Airplane
Latest Airbus S.A.S. Patents:
- Method for determining striation properties of fatigue striations and for determining the presence of fatigue damage
- Method for determining the positioning of a following aircraft with respect to a leading aircraft flying in front of the following aircraft
- Reputation-Based Trust Determination Method
- Semi-Active Noise Control System for an Aircraft
- Pump Arrangement for Providing a Saturated Liquid
Description
FIG. 1 is a top, front and left side perspective view of an airplane in a closed configuration according to the present invention, the top, front and right side perspective view being a mirror image of the perspective view shown;
FIG. 2 is a top, front and left side perspective view thereof in an open configuration, the top, rear and right side perspective view being a mirror image of the perspective view shown; and,
FIG. 3 is a top, rear and left side perspective view thereof in an open configuration, the top, rear and right side perspective view being a mirror image of the perspective view shown.
Claims
The ornamental design for an airplane, as shown and described.
Referenced Cited
Patent History
Patent number: D516007
Type: Grant
Filed: Nov 14, 2003
Date of Patent: Feb 28, 2006
Assignee: Airbus S.A.S. (Blagnac)
Inventors: Yvon Vigneron (Blagnac), Peter Hall (Bristol), Dave White (Bristol)
Primary Examiner: Marcus A. Jackson
Attorney: Oblon, Spivak, McClelland, Maier & Neustadt, P.C.
Application Number: 29/193,758
Type: Grant
Filed: Nov 14, 2003
Date of Patent: Feb 28, 2006
Assignee: Airbus S.A.S. (Blagnac)
Inventors: Yvon Vigneron (Blagnac), Peter Hall (Bristol), Dave White (Bristol)
Primary Examiner: Marcus A. Jackson
Attorney: Oblon, Spivak, McClelland, Maier & Neustadt, P.C.
Application Number: 29/193,758
Classifications
Current U.S. Class:
Aircraft, Spacecraft, Or Fuselage (D12/319)