Aircraft delta fin

Miralles , et al. August 3, 2

Patent Grant D620876

U.S. patent number D620,876 [Application Number D/319,640] was granted by the patent office on 2010-08-03 for aircraft delta fin. This patent grant is currently assigned to ICON Aircraft, Inc.. Invention is credited to Diego Miralles, Steen Strand.


United States Patent D620,876
Miralles ,   et al. August 3, 2010

Aircraft delta fin

Claims

CLAIM The ornamental design for an aircraft delta fin, as shown and described.
Inventors: Miralles; Diego (Altadena, CA), Strand; Steen (Manhattan Beach, CA)
Assignee: ICON Aircraft, Inc. (Los Angeles, CA)
Appl. No.: D/319,640
Filed: June 11, 2008

Current U.S. Class: D12/345
Current International Class: 1207
Field of Search: ;D12/319-345 ;D21/447,448 ;244/4R,5,6,7R,7B,7C,13,15,21,36,117R,119,129.1,130,211-213,215

References Cited [Referenced By]

U.S. Patent Documents
D183657 October 1958 Johnson et al.
3188022 June 1965 Ornberg
3738595 June 1973 Bouchnik
3900178 August 1975 Tupolev et al.
D248745 August 1978 Jager
4365774 December 1982 Coronel
5062595 November 1991 Maxworthy
D358576 May 1995 Sutter et al.
D396143 July 1998 McLaughlin
D397989 September 1998 Al-Sabah
D414740 October 1999 Margaritoff
D418105 December 1999 Margaritoff
D494127 August 2004 Eatkins et al.
D494920 August 2004 Eatkins et al.
D499688 December 2004 Atkinson et al.
D500730 January 2005 Bye et al.
D504862 May 2005 Seidel
D576938 September 2008 Moon
D596267 July 2009 Colgren et al.
Primary Examiner: Brooks; Cathron C.
Assistant Examiner: Stevens; Maurice
Attorney, Agent or Firm: Martensen; Michael C.

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.

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