Pair of aircraft windows

Fujino , et al. August 6, 2

Patent Grant D687366

U.S. patent number D687,366 [Application Number D/403,115] was granted by the patent office on 2013-08-06 for pair of aircraft windows. This patent grant is currently assigned to Honda Patents & Technologies North America, LLC. The grantee listed for this patent is Michimasa Fujino, Junichi Kondo, Chris Osborne. Invention is credited to Michimasa Fujino, Junichi Kondo, Chris Osborne.


United States Patent D687,366
Fujino ,   et al. August 6, 2013

Pair of aircraft windows

Claims

CLAIM The ornamental design for a pair of aircraft windows, as shown and described.
Inventors: Fujino; Michimasa (Summerfield, NC), Kondo; Junichi (Greensboro, NC), Osborne; Chris (Efland, NC)
Applicant:
Name City State Country Type

Fujino; Michimasa
Kondo; Junichi
Osborne; Chris

Summerfield
Greensboro
Efland

NC
NC
NC

US
US
US
Assignee: Honda Patents & Technologies North America, LLC (Torrance, CA)
Appl. No.: D/403,115
Filed: September 30, 2011

Current U.S. Class: D12/345
Current International Class: 1207
Field of Search: ;49/380,372 ;52/202 ;D12/345,42,183,404 ;D6/383,356,357,335,381,382,336,377,371,337,360,361 ;297/245,118,244 ;244/118.5,118.6,122R,129.3,129.4,122AH,119

References Cited [Referenced By]

U.S. Patent Documents
D363773 October 1995 Nishizawa
D455390 April 2002 Granzeier et al.
D512365 December 2005 Bladt et al.
D536436 February 2007 Nishizawa
D562779 February 2008 Lamoree et al.
D600623 September 2009 Fiedler et al.
D600624 September 2009 Fiedler et al.
D611888 March 2010 Bladt et al.
D617254 June 2010 Guard et al.
D626491 November 2010 Saint-Jalmes et al.
D631421 January 2011 Kosoniscs et al.
D654008 February 2012 Stevens
D673892 January 2013 Stephan et al.
2005/0044712 March 2005 Gideon et al.
2006/0118676 June 2006 Novak et al.
2008/0042012 February 2008 Callahan et al.
Primary Examiner: Murphy; Austin
Attorney, Agent or Firm: Plumsea Law Group, LLC

Description



FIG. 1 is a perspective view of a pair of aircraft windows showing our new design;

FIG. 2 is a top plan view thereof;

FIG. 3 is a side elevational view of one side thereof;

FIG. 4 is a side elevational view of the other side thereof;

FIG. 5 is a detailed top plan view of the portion of the fuselage showing the pair of aircraft windows;

FIG. 6 is a bottom plan view of the area shown in FIG. 5; and,

FIG. 7 is a cross sectional view shown along line 7-7 of FIG. 6.

The broken line showing of the elongated oval in FIG. 5 illustrates a hidden line. The broken line showings of the remainder of the aircraft form no part of the claimed design.

* * * * *


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