EUROCOPTER Patent applications |
Patent application number | Title | Published |
20150125258 | ROTARY WING AIRCRAFT HAVING TWO MAIN ENGINES TOGETHER WITH A LESS POWERFUL SECONDARY ENGINE, AND A CORRESPONDING METHOD - An aircraft ( | 05-07-2015 |
20150028594 | REVERSIBLE ELECTRICAL MACHINE FOR AN AIRCRAFT - A reversible electrical machine ( | 01-29-2015 |
20140319265 | METHOD OF AUTOMATICALLY TRIGGERING AN EMERGENCY BUOYANCY SYSTEM FOR A HYBRID HELICOPTER - A method of automatically triggering an emergency buoyancy system ( | 10-30-2014 |
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 |
20140191613 | ELECTRIC MACHINE WITH INTERMEDIATE PIECES HAVING MULTIPLE AIR GAPS AND A 3D MAGNETIC FLUX - The present invention relates to an electric machine ( | 07-10-2014 |
20140191612 | ELECTRIC MACHINE WITH MULTIPLE AIR GAPS AND A 3D MAGNETIC FLUX - The present invention relates to an electric machine ( | 07-10-2014 |
20140145030 | METHOD OF ARRANGING A BUOYANCY SYSTEM ON AN AIRCRAFT, A BUOYANCY SYSTEM FOR AN AIRCRAFT, AND AN AIRCRAFT - A buoyancy system ( | 05-29-2014 |
20140145028 | METHOD AND A ROTARY WING AIRCRAFT HAVING THREE ENGINES - An aircraft ( | 05-29-2014 |
20140144917 | FUEL STORAGE TANK, AN AIRCRAFT, AND A METHOD | 05-29-2014 |
20140137979 | FUEL STORAGE DEVICE, AN AIRCRAFT, AND A METHOD - A fuel storage device ( | 05-22-2014 |
20140117154 | ROTORCRAFT FITTED WITH A MOUNTING STRUCTURE FOR JOINTLY MOUNTING A CONTROL PANEL AND AN AVIONICS RACK PREVIOUSLY FITTED WITH A UNITARY CABLING ASSEMBLY - A rotorcraft fitted with means for mounting at least one front avionics rack ( | 05-01-2014 |
20140117148 | METHOD OF MANAGING AN ENGINE FAILURE ON A MULTI-ENGINED AIRCRAFT HAVING A HYBRID POWER PLANT - A method of managing an engine failure on a rotary wing aircraft ( | 05-01-2014 |
20140112490 | METHOD AND AN ACTIVE DEVICE FOR TREATING NOISE ON BOARD A VEHICLE, AND A VEHICLE PROVIDED WITH SUCH A DEVICE - A noise treatment device (D) comprising at least one local noise sound sensor ( | 04-24-2014 |
20140089542 | CHAINED INFORMATION EXCHANGE SYSTEM COMPRISING A PLURALITY OF MODULES CONNECTED TOGETHER BY HARDENED DIGITAL BUSES - A chained information exchange system ( | 03-27-2014 |
20140084109 | LANDING GEAR PROVIDED WITH A STIFFENER FOR INCREASING ITS STIFFNESS IN ROLL, AND AN AIRCRAFT - Aircraft landing gear ( | 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 |
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 |
20140077026 | PITCH STABILIZER AND ROTARY-WING AIRCRAFT EQUIPPED WITH SUCH STABILIZER - A pitch stabilizer [ | 03-20-2014 |
20140070048 | METHOD AND AN AIRCRAFT FOR MINIMIZING THE RISKS OF THE AIRCRAFT TOPPLING ON THE GROUND - A method of assisting a pilot in order to minimize the risks of an aircraft rolling over on the ground, the aircraft having a main rotor and a yaw movement control rotor ( | 03-13-2014 |
20140054411 | METHOD OF ASSISTING A PILOT OF A SINGLE-ENGINED ROTARY WING AIRCRAFT DURING A STAGE OF FLIGHT IN AUTOROTATION - A method of assisting a pilot of a single-engined rotary wing aircraft ( | 02-27-2014 |
20140039809 | METHOD OF DETECTING DEFECTS OF A ROLLING BEARING BY VIBRATION ANALYSIS - A method of detecting defects in a rolling bearing ( | 02-06-2014 |
20140034774 | FAST, LONG-RANGE AIRCRAFT - An aircraft ( | 02-06-2014 |
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 |
20140014252 | METHOD AND A DEVICE FOR BONDING A METAL FAIRING TO THE LEADING EDGE OF AN AIRFOIL - The present invention relates to a method and to a device ( | 01-16-2014 |
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 |
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 |
20130327548 | FIRE-PROTECTION STORAGE MEANS, A VEHICLE, AND A METHOD - The present invention relates to fire-protection storage means ( | 12-12-2013 |
20130323043 | ROTOR BLADE, A ROTOR, AN AIRCRAFT, AND A METHOD | 12-05-2013 |
20130320146 | TANK, A FUEL STORAGE SYSTEM, AND AN AIRCRAFT - A storage tank ( | 12-05-2013 |
20130313355 | PITCHING STABILIZATION MEANS AND A ROTARY WING AIRCRAFT INCLUDING SUCH MEANS - A pitching stabilization means ( | 11-28-2013 |
20130308995 | BALL JOINT DEVICE - A ball joint device ( | 11-21-2013 |
20130307378 | ELECTRICAL POWER SUPPLY DEVICE FOR POWERING AT LEAST ONE PIECE OF EQUIPMENT OF AN AIRCRAFT ROTOR, AND AN AIRCRAFT - An electrical power supply device ( | 11-21-2013 |
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 |
