Eglin, FR
Georges Eglin, Beziers FR
Patent application number | Description | Published |
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20090118571 | METHOD AND IMPLANT FOR CURING CYSTOCELE - An implant for the treatment of cystocele, having a thin and supple structure, comprises a support body ( | 05-07-2009 |
20100030015 | SYSTEM FOR TREATING RECTOCELE IN A WOMAN - A system for treating rectocele in a woman includes an implant comprising a support body from which there extends at least to upper suspension stabilizers each disposed on either side of a sagittal plane on a longitudinal axis, the longitudinal axes forming between them an angle greater than 45°, and two lower suspension stabilizers disposed on either side of the sagittal plane; and an introduction device for inserting the implant in the woman, the introduction device shaped analogous to that of the implant and comprising a hollow body defining a cavity configured to receive the support body of the implant, tubular straps extending from the hollow body with each defining a cavity for receiving one of the suspension stabilizers of the implant, traction means extending from an end of each of the tubular straps, and a cut initiator provided on the hollow body. | 02-04-2010 |
20100234680 | METHOD OF TREATMENT OF PROLAPSES - The present invention relates to a method of treatment of a urogenital prolapse, said method comprising the following steps: | 09-16-2010 |
Luc Eglin, Paris FR
Patent application number | Description | Published |
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20080215267 | Processing of a Signal Representing Radiation - A method for processing a noisy digital time signal yk of digital pitch k, corresponding to an initial analog signal St after being conditioned by a conditioning chain. The initial analog signal St comprises at least one pulse representing an information concerning at least one radiation ( | 09-04-2008 |
Paul Eglin, Aix En Provence FR
Patent application number | Description | Published |
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20100243792 | METHOD AND A DEVICE FOR OPTIMIZING THE OPERATION OF PROPULSIVE PROPELLERS DISPOSED ON EITHER SIDE OF A ROTORCRAFT FUSELAGE - A method of optimizing the operation of left and right propellers disposed on either side of the fuselage of a rotorcraft including a main rotor. Left and right aerodynamic surfaces include respective left and right flaps suitable for being deflected, yaw stabilization of the rotorcraft being achieved via first and second pitches respectively of the left and right propellers, and the deflection angles of the left and right flaps are adjusted solely during predetermined stages of flight in order to minimize a differential pitch of the left and right propellers so as to optimize the operation of the left and right propellers, the predetermined stages of flight including stages of flight at low speed performed at an indicated air speed (IAS) of the rotorcraft that is below a predetermined threshold, and stages of yaw-stabilized flight at high speed performed at an indicated air speed of the rotorcraft greater than the predetermined threshold. | 09-30-2010 |
20100308154 | METHOD OF CONTROLLING A HYBRID HELICOPTER IN YAW, AND A HYBRID HELICOPTER PROVIDED WITH A YAW CONTROL DEVICE SUITABLE FOR IMPLEMENTING SAID METHOD - A method of controlling the yaw attitude of a hybrid helicopter including a fuselage and an additional lift surface provided with first and second half-wings extending from either side of the fuselage, each half-wing being provided with a respective first or second propeller. The hybrid helicopter has a thrust control suitable for modifying the first pitch of the first blades of the first propeller and the second pitch of the second blades of the second propeller by the same amount. The hybrid helicopter includes yaw control elements for generating an original order for modifying the yaw attitude of the hybrid helicopter by increasing the pitch of the blades of one propeller and decreasing the pitch of the blades of the other propeller, the original order is optimized as a function of the position of the thrust control to obtain an optimized yaw control order that is applied to the first and second blades. | 12-09-2010 |
20100310371 | DRIVE CONTROL AND REGULATION METHOD AND SYSTEM FOR A HYBRID HELICOPTER - The present invention relates to a control and regulation method for a rotorcraft having at least one variable-pitch propulsive propeller and at least one power source for driving the propeller(s), said method consisting in generating at least one mean pitch setpoint βtcl for the propeller(s) as a function of a thrust variation control order Tcl, wherein the method consists in defining a plurality of operating modes, including: | 12-09-2010 |
Paul Eglin, Roquefort - La Bedoule FR
Patent application number | Description | Published |
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20120153072 | METHOD OF CONTROLLING AND REGULATING THE DEFLECTION ANGLE OF A TAILPLANE IN A HYBRID HELICOPTER - A method of controlling and regulating a rotorcraft presenting a speed of advance that is high and stabilized, the rotorcraft including at least a main lift rotor ( | 06-21-2012 |
20130079956 | METHOD OF REGULATING THE PROPULSIVE SPEED OF A HYBRID HELICOPTER - A method of regulating the propulsion speed of a hybrid helicopter. In application of a correction process for protecting the hybrid helicopter, piloting orders generated by a manual control member relate to an airspeed setpoint and they are corrected by control means in accordance with at least one correction mode in which the piloting orders are corrected in application of a rule that takes account of a setpoint consumed power corresponding to the airspeed setpoint derived from the piloting order. | 03-28-2013 |
20130131896 | METHOD OF ASSISTED PILOTING OF A ROTARY WING AIRCRAFT HAVING AT LEAST ONE PROPULSION PROPELLER, AN ASSISTED PILOTING DEVICE, AND AN AIRCRAFT | 05-23-2013 |
20130175385 | METHOD OF AUTOMATICALLY CONTROLLING A ROTARY WING AIRCRAFT HAVING AT LEAST ONE PROPULSION PROPELLER, AN AUTOPILOT DEVICE, AND AN AIRCRAFT - An autopilot device ( | 07-11-2013 |
20130184902 | PILOTING ASSISTANCE METHOD, A PILOTING ASSISTANCE DEVICE, AND AN AIRCRAFT - A piloting assistance device ( | 07-18-2013 |
20140034774 | FAST, LONG-RANGE AIRCRAFT - An aircraft ( | 02-06-2014 |
20140084105 | METHOD OF CONTROLLING THE WING FLAPS AND HORIZONTAL STABILIZER OF A HYBRID HELICOPTER - A method of controlling a high speed rotary wing aircraft ( | 03-27-2014 |
20140084106 | METHOD OF CONTROLLING THE WING FLAPS AND HORIZONTAL STABILIZER OF A HYBRID HELICOPTER - A method of controlling a high-speed rotary wing aircraft ( | 03-27-2014 |