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Publication numberUSD622653 S1
Publication typeGrant
Application numberUS 29/247,058
Publication dateAug 31, 2010
Filing dateMay 26, 2006
Priority dateJan 30, 2006
Publication number247058, 29247058, US D622653 S1, US D622653S1, US-S1-D622653, USD622653 S1, USD622653S1
InventorsMatthew D. Moore, Kelly L. Boren, Edward C. Marques
Original AssigneeThe Boeing Company
Export CitationBiBTeX, EndNote, RefMan
External Links: USPTO, USPTO Assignment, Espacenet
Aircraft
US D622653 S1
Abstract  available in
Images(11)
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Claims(1)
  1. The ornamental design for an aircraft, as shown and described.
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.

Non-Patent Citations
Reference
1"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.
2"Stealth Aircraft the Technology behind the planes", www.seorf.ohiou.edu, Jan. 20, 2006, pp. 1-12.
3Geoffrey 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.
4Meyer 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.
5Mizrahi, "Flight to the Future", Jan. 20, 2006, www.twitt.org/bldwing.htm, pp. 1-9.
Referenced by
Citing PatentFiling datePublication dateApplicantTitle
US8313055 *Oct 23, 2006Nov 20, 2012Airbus Operations SasAircraft having a reduced environmental impact
US8393567 *Nov 15, 2010Mar 12, 2013The Boeing CompanyMethod and apparatus for reducing aircraft noise
US8608108Dec 3, 2010Dec 17, 2013The Boeing CompanyAircraft configuration with ramp access to multiple decks
US20120119023 *Nov 15, 2010May 17, 2012The Boeing CompanyMethod and apparatus for reducing aircraft noise
Classifications
U.S. ClassificationD12/319