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 |
20130288809 | FLEXIBLE COUPLING MEANS AND A MECHANICAL TRANSMISSION - A coupling means ( | 10-31-2013 |
20130284150 | FUEL FEED NETWORK FOR A ROTORCRAFT ENGINE, THE NETWORK INCLUDING MEANS FOR PRIMING A PUMP FOR SUCKING FUEL FROM A FEED TANK - A fluid flow network for feeding fuel to at least one engine ( | 10-31-2013 |
20130282205 | STANDBY INSTRUMENT FOR AN AIRCRAFT, THE INSTRUMENT PROVIDING FLIGHT INFORMATION, POWER MARGIN INFORMATION, AND ASSISTANCE IN PILOTING - A standby instrument ( | 10-24-2013 |
20130277499 | AIRCRAFT AIRFOIL, AND AN AIRCRAFT PROVIDED WITH SUCH AN AIRFOIL - An airfoil ( | 10-24-2013 |
20130268146 | METHOD AND A DEVICE FOR ADAPTING THE MAN-MACHINE INTERFACE OF AN AIRCRAFT DEPENDING ON THE LEVEL OF THE PILOT'S FUNCTIONAL STATE - A method of adapting a man-machine interface ( | 10-10-2013 |
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 |
20130247577 | CONTROL METHOD FOR AN OVERSPEED SAFETY SYSTEM, AND AN ASSOCIATED SYSTEM AND AIRCRAFT - A control method for controlling an overspeed safety system ( | 09-26-2013 |
20130243597 | DEVICE FOR MONITORING THE FLAPPING AND/OR LAG BEHAVIOR OF A BLADE OF A ROTORCRAFT ROTOR - The present invention relates to a rotorcraft rotor ( | 09-19-2013 |
20130228652 | AIRCRAFT BENCH PROVIDED WITH CRASH-PROTECTION MEANS - A crashworthy bench ( | 09-05-2013 |
20130213044 | ARCHITECTURE FOR FEEDING FUEL TO A POWER PLANT FOR DRIVING A ROTARY WING OF A ROTORCRAFT - An architecture for feeding fuel to a power plant ( | 08-22-2013 |
20130212865 | DEVICE FOR FASTENING A NUT TO THE SURFACE OF A BODY BY MEANS OF AN ASSEMBLY PLATE - A device for fastening a nut ( | 08-22-2013 |
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 |
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 |
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 |
20130203021 | METHOD OF SIMULATING A FAILURE ON AN AIRCRAFT - A method of failure simulation for an aircraft ( | 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 |
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 |
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 |
20130199198 | METHOD OF AUTOMATICALLY REGULATING AN AIRCRAFT POWER PLANT, A DEVICE, AND AN AIRCRAFT - A method of automatically regulating a power plant ( | 08-08-2013 |
20130199197 | DEVICE AND A METHOD FOR REGULATING A TURBINE ENGINE, AND AN AIRCRAFT - A regulator device ( | 08-08-2013 |
20130194140 | COMMUNICATION DEVICE, AN AIRCRAFT ROTOR, AND AN AIRCRAFT - A communication device ( | 08-01-2013 |
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 |
20130184958 | METHOD OF CONTROLLING A GROUP OF ENGINES, AND AN AIRCRAFT - A method of controlling a group ( | 07-18-2013 |
20130184903 | AIRCRAFT POWER PLANT, AN AIRCRAFT, AND A METHOD OF PILOTING SAID AIRCRAFT - An aircraft power plant ( | 07-18-2013 |
20130184902 | PILOTING ASSISTANCE METHOD, A PILOTING ASSISTANCE DEVICE, AND AN AIRCRAFT - A piloting assistance device ( | 07-18-2013 |
20130182449 | ROTORCRAFT HAVING LIGHTING EQUIPMENT WITH A PLURALITY OF HEADLIGHTS OPERATED FOR LANDING, WINCHING, AND SEARCHING - A rotorcraft ( | 07-18-2013 |
20130177422 | ROTOR BLADE AND AN AIRCRAFT - A rotor blade ( | 07-11-2013 |
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 |
20130175383 | ROTARY-WING AND FIXED-WING AIRCRAFT - An aircraft ( | 07-11-2013 |
20130168501 | PRIMARY FLIGHT CONTROLS - Primary flight controls ( | 07-04-2013 |
20130164143 | LAMINATED ABUTMENT, A ROTOR PROVIDED WITH SUCH AN ABUTMENT, AND AN AIRCRAFT - A laminated abutment ( | 06-27-2013 |
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 |
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 |
20130147242 | DEVICE FOR PROTECTING AN INDIVIDUAL SITTING ON A SEAT, A SEAT, AND A VEHICLE - A protection device ( | 06-13-2013 |
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 |
20130142658 | ROTOR BLADE | 06-06-2013 |
20130134256 | ANTI-TORQUE DEVICE WITH LONGITUDINAL THRUST FOR A ROTORCRAFT - A tail assembly ( | 05-30-2013 |
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 |
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 |
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 |
20130119187 | DEVICE FOR VARYING BLADE PITCH OF A LIFT ROTOR - The present invention relates to a device ( | 05-16-2013 |
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 |
20130106177 | DEVICE FOR FEEDING ELECTRICITY TO EQUIPMENT, THE DEVICE BEING INCORPORATED IN THE FLOOR OF AN AIRCRAFT CABIN | 05-02-2013 |
