Bordes
France
137
2017-05-11
113
2019-12-17
These are the the leading inventors for applications assigned to TURBOMECA:
TURBOMECA based in Bordes, FR has been assigned the rights to these inventions. The list includes both Pending Applications and Patent Grants:
Turbine engine assembly for measuring the vibrations to which a rotating blade is subjected
#2 | 2017-02-09AIRCRAFT ENGINE COMPRISING AZIMUTH SETTING OF THE DIFFUSER WITH RESPECT TO THE COMBUSTION CHAMBER
#3 | 2017-01-05ENDOSCOPE AND METHOD FOR USING SAME
#4 | 2017-01-05 β Patent 10,450,962 granted on 2019-10-22Method and a system for reliably starting a turbine engine
#5 | 2016-11-03 β Patent 10,921,179 granted on 2021-02-16Assembly for turbine engine for measuring vibrations sustained by a rotating blade
#6 | 2016-11-03 β Patent 11,313,047 granted on 2022-04-26Method of treatment against corrosion and against wear
#7 | 2016-10-27 β Patent 10,539,077 granted on 2020-01-21Device for draining liquids for an aircraft engine
#8 | 2016-10-13 β Patent 10,858,946 granted on 2020-12-08Bladed rotor
#9 | 2016-09-29 β Patent 10,428,739 granted on 2019-10-01Self-contained power unit for implementing a method for optimizing the operability of an aircraft propulsive unit
#10 | 2016-09-22 β Patent 10,029,799 granted on 2018-07-24Air conditioning method and system for aircraft
#11 | 2016-08-18 β Patent 10,753,280 granted on 2020-08-25Turbomachine designed to operate in turning gear mode
#12 | 2016-08-11 β Patent 10,054,053 granted on 2018-08-21Turbomachine designed to operate in turning gear mode
#13 | 2016-08-11 β Patent 9,945,246 granted on 2018-04-17Monitoring of a degree of coking at dynamic seals by a starter
#14 | 2016-08-04 β Patent 10,100,743 granted on 2018-10-16Ignition device for an aircraft engine
#15 | 2016-08-04 β Patent 10,107,133 granted on 2018-10-23Method for the monitoring of a degree of coking at seals by a gas generator shaft
#16 | 2016-06-30 β Patent 10,010,976 granted on 2018-07-03Laser welding head and process
#17 | 2016-05-26 β Patent 9,500,137 granted on 2016-11-22Method for optimizing the control of a free turbine power package for an aircraft, and control for implementing same
#18 | 2016-05-05 β Patent 9,748,060 granted on 2017-08-29Hybrid cutoff member for an electric circuit
#19 | 2016-04-28 β Patent 9,869,621 granted on 2018-01-16Test bench combining high-frequency tribological stress and oligocyclic fatigue, on a blade disk of turboshaft engine of an aircraft including a test piece having a portion with a shape of a blade root of a rotor and is engaged in a groove shape complementary to another test piece
#20 | 2016-03-24 β Patent 9,810,612 granted on 2017-11-07Oligocyclic fatigue or oligocyclic and polycyclic fatigue test rig
#21 | 2016-03-10DEVICE FOR WASHING A TURBOMACHINE AIR INTAKE CASING
#22 | 2016-02-25 β Patent 9,890,792 granted on 2018-02-13Radial or mixed-flow compressor diffuser having vanes
#23 | 2016-01-28 β Patent 10,138,734 granted on 2018-11-27Turbine ring for a turbomachine
#24 | 2016-01-21METERING DEVICE FOR A FUEL FEED CIRCUIT OF AN ENGINE
#25 | 2015-12-31 β Patent 10,145,262 granted on 2018-12-04Method for monitoring a degree of clogging of the starting injectors of a turbine engine
#26 | 2015-12-31BROACH AND METHOD FOR BROACHING SLOTS FOR PARTS SUCH AS TURBINE ROTOR DISKS OR TURBOMACHINE COMPRESSOR DISKS
#27 | 2015-11-19 β Patent 10,247,192 granted on 2019-04-02Sealing assembly for turbomachine
#28 | 2015-11-05 β Patent 10,087,838 granted on 2018-10-02Device and method for temporarily increasing power
#29 | 2015-10-01 β Patent 10,352,179 granted on 2019-07-16Compression assembly for a turbine engine
#30 | 2015-09-24 β Patent 10,329,928 granted on 2019-06-25Rotor-stator assembly for a gas turbine engine
#31 | 2015-09-17 β Patent 9,927,125 granted on 2018-03-27Two-circuit injector for a turbine engine combustion chamber
#32 | 2015-09-17 β Patent 9,534,539 granted on 2017-01-03Supply and drain device for an injector
