Aircraft rudder pedal

- Icon Aircraft, Inc.
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Description

FIG. 1 is a front, left perspective view of an aircraft rudder pedal showing our new design;

FIG. 2 is a front rear view thereof;

FIG. 3 is a rear view thereof;

FIG. 4 is a right side view thereof;

FIG. 5 is a left side view thereof;

FIG. 6 is a top view thereof; and,

FIG. 7 is a bottom view thereof.

Claims

The ornamental design for an aircraft rudder pedal, as shown and described.

Referenced Cited
U.S. Patent Documents
2424523 July 1947 Watter
3576302 April 1971 Palfreyman
4848708 July 18, 1989 Farrell
5878981 March 9, 1999 Dewey
D425839 May 30, 2000 Asakura
D479167 September 2, 2003 Faust
6918316 July 19, 2005 Johansson
7690604 April 6, 2010 Christensen
D626901 November 9, 2010 Fallot
8353484 January 15, 2013 Gardner
20050016319 January 27, 2005 Kiczek
20080105790 May 8, 2008 Christensen
Patent History
Patent number: D746214
Type: Grant
Filed: Jul 16, 2014
Date of Patent: Dec 29, 2015
Assignee: Icon Aircraft, Inc. (Los Angeles, CA)
Inventors: Dong Tran (Los Angeles, CA), Klaus Tritschler (Los Angeles, CA)
Primary Examiner: Robert M Spear
Assistant Examiner: Marissa J Cash
Application Number: 29/496,695
Classifications