20130105749 | CONTROL MEANS FOR A LIFTER DEVICE, HOIST APPARATUS, AND AN AIRCRAFT | 05-02-2013 |
20130105625 | AIRCRAFT PROVIDED WITH A BUOYANCY SYSTEM FOR A ROTARY ELEMENT | 05-02-2013 |
20130105624 | LANDING GEAR, AN AIRCRAFT, AND A METHOD | 05-02-2013 |
20130093632 | AIRCRAFT ANTENNA, AND AN AIRCRAFT - The present invention relates to an antenna ( | 04-18-2013 |
20130087660 | DEVICE FOR ASSISTING THE PILOTING OF A ROTORCRAFT - A device for assisting the piloting of a rotorcraft, the rotorcraft having a flight control ( | 04-11-2013 |
20130082135 | HYBRID AIRCRAFT HAVING A ROTARY WING - An aircraft ( | 04-04-2013 |
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 |
20130078096 | SYSTEM FOR CONTROLLING PITCH VARIATION OF THE BLADES OF A PROPELLER, A PROPELLER, AND AN AIRCRAFT | 03-28-2013 |
20130078049 | SURFACE-AREA SAFETY MEANS AND A VEHICLE - Surface-area safety means ( | 03-28-2013 |
20120316832 | TECHNICAL METHOD, A MAINTENANCE DEVICE, AND AN AIRCRAFT - The present invention relates to a maintenance method for a piece of equipment ( | 12-13-2012 |
20120314034 | PILOTING ASSISTANCE SYSTEM AND AN AIRCRAFT - The present invention relates to a piloting assistance system ( | 12-13-2012 |
20120308384 | TWIST MECHANISM FOR TWISTING A ROTOR BLADE FOR A ROTORCRAFT, AND A BLADE - A twist mechanism for twisting a rotary-wing blade ( | 12-06-2012 |
20120303296 | METHOD OF DETERMINING THE STATIC FORCE DEVELOPED BY A SERVO-CONTROL - The present invention relates to a method of determining the static force developed by a servo-control ( | 11-29-2012 |
20120299450 | ELECTRICAL POWER SUPPLY DEVICE FOR ELECTRICALLY POWERING AT LEAST ONE ITEM OF EQUIPMENT ON A ROTARY ROTOR OF AN AIRCRAFT, AND AN AIRCRAFT - An electrical power supply device ( | 11-29-2012 |
20120298794 | AIRCRAFT PROVIDED WITH A DEVICE FOR REDUCING VIBRATION, AND A METHOD THEREFOR - An aircraft ( | 11-29-2012 |
20120296499 | DEVICE AND A METHOD FOR CONSTRUCTING A FLIGHT PATH IN ORDER TO REACH A DESTINATION | 11-22-2012 |
20120292430 | DEVICE FOR LAUNCHING AND RECOVERING A DRONE, AND AN ASSOCIATED AIRCRAFT | 11-22-2012 |
20120277969 | PASSING FROM A NON-SYNCHRONIZED STATE BETWEEN AN ENGINE AND A ROTOR TO A SYNCHRONIZED STATE - In order to regulate a power plant ( | 11-01-2012 |
20120269630 | ROTOR DAMPER DEVICE, AND AN ASSOCIATED ROTOR AND AIRCRAFT - A damper device ( | 10-25-2012 |
20120255386 | CONTROL LEVER FOR CONTROLLING A ROTARY WING, A MECHANICAL CONTROL SYSTEM INCLUDING SAID CONTROL LEVER, AND AN AIRCRAFT - A control lever ( | 10-11-2012 |
20120253560 | METHOD AND A DEVICE FOR ASSISTING THE PILOTING OF AN AIRCRAFT, AND AN AIRCRAFT - A method of assisting the piloting of an aircraft ( | 10-04-2012 |
20120248713 | WEATHERPROOF SURROUND FOR SAFELY JETTISONING A REMOVABLE PANEL - A weatherproof surround, for a jettisonable panel ( | 10-04-2012 |
20120241563 | EMERGENCY PILOTING BY MEANS OF A SERIES ACTUATOR FOR A MANUAL FLIGHT CONTROL SYSTEM IN AN AIRCRAFT - For emergency piloting of a manual flight control system ( | 09-27-2012 |
20120241434 | ELECTRICAL POWER SUPPLY DEVICE FOR A RESISTOR ELEMENT, AND AN ELECTRICAL SYSTEM PROVIDED WITH SAID DEVICE AND SAID RESISTOR ELEMENT - An electrical power supply device ( | 09-27-2012 |
20120234985 | CYCLIC STICK FOR MECHANICALLY TRANSMITTING COMMANDS FOR CONTROLLING A ROTORCRAFT, THE STICK HAVING A LEVER ARM THAT IS AMPLIFIED SELECTIVELY IN THE EVENT OF AN EMERGENCY - The invention provides a control mechanism for controlling flight of an aircraft, the control mechanism comprising a cyclic control stick ( | 09-20-2012 |
20120229325 | METHOD OF MEASURING HEIGHT AND DETECTING OBSTACLES, A RADIOALTIMETER, AND AN AIRCRAFT - A radioaltimeter ( | 09-13-2012 |
20120227325 | VEHICLE PANEL PROVIDED WITH A MOVABLE WINDOW, AND AN ASSOCIATED VEHICLE - A vehicle panel ( | 09-13-2012 |
20120221235 | METHOD OF OPTIMIZING THE LOADING OF LOADS IN A VEHICLE - A method of determining the locations of loads in a vehicle in such a manner as to ensure mission safety in terms of loads being retained in the aircraft. On the basis of vehicle parameters, the anchor points available in this type of vehicle for retaining the loads are identified. As a function of the available loading volume(s), a possible loading configuration is calculated using at least some of the available anchor points, at least some of the retaining means, and the characteristics of the loads. The forces that might be exerted on the selected anchor points are verified as being less than maximum limits. The calculated loading configuration is confirmed, otherwise a new loading configuration is calculated. | 08-30-2012 |
