Unmanned aircraft vehicle

Klick April 11, 2

Patent Grant D783453

U.S. patent number D783,453 [Application Number D/548,236] was granted by the patent office on 2017-04-11 for unmanned aircraft vehicle. This patent grant is currently assigned to Ritewing RC, LLC. The grantee listed for this patent is Ritewing RC, LLC. Invention is credited to Christopher K. Klick.


United States Patent D783,453
Klick April 11, 2017

Unmanned aircraft vehicle

Claims

CLAIM The ornamental design for an unmanned aircraft vehicle, substantially as shown in the attached drawings.
Inventors: Klick; Christopher K. (Mesa, AZ)
Applicant:
Name City State Country Type

Ritewing RC, LLC

Mesa

AZ

US
Assignee: Ritewing RC, LLC (Mesa, AZ)
Appl. No.: D/548,236
Filed: December 11, 2015

Current U.S. Class: D12/16.1
Current International Class: 1207
Field of Search: ;D12/16.1,319-345 ;D21/436,441-444,446-453

References Cited [Referenced By]

U.S. Patent Documents
4033070 July 1977 Strongin
D306997 April 1990 Andrews
D325557 April 1992 Cummings
5337975 August 1994 Peinemann
D388392 December 1997 McGinnis
D530659 October 2006 Guering
D620392 July 2010 Rodriguez
D628244 November 2010 Fish
7866599 January 2011 Elvin
D649506 November 2011 Morelli
D684103 June 2013 Morelli
D707614 June 2014 Colten
D728445 May 2015 Colten
D749490 February 2016 Klick
2003/0006340 January 2003 Harrison
2006/0255208 November 2006 Hawkins
2008/0194170 August 2008 Feng
Primary Examiner: Spear; Robert M
Assistant Examiner: Cash; Marissa J
Attorney, Agent or Firm: Trenner Law Firm, LLC Trenner; Mark D.

Description



FIG. 1 is a top perspective view of a first unmanned aircraft vehicle;

FIG. 2 is a bottom perspective view of the unmanned aircraft vehicle, wherein wings are shown as these may be attached to the unmanned aircraft vehicle;

FIG. 3 is a top view of the design corresponding to FIG. 1;

FIG. 4 is a bottom view of the design corresponding to FIG. 2;

FIG. 5 is a front view of the design corresponding to FIG. 1;

FIG. 6 is a back view of the design corresponding to FIG. 1;

FIG. 7 is a right side view of the design corresponding to FIG. 1;

FIG. 8 is a left side view of the design corresponding to FIG. 1;

FIG. 9 is a top perspective view of an unmanned aircraft vehicle further including canards attached to the unmanned aircraft vehicle shown in FIG. 1; and,

FIG. 10 is a bottom perspective view of the unmanned aircraft vehicle shown in FIG. 9.

* * * * *


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