| Patent Number |
Title Of Patent |
Date Issued |
| D581343 |
Element of an aircraft body |
November 25, 2008 |
|
| D581342 |
Element of an aircraft |
November 25, 2008 |
|
| D569783 |
Combined engines and tailwing for a plane |
May 27, 2008 |
|
| D566031 |
Plane |
April 8, 2008 |
|
| D495988 |
Plane |
September 14, 2004 |
|
| 7463957 |
Method for operating an aircraft |
December 9, 2008 |
| A method for operating an aircraft includes the steps of receiving guidance instructions and guidance parameters at a navigation computer, and transmitting automatic pilot instructions from the navigation computer to a flight control computer. The method also includes the steps of re |
| 7430180 |
Package switching network with a deterministic behavior |
September 30, 2008 |
| A packet switching network including subscriber stations connected to each other through at least one switch, which has a behavior defined as deterministic in that any packet sent on the network from a source subscriber station joins the destination subscriber station(s) within a lim |
| 7418851 |
Device for crimping a contact on a cable |
September 2, 2008 |
| A device for crimping a sleeve of a contact on to a sheath of an electrical cable comprises a diaphragm. The diaphragm applies walls of the sleeve against the sheath. Jaws forming the diaphragm have a generally triangular shape. The crimping device may include means for checking the |
| 7395330 |
Process and system evaluating deterministic behavior of a packet switching network |
July 1, 2008 |
| A process and system for evaluating the deterministic behavior of a packet switching network including subscriber stations connected to each other through at least one switch, the behavior defined as deterministic if any packet sent on the network from a source subscriber station joins t |
| 7362755 |
Process for implementing a switched full-duplex ethernet type communication network with redunda |
April 22, 2008 |
| A process for implementing a redundant switched full-duplex Ethernet type communication network including at least two independent elementary networks, each elementary network including at least one source subscriber equipment and at least one destination subscriber equipment, connec |
| 7356028 |
Redundant switched full-duplex Ethernet type communication network |
April 8, 2008 |
| A redundant switched full-duplex Ethernet type communication network including at least two independent elementary networks, each elementary network including at least one source subscriber equipment and at least one destination subscriber equipment, connected to each other through at |
| 7352744 |
Switched full-duplex ethernet type communication network and implementation process for this net |
April 1, 2008 |
| A switched full-duplex Ethernet type communication network including at least one source subscriber equipment and at least one destination subscriber equipment connected to each other through at least one physical link through at least one switch and at least one virtual link, which |
| 7339901 |
Process for controlling a switched full-duplex ethernet type communication network |
March 4, 2008 |
| A process for controlling a switched full-duplex Ethernet type communication network including at least one source subscriber equipment and at least one destination subscriber equipment connected to each other through at least one physical link through at least one switch and at leas |
| 7260455 |
System for operating an aircraft |
August 21, 2007 |
| A system for operating an aircraft includes a navigation computer and a flight control computer. The navigation computer receives guidance instructions and guidance parameters, and outputs automatic pilot instructions. The flight control computer receives control instructions and the |
| 7212890 |
Aircraft dialog device for dialog with system of aircraft |
May 1, 2007 |
| A dialog system for dialog between an operator of an aircraft and at least one system of the aircraft including a display configured to display at least one window including a plurality of responsive objects respectively associated with one of multiple functions of the at least one syste |
| 7168369 |
Device for moving a machine |
January 30, 2007 |
| A device for moving a machine or the like between plural workstations includes: a mechanism for suspending the machine, a guide, a structure for supplying the guide with electrical energy, a mechanical linkage between the machine and the guide, a connector for electrically connecting |
| 7123999 |
Aircraft dialog device for dialog with system of aircraft |
October 17, 2006 |
| A dialog method for dialog between an operator of an aircraft and at least one system of the aircraft. The method includes the steps of displaying on a display at least one window including a plurality of responsive objects respectively associated with one of multiple functions of the at |
| 7015829 |
Method for displaying flight information |
March 21, 2006 |
| A method for displaying flight information includes displaying a first characteristic sign illustrating a speed vector of an aircraft. The method also includes determining a first longitudinal margin of maneuver of the aircraft as a load factor, and displaying a second characteristic |
| 6990419 |
System for identifying a signal source |
January 24, 2006 |
| A system for identifying a signal source in a predetermined space, the system including multiple sensing units arranged at different locations to detect signals in the predetermined space. The system also includes one or more recording units arranged to separately and simultaneously |
| 6986483 |
Inertial reference system for an aircraft |
January 17, 2006 |
| An inertial reference system for an aircraft includes two accelerometers and a gyrometer. One accelerometer is located at a front portion of the aircraft, the other is located at a rear portion of the aircraft. The gyrometer is located at a center portion of the aircraft. The system also |
| 6980128 |
Display system for an aircraft |
December 27, 2005 |
| A display system for an aircraft includes a central unit configured to determine a speed vector of the aircraft and to determine a longitudinal margin of maneuver of the aircraft. The longitudinal margin of maneuver is expressed as a load factor and is related to one of a pitch-up maneuv |
| 6976656 |
Method for controlling the flight of an aircraft |
December 20, 2005 |
| A method for controlling an aircraft includes the steps of receiving acceleration data related to an acceleration of a front portion of the aircraft, and receiving pitch, roll, and/or yaw rate data related to a rate of a center portion of the aircraft. The method also includes a step |
| 6892152 |
Method for identifying a signal source |
May 10, 2005 |
| A method for identifying a signal source in a predetermined space, the method including inventorying a set of identified signatures corresponding to a plurality of signal sources and recording a signal simultaneously at different locations of the predetermined space. Parameters related t |