20120217368 | FASTENER DEVICE, A SEAT PROVIDED WITH SAID DEVICE, AND A VEHICLE - A fastener device ( | 08-30-2012 |
20120195767 | BLADE FOR A HELICOPTER ANTI-TORQUE DEVICE | 08-02-2012 |
20120195762 | BLADE AND METHOD OF FABRICATING SAID BLADE | 08-02-2012 |
20120195760 | LEAD-LAG DAMPER DEVICE - Damper device for damping relative movements of two elements of a mechanical system. The damper device comprises a damping chamber filled with a hydraulic fluid, a rod ( | 08-02-2012 |
20120193899 | PROTECTIVE DEVICE FOR PROTECTING AN OCCUPANT OF A VEHICLE, A SEAT, AND AN ASSOCIATED VEHICLE - A protective device ( | 08-02-2012 |
20120193476 | REMOVABLE FASTENER DEVICE EQUIPPED WITH ATTACHMENT MEANS FOR ATTACHING AN EXTERNAL LOAD AND WITH FASTENER MEANS FOR FASTENING SAID ATTACHMENT MEANS TO AN AIRCRAFT, AN ASSOCIATED AIRCRAFT, AND AN ASSOCIATED METHOD - A fastener device ( | 08-02-2012 |
20120179326 | PREDICTING TIME TO MAINTENANCE BY FUSION BETWEEN MODELING AND SIMULATION FOR ELECTRONIC EQUIPMENT ON BOARD AN AIRCRAFT - A method and system for predictive maintenance of electronic equipment on board an aircraft ( | 07-12-2012 |
20120160954 | AIRCRAFT PROVIDED WITH A SWIVELING TAIL ROTOR, AND AN ASSOCIATED METHOD - An aircraft ( | 06-28-2012 |
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 |
20120141288 | FABRICATING PARTS WITH COMPOSITE MATERIAL REINFORCEMENT HAVING A SINGLE CROSSING LINE - Method for fabricating a reinforcing coating for a part made of composite material. Pre-impregnated reinforcing fibers are used in the form of slivers and said slivers are laid on the part in two layers of longitudinal slivers by being placed thereon. This fabrication makes provision for using an angular orientation for the slivers of each layer respectively of 0° and of some other angle relative to said determined direction of the solid body for covering using an interlaced pattern type that gives layer crossing lines parallel to a longitudinal axis of the solid body for covering, which pattern type is selected to form interlacing patterns that limit the number of layer crossing lines along the longitudinal axis of the solid body for covering to a single line. | 06-07-2012 |
20120138739 | AIRCRAFT PROVIDED WITH A TAIL PLANE INCLUDING MEANS FOR COMBATING FLUTTER - An aircraft ( | 06-07-2012 |
20120138731 | ROTORCRAFT STRUCTURAL ELEMENT FOR REDUCING AERODYNAMIC DRAG - A fairing ( | 06-07-2012 |
20120132741 | METHOD OF CONTROLLING A BUOYANCY SYSTEM FOR AN AIRCRAFT, A BUOYANCY SYSTEM IMPLEMENTING SAID METHOD, AND AN AIRCRAFT - A buoyancy system ( | 05-31-2012 |
20120116613 | METHOD OF CONTROLLING AN OVERSPEED SAFETY SYSTEM FOR AEROENGINES AND A CONTROL CIRCUIT FOR IMPLEMENTING SAID METHOD - A method of controlling an overspeed safety system for an aircraft having at least two engines. The method includes setting said overspeed safety system for the engines, monitoring the speeds of rotation of the engines, detecting overspeed on one of the engines, shutting down the engine in question in the event of detecting overspeed, and inhibiting the operation of the overspeed safety system for the other engine(s) still in operation. The method also comprises the steps of monitoring safety parameters associated with the operation and/or the shutting down of the engine that has been shut down; and maintaining the inhibition or resetting the overspeed safety system for the other engine(s) still in operation, as a function of one or more safety parameters. | 05-10-2012 |
20120109426 | AIRCRAFT POWER PLANT, AN AIRCRAFT, AND A METHOD OF PILOTING SAID AIRCRAFT - A power plant ( | 05-03-2012 |
20120104152 | AIRCRAFT PROVIDED WITH HOIST MEANS, AND AN ASSOCIATED METHOD - An aircraft ( | 05-03-2012 |
20120080560 | SKID LANDING GEAR AND AN AIRCRAFT PROVIDED WITH SUCH LANDING GEAR - A landing gear ( | 04-05-2012 |
20120080558 | UNDERCARRIAGE, AN AIRCRAFT INCLUDING SAID UNDERCARRIAGE, AND A METHOD OF LANDING SAID AIRCRAFT - An undercarriage ( | 04-05-2012 |
20120077607 | FLEXIBLE COUPLING MEANS - A coupling means ( | 03-29-2012 |
20120075120 | STEPPED INSTRUMENT PANEL FOR AIRCRAFT - An instrument panel for a rotorcraft having two pilot seats, said instrument panel being arranged under an anti-glare shield ( | 03-29-2012 |
