Patent
   D723447
Priority
Sep 16 2010
Filed
Mar 16 2011
Issued
Mar 03 2015
Expiry
Mar 03 2029
Assg.orig
Entity
unknown
0
24
n/a
The ornamental design for a fuselage, as shown and described.

FIG. 1 is a perspective view of the fuselage, in accordance with the present invention;

FIG. 2 is a top plan view of the fuselage shown in FIG. 1;

FIG. 3 is a bottom plan view of the fuselage shown in FIG. 1;

FIG. 4 is a right side elevation view of the fuselage shown in FIG. 1, the left side being a mirror image thereof;

FIG. 5 is a front elevation view of the fuselage shown in FIG. 1; and,

FIG. 6 is a representational elevation view of FIG. 5, shown solely for the purpose of illustrating that the fuselage is composed of four degrees of radii in six segments. The angled partial broken lines indicate the point at which one radius meets another radius. These broken lines form no part of the claimed design. The broken line circle shown intersecting the fuselage is shown solely to emphasize the six radii segments, and forms no part of the claimed design.

The jagged circumferential lines wrapping around the middle portion of the fuselage in FIGS. 1-4 indicate that the appearance of any portion of the article between the break lines forms no part of the claimed design. The windows and floor of this embodiment are shown in broken line and as such form no part of the claimed invention.

Meyer, Michael, Sturm, Ralph, Trahmer, Bernd, Lesemann, Jan

Patent Priority Assignee Title
Patent Priority Assignee Title
3955781, Mar 10 1974 Supersonic aircraft with the engines disposed under the delta wing middle portion
4712751, Jul 24 1985 Messerschmitt-Boelkow-Blohm Gesellschaft mit beschraenkter Haftung Tail end structure for an aircraft fuselage
5806797, Oct 13 1992 The Boeing Company Airplane fuselage
6834833, Oct 02 2001 The Boeing Company Twin aisle small airplane
7410352, Apr 13 2005 The Boeing Company Multi-ring system for fuselage barrel formation
7721992, Mar 07 2007 The Boeing Company Aircraft floor to fuselage attachment
7735779, Nov 02 2006 The Boeing Company Optimized fuselage structure
7787979, Mar 14 2007 The Boeing Company Splicing fuselage sections without shims
7861970, Nov 02 2006 The Boeing Company Fuselage structure including an integrated fuselage stanchion
7874516, Nov 15 2004 Airbus France Structural frame for an aircraft fuselage
7896291, Apr 10 2006 Airbus Operations GmbH Aircraft door with oversizing
7967250, May 12 2008 EMBRAER S A Hybrid aircraft fuselage structural components and methods of making same
8146860, Apr 10 2006 Airbus Operations GmbH Aircraft fuselage with circular-arc-shaped exterior contour
8215582, Mar 29 2006 Airbus Operations Limited Aircraft fuselage interior
20040031881,
20080093503,
20080105785,
20080209712,
20090152399,
20100084510,
20110001006,
GB2443542,
GB560580,
WO2007120201,
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Executed onAssignorAssigneeConveyanceFrameReelDoc
Mar 16 2011Airbus Operations GmbH(assignment on the face of the patent)
Mar 16 2011STURM, RALPHAirbus Operations GmbHASSIGNMENT OF ASSIGNORS INTEREST SEE DOCUMENT FOR DETAILS 0262150074 pdf
Mar 30 2011LESEMANN, JANAirbus Operations GmbHASSIGNMENT OF ASSIGNORS INTEREST SEE DOCUMENT FOR DETAILS 0262150074 pdf
Mar 30 2011MEYER, MICHAELAirbus Operations GmbHASSIGNMENT OF ASSIGNORS INTEREST SEE DOCUMENT FOR DETAILS 0262150074 pdf
Mar 30 2011TRAHMER, BERNDAirbus Operations GmbHASSIGNMENT OF ASSIGNORS INTEREST SEE DOCUMENT FOR DETAILS 0262150074 pdf
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