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Patent
D746214
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Priority
Jul 16 2014
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Filed
Jul 16 2014
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Issued
Dec 29 2015
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Expiry
Dec 29 2029
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Assg.orig
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Entity
unknown
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1
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12
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n/a
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The ornamental design for an aircraft rudder pedal, as shown and described.
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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.
Tritschler, Klaus, Tran, Dong
Patent |
Priority |
Assignee |
Title |
2424523, |
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3576302, |
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|
4848708, |
Nov 13 1987 |
The Boeing Company |
Adjustable assembly for aircraft rudder, brake and nose landing gear steering control |
5878981, |
Apr 14 1997 |
|
Flight console for radio controlled aircraft |
6918316, |
Nov 24 1997 |
DRIVESOL WORLDWIDE AB |
Adjustable pedal assembly |
7690604, |
Nov 06 2006 |
Honeywell International, Inc |
Rudder pedal assembly including non-parallel slide rails |
8353484, |
Nov 10 2009 |
CESSNA AIRCRAFT RHODE ISLAND INC ; Textron Innovations Inc |
Cockpit rudder control mechanism for an aircraft |
20050016319, |
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|
|
20080105790, |
|
|
|
D425839, |
Sep 02 1999 |
Napolex Corporation |
Pedal for automobiles |
D479167, |
May 21 2002 |
LOGITECH EUROPE S A |
Pedals with floor lock |
D626901, |
Feb 09 2010 |
Ernie Green Industries, Inc. |
Accelerator pedal |
Date |
Maintenance Fee Events |
n/a
Date |
Maintenance Schedule |
n/a