20120074262 | DE-ICING SYSTEM FOR A FIXED OR ROTARY AIRCRAFT WING - A de-icing system for a fixed or rotary aircraft wing, the system including means for generating ultrasound that is transmitted at least locally to an outside surface of the wing, which means comprise a base structure ( | 03-29-2012 |
20120070300 | BLADE WITH MINIMIZED VULNERABILITY | 03-22-2012 |
20120068015 | METHOD OF ACTIVATING PROTECTION MEANS FOR PROTECTING AN OCCUPANT OF AN AIRCRAFT, AND AN AIRCRAFT IMPLEMENTING SAID METHOD - A method of activating protection means ( | 03-22-2012 |
20120068007 | ROTARY WING AIRCRAFT PROVIDED WITH PROPULSION MEANS, AND A METHOD APPLIED BY SAID AIRCRAFT - An aircraft ( | 03-22-2012 |
20120043420 | SKID UNDERCARRIAGE AND A METHOD OF PREVENTING A ROTORCRAFT PROVIDED WITH SUCH AN UNDERCARRIAGE FROM TILTING - An undercarriage ( | 02-23-2012 |
20120031544 | METHOD OF FABRICATING A SPAR FOR A ROTORCRAFT BLADE - A method of forming a rotorcraft blade is provided. A first support shaft ( | 02-09-2012 |
20120025032 | ELECTRICAL ARCHITECTURE FOR A ROTARY WING AIRCRAFT WITH A HYBRID POWER PLANT - A hybrid power plant ( | 02-02-2012 |
20120022835 | METHOD AND A DEVICE FOR SYNTHESIZING AN ELECTRICAL AND ELECTRONIC ARCHITECTURE - A device for synthesizing an electrical and electronic architecture ( | 01-26-2012 |
20120018570 | METHOD OF MINIMIZING THE ATTITUDE HUMP PHENOMENON AND A ROTARY WING AIRCRAFT PROVIDED WITH STABILIZER MEANS THEREFOR - A method of minimizing the attitude hump phenomenon relating to a rotary wing aircraft ( | 01-26-2012 |
20120016580 | PILOTING ASSISTANCE METHOD FOR AIRCRAFT - The present invention relates to a piloting assistance method for an aircraft, the method consisting in using data from at least one active telemeter sensor (A) in order to construct a sensor safety cordon (B) for avoiding the terrain and obstacles that are overflown. The method; | 01-19-2012 |
20120012693 | METHOD AND AN AIRCRAFT PROVIDED WITH A SWIVELING TAIL ROTOR - A method of piloting an aircraft ( | 01-19-2012 |
20120011840 | SERVO-CONTROL PROVIDED WITH A LIMIT FORCE DETECTOR DEVICE - The present invention relates to a servo-control ( | 01-19-2012 |
20120008697 | COMMUNICATIONS NETWORK THAT IS DISTRIBUTED, MODULAR, AND CONFIGURABLE FOR AN ON-BOARD AVIONICS SYSTEM - A communications network for an on-board avionics system for conveying information between at least one on-board computer ( | 01-12-2012 |
20120006934 | METHOD AND A ROTARY WING AIRCRAFT THAT ARE OPTIMIZED SO AS TO MINIMIZE THE CONSEQUENCES FOR THE OCCUPANTS OF SAID AIRCRAFT OF AN OFF-SPECIFICATION EMERGENCY LANDING - A method of minimizing the consequences for the occupants of a rotary wing aircraft ( | 01-12-2012 |
20110319008 | METHOD OF AVOIDING A GRID CLOGGING, A GRID AND AN AIR INTAKE IMPLEMENTING SUCH A METHOD - The present invention relates to an air intake grid ( | 12-29-2011 |
20110315271 | DEVICE FOR FILLING A TANK BY GRAVITY OR UNDER PRESSURE - The present invention relates to a filler device ( | 12-29-2011 |
20110313703 | INERTIAL MEASUREMENT DEVICE AND AN AIRCRAFT INCLUDING SUCH A DEVICE - The present invention relates to an inertial measurement device secured to a structure of a vehicle for which it is desired to measure speeds and/or accelerations, the device comprising at least one piece of moving equipment in rotation about a stationary axis of rotation Y relative to the structure, said moving equipment including at least two measurement means having respective sensitivity axes X′ and Z′ that are mutually orthogonal and that lie in a plane perpendicular to the stationary axis of rotation Y, a motor for driving the moving equipment in rotation, means for determining the angular position of the moving equipment, means for responding to the angular position of the moving equipment to determine the projection of the measurements taken in the rotary frame of reference axes X′ and Z′ by the said at least two measurement means onto a vehicle frame of reference X and Z. | 12-22-2011 |
20110308905 | DEVICE FOR DAMPING THE VIBRATION OF A STRUCTURE - The present invention relates to a device ( | 12-22-2011 |
