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Inventor: Cazals; Olivier
Address: Daux, FR
No. of patents: 18
Patents:
| Patent Number |
Title Of Patent |
Date Issued |
| D597472 |
Aircraft |
August 4, 2009 |
|
| D595634 |
Aircraft tail |
July 7, 2009 |
|
| D595214 |
Aircraft tail |
June 30, 2009 |
|
| D595213 |
Aircraft tail |
June 30, 2009 |
|
| D595212 |
Aircraft tail |
June 30, 2009 |
|
| D595211 |
Aircraft tail |
June 30, 2009 |
|
| D595210 |
Aircraft tail |
June 30, 2009 |
|
| D595209 |
Aircraft tail |
June 30, 2009 |
|
| D595208 |
Aircraft tail |
June 30, 2009 |
|
| D595207 |
Aircraft tail |
June 30, 2009 |
|
| D595206 |
Aircraft tail |
June 30, 2009 |
|
| D594811 |
Aircraft tail |
June 23, 2009 |
|
| D594810 |
Aircraft tail |
June 23, 2009 |
|
| D594809 |
Aircraft tail |
June 23, 2009 |
|
| D594808 |
Aircraft tail |
June 23, 2009 |
|
| D581343 |
Element of an aircraft body |
November 25, 2008 |
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| D581342 |
Element of an aircraft |
November 25, 2008 |
|
| 7240877 |
Multi-engined aircraft with lowering shaft |
July 10, 2007 |
| A multi-engine aircraft having one engine positioned at the tail of the fuselage may include rear tail units in a vertical longitudinal plane-of-symmetry of the fuselage. The tail engine is disposed in front of the rear tail units on the upper part of the tail of the fuselage. The ta |
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