Aircraft delta fin

- ICON Aircraft, Inc.
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Description

FIG. 1 is a front perspective view of the aircraft delta fin;

FIG. 2 is a front view of the aircraft delta fin;

FIG. 3 is a back view of the aircraft delta fin;

FIG. 4 is a view of one side of the aircraft delta fin;

FIG. 5 is a view of the opposite side of the aircraft delta fin;

FIG. 6 is a top view of the aircraft delta fin; and,

FIG. 7 is a bottom view of the aircraft delta fin.

The broken lines in FIGS. 1-7 represent adjacent aircraft panel support structures and other aircraft panel components in the environment of the claimed design, but which do not form part of the claimed design.

Claims

The ornamental design for an aircraft delta fin, as shown and described.

Referenced Cited
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D358576 May 23, 1995 Sutter et al.
D396143 July 21, 1998 McLaughlin
D397989 September 8, 1998 Al-Sabah
D414740 October 5, 1999 Margaritoff
D418105 December 28, 1999 Margaritoff
D494127 August 10, 2004 Eatkins et al.
D494920 August 24, 2004 Eatkins et al.
D499688 December 14, 2004 Atkinson et al.
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D576938 September 16, 2008 Moon
D596267 July 14, 2009 Colgren et al.
Patent History
Patent number: D620876
Type: Grant
Filed: Jun 11, 2008
Date of Patent: Aug 3, 2010
Assignee: ICON Aircraft, Inc. (Los Angeles, CA)
Inventors: Diego Miralles (Altadena, CA), Steen Strand (Manhattan Beach, CA)
Primary Examiner: Cathron C. Brooks
Assistant Examiner: Maurice Stevens
Attorney: Michael C. Martensen
Application Number: 29/319,640
Classifications
Current U.S. Class: Element Or Attachment (9) (D12/345)