Patent application number | Description | Published |
20130078049 | SURFACE-AREA SAFETY MEANS AND A VEHICLE - Surface-area safety means ( | 03-28-2013 |
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 |
20130082135 | HYBRID AIRCRAFT HAVING A ROTARY WING - An aircraft ( | 04-04-2013 |
20130093632 | AIRCRAFT ANTENNA, AND AN AIRCRAFT - The present invention relates to an antenna ( | 04-18-2013 |
20130114995 | BALL-JOINT MECHANISM BETWEEN A CLEVIS AND A CONNECTING ROD, IN PARTICULAR FOR CONTROL APPARATUS OF A ROTORCRAFT - A ball-joint mechanism between a connecting rod ( | 05-09-2013 |
20130119187 | DEVICE FOR VARYING BLADE PITCH OF A LIFT ROTOR - The present invention relates to a device ( | 05-16-2013 |
20130119192 | ANTIVIBRATION SUSPENSION MEANS FOR A TIE BAR OF AN AIRCRAFT POWER TRANSMISSION GEARBOX, AN ANTIVIBRATION SUSPENSION DEVICE, AND AN AIRCRAFT - An antivibration suspension device ( | 05-16-2013 |
20130127081 | APPLIANCE FOR LOCALIZED HEATING OF A POLYMER MATERIAL SURFACE TO BE REPAIRED BY BLOWING A HOT FLUID INSIDE A CONFINEMENT CHAMBER - The invention provides an appliance for localized heating of a polymer material surface to be repaired by blowing a hot fluid inside a confinement chamber ( | 05-23-2013 |
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 |
20130134256 | ANTI-TORQUE DEVICE WITH LONGITUDINAL THRUST FOR A ROTORCRAFT - A tail assembly ( | 05-30-2013 |
20130142658 | ROTOR BLADE | 06-06-2013 |
20130146706 | METHOD AND A ROTARY WING AIRCRAFT OPTIMIZED FOR MINIMIZING THE CONSEQUENCES OF A RUNNING OFF-SPECIFICATION EMERGENCY LANDING - A method of minimizing the consequences of an off-specification landing for the occupants of an aircraft ( | 06-13-2013 |
20130147242 | DEVICE FOR PROTECTING AN INDIVIDUAL SITTING ON A SEAT, A SEAT, AND A VEHICLE - A protection device ( | 06-13-2013 |
20130149149 | ROTOCRAFT ROTOR INCLUDING A FLAPPING ABUTMENT MECHANISM FOR BLADES HINGED ON A HUB OF THE ROTOR - An abutment mechanism for limiting the flapping of the blades of a rotor ( | 06-13-2013 |
20130164074 | DEVICE FOR REVERSIBLY FASTENING A PANEL TO A STRUCTURE SO AS TO OBTAIN A WINDOW IN THAT STRUCTURE, A VEHICLE, AND A METHOD | 06-27-2013 |
20130164143 | LAMINATED ABUTMENT, A ROTOR PROVIDED WITH SUCH AN ABUTMENT, AND AN AIRCRAFT - A laminated abutment ( | 06-27-2013 |
20130184903 | AIRCRAFT POWER PLANT, AN AIRCRAFT, AND A METHOD OF PILOTING SAID AIRCRAFT - An aircraft power plant ( | 07-18-2013 |
20130192903 | ON-BOARD DEVICE FOR MEASURING THE WEIGHT OF AN AIRCRAFT AND THE POSITION OF ITS CENTER OF GRAVITY - An on-board device ( | 08-01-2013 |
20130194140 | COMMUNICATION DEVICE, AN AIRCRAFT ROTOR, AND AN AIRCRAFT - A communication device ( | 08-01-2013 |
20130199197 | DEVICE AND A METHOD FOR REGULATING A TURBINE ENGINE, AND AN AIRCRAFT - A regulator device ( | 08-08-2013 |
20130199204 | METHOD AND A DEVICE FOR PERFORMING A CHECK OF THE HEALTH OF A TURBINE ENGINE OF AN AIRCRAFT PROVIDED WITH AT LEAST ONE TURBINE ENGINE - A method of automatically performing an engine health check for checking the health of at least one turbine engine of an aircraft. During flight, the stability of at least one monitoring parameter is verified by acquiring a measurement signal, by performing first filtering of each signal by a high-pass filter over a long first duration (TPS | 08-08-2013 |
20130200231 | INTERFACE AND A METHOD FOR MOUNTING TOGETHER A PIECE OF EQUIPMENT AND A ROTARY DRIVE SOURCE IN A ROTORCRAFT POWER PLANT - An interface and a method for mounting a piece of equipment ( | 08-08-2013 |
20130201023 | DRAINAGE CIRCUIT FOR DRAINING LIQUID COMING FROM A POWER PLANT OF A ROTORCRAFT, THE CIRCUIT INCORPORATING AN APPLIANCE FOR MONITORING AN EXCESSIVE FLOW OF THE LIQUID - The invention relates to a drainage circuit ( | 08-08-2013 |
20130203021 | METHOD OF SIMULATING A FAILURE ON AN AIRCRAFT - A method of failure simulation for an aircraft ( | 08-08-2013 |
20130204468 | METHOD AND A DEVICE FOR PERFORMING A HEALTH CHECK OF A TURBINE ENGINE OF AN AIRCRAFT HAVING AT LEAST ONE SUCH ENGINE - A method of performing a health check of at least one turbine engine ( | 08-08-2013 |
20130204507 | METHOD AND A DEVICE FOR MONITORING AN ENGINE - A method of monitoring at least one limited-lifetime part. During an identification step (STP | 08-08-2013 |