20110307125 | METHOD OF MONITORING THE EFFECTIVENESS OF A DAMPER, AND A DEVICE FOR IMPLEMENTING SAID METHOD - The present invention relates to a method of monitoring the effectiveness of a damper system, wherein the method consists in measuring the relative movements of two strength members, in filtering the measurements in order to isolate those that relate to the lead-lag resonant frequency of the blade, in rectifying the signal, in recording the signal, in comparing the rectified signal (S) with a threshold value (S | 12-15-2011 |
20110290942 | ELECTRICAL POWER SUPPLY AND CONTROL DEVICE FOR EQUIPMENT OF A ROTOR, AND AN AIRCRAFT FITTED WITH SUCH A DEVICE - The present invention relates to an electrical power supply and control device ( | 12-01-2011 |
20110290774 | HANDLING AN INSERT TO IMPLANT IT IN A CELLULAR PANEL AND TO WITHDRAW IT FROM THE PANEL - Tooling is organized firstly to implant an insert ( | 12-01-2011 |
20110290200 | AIRCRAFT POWER PLANT, AN AIRCRAFT, AND A METHOD OF USING A PISTON ENGINE IN A POWER PLANT HAVING A CONVENTIONAL GEARBOX - The present invention relates to a power plant ( | 12-01-2011 |
20110284688 | ROTOR PROVIDED WITH A DEVICE FOR PROTECTING IT AGAINST LIGHTNING, AND AN AIRCRAFT PROVIDED WITH SUCH A ROTOR | 11-24-2011 |
20110276232 | METHOD OF CONTROLLING A BUOYANCY SYSTEM FOR AN AIRCRAFT, AND A CONTROL SYSTEM IMPLEMENTING SAID METHOD - The present invention relates to a method of controlling a buoyancy system for an aircraft, wherein the buoyancy system including automatic trigger means and the method consists in:
| 11-10-2011 |
20110276202 | SIMPLIFIED FLIGHT CONTROL SYSTEM INCLUDING A DECLUTCHABLE FRICTION DEVICE - The present invention relates to a friction device ( | 11-10-2011 |
20110273324 | CONTINUOUS HIGH-ACCURACY LOCATING METHOD AND APPARATUS - Method and apparatus for locating an object ( | 11-10-2011 |
20110268573 | DEVICE FOR REDUCING THE VIBRATION GENERATED BY A ROTORCRAFT LIFT ROTOR, AND A ROTOR HUB PROVIDED WITH SUCH A DEVICE | 11-03-2011 |
20110260001 | LANDING GEAR PROVIDED WITH ENERGY ABSORBER MEANS, AN AIRCRAFT PROVIDED WITH SAID LANDING GEAR, AND A METHOD OF LANDING - Aircraft landing gear ( | 10-27-2011 |
20110260000 | ENERGY ABSORBER SYSTEM FOR AN UNDERCARRIAGE, AND AN AIRCRAFT PROVIDED WITH SAID ENERGY ABSORBER SYSTEM - An energy absorber system ( | 10-27-2011 |
20110246975 | CONTROL ARCHITECTURE AND PROCESS FOR PORTING APPLICATION SOFTWARE FOR EQUIPMENT ON BOARD AN AIRCRAFT TO A CONSUMER STANDARD COMPUTER HARDWARE UNIT - The software unit arrangement method is a step of developing a standardized software-hardware abstraction software layer ( | 10-06-2011 |
20110236209 | BLADE DAMPER, AND A ROTOR FITTED WITH SUCH A DAMPER - The present invention relates to a damper ( | 09-29-2011 |
20110236208 | ROTARY WING BLADE, A ROTARY WING INCLUDING SUCH A BLADE, AND AN AIRCRAFT | 09-29-2011 |
20110234425 | ADAPTING SELECTIVE TERRAIN WARNINGS AS A FUNCTION OF THE INSTANTANEOUS MANEUVERABILITY OF A ROTORCRAFT - A method of generating a terrain avoidance warning for a rotary wing aircraft including generating an avoidance trajectory including a proximal segment representative of a transfer time and an avoidance curve including at least one distal segment of a conic section curve following on from the proximal segment, wherein the proximal segment extends in continuation from a predicted trajectory over a distance representing an applicable reaction time, the applicable reaction time being minimized as a function of a route sheet for the aircraft, and wherein the generating includes calculating the at least one distal segment as a function of an instantaneous maneuverability of the aircraft. | 09-29-2011 |
20110230304 | MECHANICAL ASSEMBLY PROVIDED WITH MEANS FOR MONITORING FOR A STRUCTURAL ANOMALY, A GEARBOX PROVIDED WITH SUCH A MECHANICAL ASSEMBLY, AND A METHOD OF MONITORING FOR A STRUCTURAL ANOMALY - The present invention relates to a mechanical assembly ( | 09-22-2011 |
20110225212 | METHOD AND A DEVICE FOR FLYING SAFELY AT LOW ALTITUDE IN AN AIRCRAFT - The present invention relates to a method of flying safely and at low altitude in an aircraft, in which method unsafe relief (R | 09-15-2011 |
20110211959 | BLADE WITH ADAPTIVE TWISTING, AND A ROTOR PROVIDED WITH SUCH A BLADE - A rotor blade ( | 09-01-2011 |
20110208973 | OVERALL OPTIMIZATION OF THE CONFIGURATION OF A MESHED WIRELESS NETWORK OF RF DEVICES IN AN AIRCRAFT - The invention relates to overall optimization of an identification system ( | 08-25-2011 |
20110204685 | ANTI-CRASH SEAT FOR A VEHICLE - An anti-crash seat ( | 08-25-2011 |
20110204182 | ROTARY WING AIRCRAFT PROVIDED WITH AN EMERGENCY UNDERCARRIAGE - A rotary wing aircraft ( | 08-25-2011 |
