan UAV that can be collapsed into a stowed configuration and then deployed for flight by, for example, inflating the duct to a deployed configuration. The UAV includes a plurality of rotor blades, a plurality of struts and a plurality of control vanes each being pivotally mounted to a center body by a hinge so that the rotor blades, the struts and the control vanes can be folded into the stowed configuration to be substantially parallel to the center body and be unfolded into the deployed configuration to be substantially perpendicular to the center body. The UAV also includes a pressurization system providing a pressurant to a chamber within the duct so as to inflate the duct and cause the struts, the rotor blades and the control vanes to move from the stowed configuration to the deployed configuration.


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