Frédéric Sauvinet
Frédéric Sauvinet, Tournefeuille FR
Patent application number | Description | Published |
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20090230253 | METHOD AND DEVICE FOR PILOTING AN AIRCRAFT OPTIMIZING THE CONTROL OF THE AILERONS IN AN ENHANCED-LIFT CONFIGURATION - In conformance with the invention, based on the incident conditions and velocity, the steering of the ailerons is weakly negative (b | 09-17-2009 |
20090250551 | METHOD FOR IMPROVING ROLL STEERING OF AN AIRCRAFT AND AIRCRAFT USING SAME - The invention concerns a method which consists in subdividing the direction of the control surface into at least two elements ( | 10-08-2009 |
20100219298 | METHOD AND DEVICE FOR GENERATING AN OPTIMUM AERODYNAMIC CONFIGURATION OF AN AIRCRAFT DURING A FLIGHT - A process and device for the automatic flight optimisation of the aerodynamic configuration of an aircraft. | 09-02-2010 |
20100222946 | PROCESS AND DEVICE FOR AUTOMATICALLY OPTIMIZING ON THE GROUND THE AERODYNAMIC CONFIGURATION OF AN AIRCRAFT - A process and a device for automatically optimising on the ground the aerodynamic configuration of an aircraft. | 09-02-2010 |
20110029165 | METHOD FOR DETERMINING THE SPEED AT WHICH AN AIRCRAFT BREAKS FREE OF THE GROUND EFFECT - According to the invention, during take-off, the aircraft (AC) is given the tail strike attitude (θ | 02-03-2011 |
20110042526 | METHOD FOR REDUCING THE TAKEOFF RUN OF AN AIRCRAFT - The method of the invention comprises imparting to the flaps ( | 02-24-2011 |
20110054719 | METHOD FOR DRAMATICALLY REDUCING THE TAKE-OFF RUN OF AN AIRCRAFT - According to the invention, during take-off, the aircraft (AC) is given an attitude (θ | 03-03-2011 |
Frédéric Sauvinet, Tournefeuille FR
Patent application number | Description | Published |
---|---|---|
20110029165 | METHOD FOR DETERMINING THE SPEED AT WHICH AN AIRCRAFT BREAKS FREE OF THE GROUND EFFECT - According to the invention, during take-off, the aircraft (AC) is given the tail strike attitude (θ | 02-03-2011 |
20110042526 | METHOD FOR REDUCING THE TAKEOFF RUN OF AN AIRCRAFT - The method of the invention comprises imparting to the flaps ( | 02-24-2011 |
20110054719 | METHOD FOR DRAMATICALLY REDUCING THE TAKE-OFF RUN OF AN AIRCRAFT - According to the invention, during take-off, the aircraft (AC) is given an attitude (θ | 03-03-2011 |