Hovercraft with fore and aft thrusters and winglets

Sanders, Jr. September 28, 2

Patent Grant D496606

U.S. patent number D496,606 [Application Number D/190,971] was granted by the patent office on 2004-09-28 for hovercraft with fore and aft thrusters and winglets. This patent grant is currently assigned to UFOZ, LLC. Invention is credited to John K. Sanders, Jr..


United States Patent D496,606
Sanders, Jr. September 28, 2004

Hovercraft with fore and aft thrusters and winglets

Claims

The ornamental design for the hovercraft with fore and aft thrusters and winglets, as shown and described.
Inventors: Sanders, Jr.; John K. (Costa Mesa, CA)
Assignee: UFOZ, LLC (Oahu, HI)
Appl. No.: D/190,971
Filed: September 29, 2003

Current U.S. Class: D12/5
Current International Class: 1214
Field of Search: ;D12/5,2-4,324-330 ;180/116-117,120,126 ;244/23A,23C,17.23

References Cited [Referenced By]

U.S. Patent Documents
D183816 October 1958 Simmons
D187625 April 1960 Postelson
2955780 October 1960 Hulbert
2968453 January 1961 Bright
3039550 June 1962 Beardsley
3066753 December 1962 Hurley et al.
3209848 October 1965 Holloway
D216842 March 1970 Bertelsen
3507462 April 1970 Stefan
3556438 January 1971 Meditz
3656575 April 1972 Vryland
3827527 August 1974 Bertelsen
D243837 March 1977 Adams
4043421 August 1977 Smith
D292194 October 1987 Moller
4828058 May 1989 Bjorn-Ake
4880071 November 1989 Tracy
D473161 April 2003 Inkster
Primary Examiner: Holtje; Nelson C.
Attorney, Agent or Firm: Chong; Leighton K. Ostrager Chong & Flaherty (Hawaii)

Description



FIG. 1 is a plan view of my new design for a hovercraft with fore and aft thrusters and winglets;

FIG. 2 is a right side elevation view of the hovercraft design shown in FIG. 1;

FIG. 3 is a bottom view of the hovercraft design shown in FIG. 1;

FIG. 4 is a rear view of the hovercraft design shown in FIG. 1;

FIG. 5 is a front view of the hovercraft design shown in FIG. 1;

FIG. 6 is a bottom perspective view of the hovercraft design shown in FIG. 1; and,

FIG. 7 is a top perspective view of the hovercraft design shown in FIG. 1.

* * * * *


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