Patent application number | Description | Published |
20130211703 | METHOD OF PROVIDING A VOLUME-MASS LAW FOR FUEL CONSUMPTION - A method of providing a volume-mass law for determination of a fuel flow rate of an engine, particularly providing a fuel flow rate to a helicopter turbine, comprising the steps of: determining a sample type of fuel and a start density ρ | 08-15-2013 |
20130264412 | ROTARY WING AIRCRAFT HAVING A TAIL ROTOR, AND A METHOD OF OPTIMIZING THE OPERATION OF A TAIL ROTOR - A rotary wing aircraft ( | 10-10-2013 |
20130277499 | AIRCRAFT AIRFOIL, AND AN AIRCRAFT PROVIDED WITH SUCH AN AIRFOIL - An airfoil ( | 10-24-2013 |
20130291549 | DEVICE AND A METHOD OF REGULATING A POWER PLANT INCLUDING AT LEAST ONE TURBINE ENGINE, AND AN AIRCRAFT - A regulator device ( | 11-07-2013 |
20130294884 | DEVICE FOR MONITORING THE SEALING OF A ROTORCRAFT TRANSMISSION BOX BY SUCTION - A device for monitoring the sealing state of a casing ( | 11-07-2013 |
20130313355 | PITCHING STABILIZATION MEANS AND A ROTARY WING AIRCRAFT INCLUDING SUCH MEANS - A pitching stabilization means ( | 11-28-2013 |
20130323043 | ROTOR BLADE, A ROTOR, AN AIRCRAFT, AND A METHOD | 12-05-2013 |
20130327548 | FIRE-PROTECTION STORAGE MEANS, A VEHICLE, AND A METHOD - The present invention relates to fire-protection storage means ( | 12-12-2013 |
20130327896 | ROTORCRAFT YAW PILOTING SYSTEM MAKING USE OF A MEMBER OF THE HUMAN-OPERATED TYPE AND OF A FLIGHT CONTROL GENERATOR FO THE OBJECTIVE TYPE - A system and a method for controlling a rotorcraft ( | 12-12-2013 |
20130340459 | FLUID TEMPERATURE CONTROL INSTALLATION FOR ROTORCRAFT, ASSOCIATING A SYSTEM FOR COOLING A POWER PLANT WITH A SYSTEM FOR HEATING A CABIN - A fluid temperature control installation for a rotorcraft, the installation comprising a system for cooling a main transmission ( | 12-26-2013 |
20140020396 | METHOD OF AUTOMATICALLY REGULATING AN AIRCRAFT POWER PLANT, A DEVICE, AND AN AIRCRAFT - The present invention relates to an automatic method of regulating a power plant ( | 01-23-2014 |
20140200844 | METHOD OF OPTIMIZING THE PERFORMANCE OF AN AIRCRAFT, A DEVICE, AND AN AIRCRAFT - A method of optimizing the performance of a rotary wing aircraft having at least one turbine engine with a gas generator and a turbine assembly comprising at least one turbine. In a definition step (STP | 07-17-2014 |