Tiltrotor aircraft with forward-swept wings

Robertson , et al. September 22, 2

Patent Grant D739335

U.S. patent number D739,335 [Application Number D/470,694] was granted by the patent office on 2015-09-22 for tiltrotor aircraft with forward-swept wings. This patent grant is currently assigned to Bell Helicopter Textron Inc.. The grantee listed for this patent is Bell Helicopter Textron Inc.. Invention is credited to Berlin Benfield, Kirk Groninga, Cory Hitte, Daniel Robertson.


United States Patent D739,335
Robertson ,   et al. September 22, 2015

Tiltrotor aircraft with forward-swept wings

Claims

CLAIM The ornamental design for a tiltrotor aircraft with forward-swept wings, as shown and described.
Inventors: Robertson; Daniel (Southlake, TX), Benfield; Berlin (Grapevine, TX), Hitte; Cory (Fort Worth, TX), Groninga; Kirk (Keller, TX)
Applicant:
Name City State Country Type

Bell Helicopter Textron Inc.

Fort Worth

TX

US
Assignee: Bell Helicopter Textron Inc. (Fort Worth, TX)
Appl. No.: D/470,694
Filed: October 24, 2013

Current U.S. Class: D12/345
Current International Class: 1207
Field of Search: ;D12/16.1,319-345 ;D21/441,442,447,450,453

References Cited [Referenced By]

U.S. Patent Documents
3035789 May 1962 Young
D226826 May 1973 Wernicke
D311719 October 1990 Haga
5054716 October 1991 Wilson
D323315 January 1992 Haga
5096140 March 1992 Dornier et al.
D332079 December 1992 Haga et al.
5352090 October 1994 Churchill et al.
5381985 January 1995 Wechsler et al.
5405105 April 1995 Kress
D394422 May 1998 Magee
D401898 December 1998 Lauder et al.
6260793 July 2001 Balayn et al.
6328256 December 2001 Ryan et al.
2008/0308682 December 2008 Builta et al.
2012/0043412 February 2012 Brunken
Primary Examiner: Holtje; Martie K
Attorney, Agent or Firm: Bell Helicopter Textron Inc.

Description



FIG. 1 is a front perspective view of a tiltrotor aircraft with forward-swept wings with the rotor nacelles facing upward;

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;

FIG. 6 is a top plan view thereof;

FIG. 7 is a bottom plan view thereof;

FIG. 8 is a front perspective view of a tiltrotor aircraft with forward-swept wings with the rotor nacelles facing forward;

FIG. 9 is a front elevational view of FIG. 8;

FIG. 10 is a rear elevational view of FIG. 8;

FIG. 11 is a right-side elevational view of FIG. 8;

FIG. 12 is a left-side elevational view of FIG. 8;

FIG. 13 is a top plan view of FIG. 8; and,

FIG. 14 is a bottom plan view of FIG. 8.

The tiltrotor aircraft depicted by broken lines in the drawings has been shown for the purpose of illustrating environment that forms no part of the claimed design.

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