Aircraft

- The Boeing Company
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Description

FIG. 1 is a perspective view of a first embodiment of an aircraft showing my new design;

FIG. 2 is a left side view of the aircraft as shown in FIG. 1 showing our new design, which is a mirror image of the right side view;

FIG. 3 is a top view of the aircraft as shown in FIG. 1 showing our new design;

FIG. 4 is a bottom view of the aircraft as shown in FIG. 1 showing our new design;

FIG. 5 is a front view of the aircraft as shown in FIG. 1 showing our new design;

FIG. 6 is a back view of the aircraft as shown in FIG. 1 showing our new design;

FIG. 7 is a perspective view of a second embodiment of an aircraft showing our new design;

FIG. 8 is a left side view of the aircraft as shown in FIG. 7 showing our new design, which is a mirror image of the right side view;

FIG. 9 is a top view of the aircraft as shown in FIG. 7 showing our new design;

FIG. 10 is a bottom view of the aircraft as shown in FIG. 7 showing our new design;

FIG. 11 is a front view of the aircraft as shown in FIG. 7 showing our new design; and,

FIG. 12 is a back view of the aircraft as shown in FIG. 7 showing our new design.

The broken line showing of portions of an aircraft is included for the purpose of illustrating environmental structure and forms no part of the claimed design.

Claims

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

Referenced Cited
U.S. Patent Documents
3576300 April 1971 Palfreyman
3727862 April 1973 Kaufhold et al.
4019699 April 26, 1977 Wintersdorff et al.
4036452 July 19, 1977 Schairer
4171786 October 23, 1979 Krenz
4311289 January 19, 1982 Finch
4447022 May 8, 1984 Lion
4449680 May 22, 1984 Gratzer et al.
4836469 June 6, 1989 Wagenfeld
5348256 September 20, 1994 Parikh
5738298 April 14, 1998 Ross et al.
6102328 August 15, 2000 Kumata et al.
6308913 October 30, 2001 Fujino et al.
D516995 March 14, 2006 Eatkins et al.
D566031 April 8, 2008 Beaunis et al.
Other references
  • Meyer Reshotko, Jack H. Goodykoontz and Robert G. Dorsch, “Engine-Over-the-Wing Noise Research”, J. Aircraft, Apr. 1974, pp. 195-196, Vol. 11, No. 4.
  • “Noise-Reduction Benefits Analyzed for Over-the-Wing-Mounted Advanced Turbofan Engine (Synopsis)”, www-paso.grc.nasa.gov/Library/Abstracts/berton6.hmtl, Jan. 20, 2006, pp. 1-2.
  • Mizrahi, “Flight to the Future”, Jan. 20, 2006, www.twitt.org/bldwing.htm, pp. 1-9.
  • “Stealth Aircraft the Technology behind the planes”, www.seorf.ohiou.edu, Jan. 20, 2006, pp. 1-12.
  • Geoffrey A. Hill and Russell H. Thomas, “Challenges and Opportunities for Noise Reduction Through Advanced Aircraft Propulsion Airframe Integration and Configurations”, 8th CEAS Workshop: Aeroacoustics of New Aircraft and Engine Configurations, Budapest, Hungary, 2004, pp. 1-13.
Patent History
Patent number: D622653
Type: Grant
Filed: May 26, 2006
Date of Patent: Aug 31, 2010
Assignee: The Boeing Company (Irvine, CA)
Inventors: Matthew D. Moore (Everett, WA), Kelly L. Boren (Arlington, WA), Edward C. Marques (Issaquah, WA)
Primary Examiner: Lisa P Lichtenstein
Attorney: Moore & Van Allen PLLC
Application Number: 29/247,058
Classifications
Current U.S. Class: Aircraft, Spacecraft, Or Fuselage (D12/319)