Patent
   D764384
Priority
Jul 15 2014
Filed
Jul 15 2014
Issued
Aug 23 2016
Expiry
Aug 23 2030
Assg.orig
Entity
unknown
0
9
n/a
The ornamental design for an aircraft delta fin, as shown and described.

FIG. 1 is a rear, top perspective drawing of an aircraft delta fin showing our new design and its environment.

FIG. 2 is a detailed rear, top perspective view thereof;

FIG. 3 is a right side perspective view thereof;

FIG. 4 is a left side perspective view thereof;

FIG. 5 is a back plan view thereof; and,

FIG. 6 is a bottom plan view of thereof.

The portions of the drawings shown in broken lines indicate surrounding structure and environment that forms no part of the claimed design.

Tritschler, Klaus, Tran, Dong

Patent Priority Assignee Title
Patent Priority Assignee Title
2960286,
3738595,
4291853, Dec 26 1978 The Boeing Company Airplane all-moving airfoil with moment reducing apex
6202959, Aug 05 1998 Airbus Operations Limited Aircraft fin and rudder
7070144, Jan 03 2003 Orbital Research Inc. Aircraft and missile afterbody flow control device and method of controlling flow
20040056150,
20120091266,
D620876, Jun 11 2008 ICON AIRCRAFT, INC Aircraft delta fin
D739807, Jul 15 2013 ICON AIRCRAFT, INC Amphibious sport aircraft
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Executed onAssignorAssigneeConveyanceFrameReelDoc
Jul 15 2014Icon Aircraft, Inc.(assignment on the face of the patent)
Aug 06 2014TRAN, DONGICON AIRCRAFT, INC ASSIGNMENT OF ASSIGNORS INTEREST SEE DOCUMENT FOR DETAILS 0335060129 pdf
Aug 06 2014TRITSCHLER, KLAUSICON AIRCRAFT, INC ASSIGNMENT OF ASSIGNORS INTEREST SEE DOCUMENT FOR DETAILS 0335060129 pdf
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