Fuselage for a quad-rotor convertible aircraft
Colten , et al. June 24, 2
U.S. patent number D707,614 [Application Number D/462,516] was granted by the patent office on 2014-06-24 for fuselage for a quad-rotor convertible aircraft. This patent grant is currently assigned to Rosemount Aerospace Inc.. The grantee listed for this patent is Rosemount Aerospace Inc.. Invention is credited to Todd Michael Colten, Christopher Scott Gibson.
| United States Patent | D707,614 |
| Colten , et al. | June 24, 2014 |
Fuselage for a quad-rotor convertible aircraft
Claims
CLAIM The ornamental design for a fuselage for a quad-rotor convertible aircraft, as shown and described.
| Inventors: | Colten; Todd Michael (St. Paul, MN), Gibson; Christopher Scott (Waxhaw, NC) | ||||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|
| Applicant: |
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| Assignee: | Rosemount Aerospace Inc.
(Burnsville, MN) |
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| Appl. No.: | D/462,516 | ||||||||||
| Filed: | August 5, 2013 |
| Current U.S. Class: | D12/319; D12/345; D21/447; D21/450 |
| Current International Class: | 1207 |
| Field of Search: | ;D12/16.1,319,320,325,326,327,328,329,337,344,345 ;D21/430,436,437,441,442,443,444,447,450,451,453 ;D10/119.4 ;244/5,6,7R,7A,12.1,12.2,12.5,17.11,17.13,17.17,17.23,17.25,17.27,23C,23R,53R,63,117R,119,123.1 ;446/36,37,46-48,230,231,232,233,236 ;280/1.12,1.21 ;701/14,15,16 |
References Cited [Referenced By]
U.S. Patent Documents
| D141292 | May 1945 | Poyer |
| D159071 | June 1950 | Jones |
| D202454 | September 1965 | Smith |
| 3410506 | November 1968 | Hayes |
| 4213586 | July 1980 | Sengstock et al. |
| 4261533 | April 1981 | Roberts et al. |
| D453317 | February 2002 | DeTore et al. |
| D466858 | December 2002 | Carroll et al. |
| D530659 | October 2006 | Guering |
| D628528 | December 2010 | Cabezas Carrasco |
| D648808 | November 2011 | Seydoux et al. |
| 2007/0029439 | February 2007 | Merems et al. |
| 2009/0008497 | January 2009 | Corsiglia et al. |
Assistant Examiner: Holtje; Martie K
Attorney, Agent or Firm: Edwards Wildman Palmer LLP Wiley; Scott D. Jones; Joshua L.
Description
FIG. 1 is a top right front perspective view of a fuselage for a quad-rotor convertible aircraft showing our new design;
FIG. 2 is a top plan view thereof;
FIG. 3 is a bottom plan view thereof;
FIG. 4 is a front elevational view thereof;
FIG. 5 is a rear elevational view thereof;
FIG. 6 is a right side elevational view thereof; and,
FIG. 7 is a left side elevational view thereof.
The structural features depicted by broken lines have been shown for the purpose of illustrating portions of the fuselage for a quad-rotor convertible Aircraft that form no part of the claimed design.
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