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. 04, 2018

Filed:

Aug. 22, 2016
Applicant:

Harris Corporation, Melbourne, FL (US);

Inventors:

William R. Palmer, Melbourne, FL (US);

Daniel L. Schlig, Melbourne, FL (US);

Timothy F. McLellan, Viera, FL (US);

Assignee:

Harris Corporation, Melbourne, FL (US);

Attorneys:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64C 37/02 (2006.01); B64C 39/02 (2006.01); F03D 9/32 (2016.01); B64B 1/12 (2006.01); B64B 1/20 (2006.01); F03D 1/04 (2006.01); F03D 9/00 (2016.01); B64B 1/06 (2006.01); B64B 1/50 (2006.01); B64B 1/58 (2006.01); B64B 1/62 (2006.01); F03B 17/06 (2006.01); F03D 13/20 (2016.01); B63B 35/00 (2006.01); B63G 8/00 (2006.01); B64C 9/00 (2006.01); F03D 5/00 (2006.01);
U.S. Cl.
CPC ...
B64C 39/022 (2013.01); B64B 1/06 (2013.01); B64B 1/12 (2013.01); B64B 1/20 (2013.01); B64B 1/50 (2013.01); B64B 1/58 (2013.01); B64B 1/62 (2013.01); B64C 39/024 (2013.01); F03B 17/06 (2013.01); F03D 1/04 (2013.01); F03D 9/002 (2013.01); F03D 9/32 (2016.05); F03D 13/20 (2016.05); B63B 2035/006 (2013.01); B63G 2008/002 (2013.01); B64C 2009/005 (2013.01); B64C 2201/148 (2013.01); F03D 5/00 (2013.01); F05B 2220/706 (2013.01); F05B 2240/123 (2013.01); F05B 2240/21 (2013.01); F05B 2240/921 (2013.01); F05B 2240/922 (2013.01); F05B 2270/18 (2013.01);
Abstract

Tethered unmanned aerial vehicle (TUAV) includes at least one wing fixed to a fuselage. The wing is comprised of an airfoil shaped body capable of producing lift in response to a flow of air across a major wing surface, and can include at least one flight control surface, such as an aileron. One or more buoyancy cell is disposed within the fuselage for containing a lighter than air gas to provide positive buoyancy for the TUAV when the TUAV is disposed in air. A tether attachment structure facilitates attachment of the TUAV to a tether which is secured to an attachment point for securing the TUAV to the ground when aloft. A wind-powered generator is integrated with the TUAV and configured to generate electric power in response to the flow of air across the least one wing when the TUAV is aloft.


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