Blended wing and multiple body airplane configuration

- The Boeing Company
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Description

FIG. 1 is a top, front isometric view of the aircraft, with the broken line showing for illustrative purposes and forming no part of the claimed design;

FIG. 2 is a top plan view of the aircraft;

FIG. 3 is a bottom plan view of the aircraft;

FIG. 4 is a left side elevation view of the aircraft;

FIG. 5 is a right side elevation view of the aircraft;

FIG. 6 is a front elevation view of the aircraft; and,

FIG. 7 is a rear elevation view of the aircraft.

Claims

The ornamental design for a blended wing and multiple-body airplane configuration, as shown and described.

Referenced Cited
U.S. Patent Documents
D139438 November 1944 Hughes et al.
D146072 December 1946 Bowers
D273005 March 13, 1984 McComas
Patent History
Patent number: D456337
Type: Grant
Filed: Mar 23, 2001
Date of Patent: Apr 30, 2002
Assignee: The Boeing Company (Seattle, WA)
Inventors: Mithra M. K. V. Sankrithi (Federal Way, WA), Steven J. Wald (Seattle, WA), Gary R. Thomas (Seattle, WA)
Primary Examiner: Marcus A. Jackson
Attorney, Agent or Law Firm: Conrad O. Gardner
Application Number: 29/139,037
Classifications
Current U.S. Class: Plural Fuselages Or Tail Booms (D12/335)
International Classification: 1207;