20110203718 | METHOD OF FABRICATING A HONEYCOMB STRUCTURED PANEL - A method of fabricating a panel ( | 08-25-2011 |
20110190964 | TURNING-STABILIZED ESTIMATION OF THE ATTITUDE ANGLES OF AN AIRCRAFT - The present invention relates to estimating the attitude angles of an aircraft ( | 08-04-2011 |
20110186686 | REMOVABLE SUPPORT FOR OPTIONAL EXTERNAL EQUIPMENT ON AN AIRCRAFT, AND AN AIRCRAFT PROVIDED WITH SUCH A SUPPORT - The present invention relates to a removable support ( | 08-04-2011 |
20110180663 | METHOD AND A DEVICE FOR DRAINING A TANK, AND A TANK AND AN AIRCRAFT FITTED WITH SUCH A DEVICE - The present invention relates to a method of draining a tank ( | 07-28-2011 |
20110174929 | LOCKING DEVICE FOR LOCKING A STRUCTURAL ELEMENT AGAINST AN ADJACENT STRUCTURE, AN AIRCRAFT PROVIDED WITH SAID DEVICE, AND AN EXTRACTION METHOD IMPLEMENTED BY SAID DEVICE - The present invention relates to a locking device provided with a latch ( | 07-21-2011 |
20110155848 | AIRCRAFT UNDERCARRIAGE HAVING A ROCKER LEVER WITH A SWIVEL AND A HINGED TWIN WHEELS - The invention relates to an aircraft undercarriage ( | 06-30-2011 |
20110155841 | VIBRATION DAMPER MECHANISM, AND A FLYING MACHINE INCLUDING A CARRIER STRUCTURE AND A ROTOR PROVIDED WITH SUCH A MECHANISM - The present invention provides a mechanism ( | 06-30-2011 |
20110151133 | METHOD OF FABRICATING A PAINTED SUBSTRATE THAT IS ELECTRICALLY NON-CONDUCTIVE - The present invention relates to a method of fabricating a painted substrate ( | 06-23-2011 |
20110147512 | ROTOR CARRIER STRUCTURE, A FLYING MACHINE PROVIDED WITH SUCH A CARRIER STRUCTURE, AND A METHOD OF AVOIDING UNSTABLE COUPLING BETWEEN RESONANT VIBRATION MODES - The invention provides a carrier structure ( | 06-23-2011 |
20110144942 | METHOD OF USING TELEMETRY TO DETECT AT LEAST ONE SUSPENDED THREADLIKE OBJECT, THE OBJECT LYING IN THE DETECTION FIELD OF A TELEMETER MOUNTED ON BOARD A VEHICLE - A method of detecting at least one suspended threadlike object by telemetry, the object lying in the detection field of a telemeter on board a vehicle. The method wherein in step iii), for each vertical plane taken into consideration, and for each set of at least four candidate points close to the vertical plane in question, using the least squares method to calculate the values of three parameters a, b, and c of a catenary having an equation of the form: | 06-16-2011 |
20110138817 | METHOD OF INCREASING THE SAFETY OF A POWER PLANT, AND A POWER PLANT SUITABLE FOR IMPLEMENTING THE METHOD - The present invention relates to a method of increasing the safety of a power plant ( | 06-16-2011 |
20110137497 | AIRCRAFT PROVIDED WITH A DEVICE FOR ASSISTING THE PILOT WHEN CARRYING AN EXTERNAL LOAD WITH A SLING, AND A METHOD IMPLEMENTED BY SAID DEVICE - The present invention relates to an aircraft ( | 06-09-2011 |
20110130895 | METHOD OF OBTAINING A LOCAL TERRAIN ELEVATION DATABASE FROM DETECTOR MEANS ON BOARD A VEHICLE - A method essentially comprising a step of storing each plot mesh. Each plot mesh receiving plots sent thereto by detector means and retaining in memory at least the altitude of the highest plot and the number of plots neighboring said highest plot in said mesh. The altitude and the number of plots neighboring are updated each time a new plot is sent to the plot mesh. A step of rejecting plot meshes is presenting a number of neighboring plots that is less than a predetermined rejection threshold value. The rejection threshold value is a function of the position of the mesh relative to the detector means. A step is preparing the local terrain elevation database from the plot meshes (M(i,j)) that are not rejected. | 06-02-2011 |
20110127377 | TAIL SKID FOR PROTECTING A STRUCTURAL ELEMENT OF AN AIRCRAFT, AN AIRCRAFT PROVIDED WITH SUCH A TAIL SKID, AND AN ANTI-OVERTURNING METHOD IMPLEMENTED BY SAID TAIL SKID - The present invention relates to a tail skid ( | 06-02-2011 |
20110121127 | POWER PLANT, A HELICOPTER INCLUDING SUCH A POWER PLANT, AND A METHOD IMPLEMENTED BY SAID POWER PLANT - The present invention relates to a power plant ( | 05-26-2011 |
20110115131 | METHOD FOR MANUFACTURING ELECTRICALLY NON-CONDUCTIVE PAINTED SUBSTRATE - The present invention relates to a method of fabricating a painted substrate ( | 05-19-2011 |
20110114798 | LONG-RANGE AIRCRAFT WITH HIGH FORWARD SPEED IN CRUISING FLIGHT - The present invention relates to an aircraft ( | 05-19-2011 |
