Patent
   D693287
Priority
Feb 10 2012
Filed
Feb 10 2012
Issued
Nov 12 2013
Expiry
Nov 12 2027
Assg.orig
Entity
unknown
0
19
n/a
The ornamental design for a helicopter pedals, as shown and described.

FIG. 1 is a top, right front perspective view of the helicopter pedals showing our new design;

FIG. 2 is a front elevational view thereof;

FIG. 3 is a right side elevational view thereof;

FIG. 4 is a rear elevational view thereof;

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

FIG. 6 is a bottom plan view thereof.

The broken line showing of structural elements is included for the purpose of illustrating portions of the helicopter pedals that form no part of the claimed design.

Yates, Travis Lee, Linton, Bradley Don

Patent Priority Assignee Title
Patent Priority Assignee Title
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4961548, Dec 21 1988 Rockwell International Corporation Translating center control system
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5121889, May 06 1991 Grumman Aerospace Corporation Electronic foot controls
5878981, Apr 14 1997 Flight console for radio controlled aircraft
7644893, Feb 15 2006 Sikorsky Aircraft Corporation Full authority fly-by-wire pedal system
7690604, Nov 06 2006 Honeywell International, Inc Rudder pedal assembly including non-parallel slide rails
7806372, Feb 15 2006 Sikorsky Aircraft Corporation Full authority fly-by-wire pedal system
7874526, Feb 15 2006 Sikorsky Aircraft Corporation Full authority fly-by-wire pedal system
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D479167, May 21 2002 LOGITECH EUROPE S A Pedals with floor lock
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Executed onAssignorAssigneeConveyanceFrameReelDoc
Nov 07 2011YATES, TRAVIS LEEBELL HELICOPTER TEXTRON INC ASSIGNMENT OF ASSIGNORS INTEREST SEE DOCUMENT FOR DETAILS 0280060364 pdf
Feb 10 2012Bell Helicopter Textron Inc.(assignment on the face of the patent)
Mar 01 2012LINTON, BRADLEY DONBELL HELICOPTER TEXTRON INC ASSIGNMENT OF ASSIGNORS INTEREST SEE DOCUMENT FOR DETAILS 0280060364 pdf
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