Elements of an aircraft tail
Latest Airbus Operations S.A.S. Patents:
- Deflector provided with faces with different curvatures for a thrust reverser of an aircraft engine nacelle
- Method and a device for manufacturing a part starting from a cushion made of deformable material, in particular for an edge of an element of an aircraft
- Device for manufacturing a stiffened panel making it possible to control the geometry of said stiffened panel, and method for manufacturing a stiffened panel using said device
- Method and system for testing an avionic computer
- Modulable installation for assembling aircraft, and method for changing configuration within such an installation
Throughout the Figures, broken lines showing environment or structure are for illustrative purposes only and form no part of the claimed design.
Claims
The ornamental design for elements of an aircraft tail, as shown and described.
D308043 | May 22, 1990 | Butler |
D311720 | October 30, 1990 | Butler |
D314366 | February 5, 1991 | Waaland et al. |
D500981 | January 18, 2005 | Wilding et al. |
D508013 | August 2, 2005 | Rihn et al. |
D594214 | June 16, 2009 | Matis et al. |
D594809 | June 23, 2009 | Cazals |
D594811 | June 23, 2009 | Cazals |
D595207 | June 30, 2009 | Cazals |
D595213 | June 30, 2009 | Cazals |
D595214 | June 30, 2009 | Cazals |
D597472 | August 4, 2009 | Cazals |
- U.S. Appl. No. 29/323,649, filed Aug. 28, 2008. Title: Aircraft.
- “Boeing Flies Blended Wing Body Research Aircraft” Published by Michael on Jul. 26, 2007 in Aviation News and Boeing, Retrieved from: http://blog.flightstory.net/242/boeing-flies-blended-wing-body-research-aircraft.
Type: Grant
Filed: Aug 28, 2008
Date of Patent: Nov 9, 2010
Assignee: Airbus Operations S.A.S. (Toulouse Cedex)
Inventor: Olivier Cazals (Daux)
Primary Examiner: Cathron C. Brooks
Assistant Examiner: Maurice Stevens
Attorney: Osler, Hoskin & Harcourt LLP
Application Number: 29/323,643