20110108676 | AIR INLET FOR AN AIRCRAFT TURBINE ENGINE, AN AIRCRAFT PROVIDED WITH SUCH AN AIR INLET, AND A METHOD OF OPTIMIZING THE OPERATION OF AN AIRCRAFT TURBINE ENGINE WITH THE HELP OF AN AIR INLET - The present invention relates to an air inlet ( | 05-12-2011 |
20110097208 | SET OF CYCLIC SWASHPLATES FOR CONTROLLING THE PITCH OF BLADES OF A MAIN ROTOR, AND A ROTOR PROVIDED WITH SUCH A SET | 04-28-2011 |
20110097193 | DEVICE FOR REDUCING VIBRATION GENERATED BY ROTORCRAFT ROTOR, AND ROTORCRAFT PROVIDED WITH SUCH DEVICE | 04-28-2011 |
20110095572 | HONEYCOMB-STRUCTURED FLOOR PANEL FOR A VEHICLE, THE PANEL INCORPORATING A FASTENER ELEMENT FOR FASTENING EQUIPMENT OF THE VEHICLE - The invention provides a laminated floor panel for a vehicle cabin. The panel comprises a core ( | 04-28-2011 |
20110095132 | FILTER MECHANISM FOR FILTERING THE VIBRATION TO WHICH EQUIPMENT IS SUBJECTED IN A MOVING AIRCRAFT, IN PARTICULAR A ROTORCRAFT - The invention provides a vibration filter mechanism for aircraft equipment. A weighted lever arm ( | 04-28-2011 |
20110085889 | MECHANISM FOR ATTENUATING TORQUE PULSATIONS BETWEEN AN ENGINE AND A ROTORCRAFT ROTOR DRIVEN BY THE ENGINE - The invention provides a mechanism for attenuating torque pulsations between an engine ( | 04-14-2011 |
20110079681 | SEAT FOR POWERED AIRCRAFT, THE SEAT INCORPORATING MEANS FOR PROTECTING ITS PASSENGER IN THE EVENT OF A CRASH - A seat for a powered aircraft, the seat comprising a bucket ( | 04-07-2011 |
20110071709 | HIGHLY REPRESENTATIVE REAL-TIME SIMULATION OF AN AVIONICS SYSTEM - Optionally-mixed highly representative real time simulation of at least part of an avionics system ( | 03-24-2011 |
20110071708 | ASSISTED PILOTING METHOD AND DEVICE FOR AN AIRCRAFT FOR USE IN THE EVENT OF A FIRST LIMIT INDICATOR BREAKING DOWN - An assisted piloting method for an aircraft having at least two engines ( | 03-24-2011 |
20110052395 | FREQUENCY ADAPTER AND RETURN MEANS SUITABLE FOR BEING ARRANGED IN SUCH A FREQUENCY ADAPTER - A frequency adapter ( | 03-03-2011 |
20110049295 | REUSABLE ROTORCRAFT BUMPER, AND A ROTORCRAFT HAVING SUCH A BUMPER - A reusable bumper ( | 03-03-2011 |
20110047711 | FASTENER TOOL FOR FASTENING A TRANSMISSION SHAFT, AND A BALANCING BENCH INCLUDING SUCH A TOOL - The present invention relates to a fastener tool ( | 03-03-2011 |
20110031346 | METHOD OF ASSISTING PILOTING, PILOTING ASSISTANCE MEANS, AND A PILOTING ASSISTANCE DEVICE FOR A ROTORCRAFT USING SAID PILOTING ASSISTANCE MEANS TO IMPLEMENT SAID PILOTING ASSISTANCE METHOD - The present invention relates to a device and method of assisting the piloting of a rotorcraft, the rotorcraft having a flight control ( | 02-10-2011 |
20110027082 | METHOD OF REDUCING OR EVEN ELIMINATING THE VIBRATION OF A ROTORCRAFT LIFT AND PROPULSION ROTOR, AND AN AIRFOIL ASSEMBLY AND A ROTOR IMPLEMENTING SAID METHOD - The present invention relates to a method of reducing the vibration of a lift and propulsion rotor ( | 02-03-2011 |
20110024551 | VARIABLE DAMPING OF HAPTIC FEEDBACK FOR A FLIGHT-ATTITUDE CHANGING LINKAGE OF AN AIRCRAFT - The present invention relates to haptic feedback for operating at least one manual flight control device ( | 02-03-2011 |
20110020592 | INSULATING COATING WITH MASS AMPLIFICATION - An insulating coating ( | 01-27-2011 |
20100332123 | METHOD OF ASSISTING PILOTING AT LOW ALTITUDE - A method of assisting the piloting of an aircraft ( | 12-30-2010 |
20100331438 | STRIPPING COMPOSITION FOR A MOLD FOR MAKING A COMPOSITE MATERIAL PART, AND METHOD OF PREPARING - A stripping composition, and a method of making the stripping composition. The stripping composition including 100 parts by weight of a base ingredient consisting in epoxy polydimethylsiloxane, 0.5 to 10 parts by weight of a polymerization agent for polymerizing the base ingredient and constituted by a diaryliodonium salt, not more than 30 parts by weight of an anti-adhesion modulator constituted by a silicone polymer; and not more than 40 parts by weight of an anti-stick agent making the composition less tacky prior to polymerization and constituted by at least one vinyl ether compound. | 12-30-2010 |
20100319357 | DEVICE AND A METHOD FOR STARTING A TURBINE ENGINE FITTED TO A HELICOPTER, MAKING USE OF AN ELECTRICAL ENERGY SOURCE THAT INCLUDES DISCHARGE BOOSTER MEMBERS - The invention provides a device and a method for starting at least one turbine engine ( | 12-23-2010 |