"What, sir, would you make a ship sail against the wind and currents by lighting a bonfire under her deck? I pray you, excuse me, I have not the time to listen to such nonsense."
Napoleon Bonaparte ; When told of the Robert Fulton steamboat
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| Application No. | Application Title | Issue Date |
| 20100155524 | MONOMOLECULAR CARBON-BASED FILM FOR FORMING LUBRICIOUS SURFACE ON AIRCRAFT PARTS A monomolecular carbon-based film can be placed on an aircraft part, such as the leading edge designed to directly impinge against air during flight, ascent or descent, in order to form a smooth surface having increased lubricity and reduced air friction. The aircraft p... | 06/24/2010 |
| 20100155527 | MONOMOLECULAR CARBON-BASED FILM FOR FORMING LUBRICIOUS SURFACE ON AIRCRAFT PARTS A monomolecular carbon-based film can be placed on an aircraft part, such as the leading edge designed to directly impinge against air during flight, ascent or descent, in order to form a smooth surface having increased lubricity and reduced air friction. The aircraft p... | 06/24/2010 |
| 20100032519 | AIRPLANE WITH A MODIFIABLE SURFACE OF VERTICAL EMPANNAGE An aircraft has a vertical fin fastened to the rear and above a fuselage of elongated form, essentially in a vertical plane of symmetry of the aircraft. The vertical fin has at least two stable positions, an extended position and a returned position, such that a surface... | 02/11/2010 |
| 20090026311 | Aircraft tail assembly An aircraft tail assembly planform comprising curvilinear leading edges (21) and trailing edges (22), with an aircraft tail assembly configuration in which the hinge line (13) is rectilinear and has a non-constant percentage with respect to the chor... | 01/29/2009 |
| 20070131821 | Wing/winglet configuration and aircraft including it A wing/winglet configuration includes an airfoil and a winglet disposed at one end of said airfoil, said airfoil and said winglet defining an airfoil zone, a winglet zone and a connecting zone of connection of the winglet and the airfoil, a portion of the upper surface ... | 06/14/2007 |
| 20070136030 | METHOD AND DEVICE FOR DETECTING AN OVERSTEPPING OF DESIGN LOADS OF THE FIN OF AN AIRCRAFT The device (1) comprises a set (2) of information sources, means (3) for determining, with the aid of information emanating from said set (2), a current bending moment, means (5) for determining, with the aid of information emanating f... | 06/14/2007 |