Collective control post and grip for a rotorcraft

Yates , et al. November 26, 2

Patent Grant D694168

U.S. patent number D694,168 [Application Number D/413,127] was granted by the patent office on 2013-11-26 for collective control post and grip for a rotorcraft. This patent grant is currently assigned to Bell Helicopter Textron Inc.. The grantee listed for this patent is Bradley Don Linton, Travis Lee Yates. Invention is credited to Bradley Don Linton, Travis Lee Yates.


United States Patent D694,168
Yates ,   et al. November 26, 2013

Collective control post and grip for a rotorcraft

Claims

CLAIM The ornamental design for a collective control post and grip for a rotorcraft, as shown and described.
Inventors: Yates; Travis Lee (Lakeside, TX), Linton; Bradley Don (Mansfield, TX)
Applicant:
Name City State Country Type

Yates; Travis Lee
Linton; Bradley Don

Lakeside
Mansfield

TX
TX

US
US
Assignee: Bell Helicopter Textron Inc. (Fort Worth, TX)
Appl. No.: D/413,127
Filed: February 10, 2012

Current U.S. Class: D12/345
Current International Class: 1207
Field of Search: ;D12/319,326-329,331,334,337-339,344,345,400,415,423-425,192,421 ;D14/405,412-416 ;D21/324,333,477,566,430,436-453 ;273/148B ;244/2,5,6,7C,7R,7A,8,12.1,12.3,12.4,12.2,17.11,17.19,17.23,17.25,17.27,60,99.1,117R,118.5,119,221,223,229,234 ;74/471XY,491 ;318/574,585 ;345/156,161 ;463/36-38 ;296/37.8 ;D15/28

References Cited [Referenced By]

U.S. Patent Documents
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4130259 December 1978 Carlson et al.
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4895040 January 1990 Soederberg
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5456428 October 1995 Hegg
5769363 June 1998 Griswold et al.
5900710 May 1999 Gautier et al.
6254037 July 2001 Fenny et al.
D462685 September 2002 Yamamoto et al.
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6682116 January 2004 Okumura
D516096 February 2006 Bergman et al.
D581861 December 2008 Anttila et al.
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D613232 April 2010 Guering
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2009/0139360 June 2009 Diccion
2009/0230252 September 2009 Daunois et al.
Primary Examiner: Veynar; Caron D
Assistant Examiner: Holtje; Martie K
Attorney, Agent or Firm: Baker Botts L.L.P.

Description



FIG. 1 is a left front perspective view of a collective control post and grip for a rotorcraft showing our new design;

FIG. 2 is a front elevational view thereof;

FIG. 3 is a rear elevational view thereof;

FIG. 4 is a right side elevational view thereof;

FIG. 5 is a left side elevational view thereof; and,

FIG. 6 is a top plan view thereof.

The broken line rectangle in FIG. 3 has been included for the purpose of establishing a boundary between claimed and unclaimed structure, the area within which forming no part of the claimed design.

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