#33 | 2015-09-03 β Patent 10,054,056 granted on 2018-08-21Turbine engine combustion assembly with a variable air supply
#34 | 2015-08-20 β Patent 9,758,238 granted on 2017-09-12Accessory drive gearbox for controlling the flaps of an aircraft
#35 | 2015-08-06 β Patent 9,423,330 granted on 2016-08-23Method of determining the non-propagation threshold of fatigue cracks at high frequency
#36 | 2015-07-30 β Patent 9,874,149 granted on 2018-01-23Method and system for starting an aircraft turboengine
#37 | 2015-07-23 β Patent 9,561,949 granted on 2017-02-07Filler device for a fluid tank
#38 | 2015-07-02 β Patent 10,100,742 granted on 2018-10-16Drainage method and purge collector of a carburation system of a helicopter
#39 | 2015-06-25 β Patent 9,689,313 granted on 2017-06-27Dual-circuit modular injection tube
#40 | 2015-06-18 β Patent 10,071,813 granted on 2018-09-11Helicopter engine air intake with increased bypass flow
#41 | 2015-05-28 β Patent 10,301,035 granted on 2019-05-28Method and configuration for an auxiliary power engine to deliver propulsive and/or non-propulsive energy in a helicopter architecture
#42 | 2015-05-14 β Patent 10,072,580 granted on 2018-09-11Method and system for the emergency start-up of an energy generator set
#43 | 2015-05-07 β Patent 10,059,460 granted on 2018-08-28Method and architecture for the optimized transfer of power between an auxiliary power motor and the main engines of a helicopter
#44 | 2015-03-26 β Patent 9,829,005 granted on 2017-11-28Centrifugal compressor provided with a marker for measuring wear and a method of monitoring wear using said marker
#45 | 2015-01-01 β Patent 9,915,173 granted on 2018-03-13Bearing support for a hot section of a turboshaft engine, and an associated turboshaft engine
#46 | 2014-12-25 β Patent 9,926,809 granted on 2018-03-27Method for discharging exhaust gas from a gas turbine and exhaust assembly having optimised configuration
#47 | 2014-10-09 β Patent 9,315,274 granted on 2016-04-19Method and system for regulating power in the event of at least one aircraft engine failure
#48 | 2014-10-09 β Patent 9,546,599 granted on 2017-01-17Turbine engine comprising an electrically activated fuel supply pump, and turbine engine fuel supply method
#49 | 2014-10-02 β Patent 9,302,775 granted on 2016-04-05Method and architecture for recovery of energy in an aircraft
#50 | 2014-09-18 β Patent 10,551,064 granted on 2020-02-04Annular wall of a combustion chamber with improved cooling at the level of primary and/or dilution holes
#51 | 2014-08-07PINION VIBRATION DAMPING USING VISCOELASTIC PATCH
#52 | 2014-07-31 β Patent 10,156,358 granted on 2018-12-18Combustion chamber wall
#53 | 2014-07-24 β Patent 9,558,450 granted on 2017-01-31System for recommending helicopter engine maintenance
#54 | 2014-05-29VARIABLE-PITCH NOZZLE FOR A RADIAL TURBINE, IN PARTICULAR FOR AN AUXILIARY POWER SOURCE TURBINE
#55 | 2014-05-22 β Patent 9,592,907 granted on 2017-03-14Device for electrically powering an aircraft on the ground
#56 | 2014-05-15METHOD OF DIFFUSING A GAS TURBINE COMPRESSION STAGE, AND DIFFUSION STAGE FOR IMPLEMENTING SAME
#57 | 2014-05-08 β Patent 9,683,576 granted on 2017-06-20Centrifugal compressor impeller
#58 | 2014-05-08 β Patent 9,580,179 granted on 2017-02-28Air conditioning system for an aircraft passenger compartment
#59 | 2014-05-08 β Patent 9,988,987 granted on 2018-06-05Method of starting a turbomachine while reducing thermal unbalance
#60 | 2014-05-01 β Patent 9,677,505 granted on 2017-06-13Method for injecting fuel into a combustion chamber of a gas turbine, and injection system for implementing same
#61 | 2014-04-24 β Patent 9,964,033 granted on 2018-05-08Two-spool design for a turboshaft engine with a high-pressure compressor connected to a low-pressure turbine
#62 | 2014-04-24 β Patent 8,925,331 granted on 2015-01-06Annular combustion chamber of a turbomachine
#63 | 2014-04-17 β Patent 9,618,008 granted on 2017-04-11Gas turbine diffuser blowing method and corresponding diffuser
#64 | 2014-03-27 β Patent 9,555,752 granted on 2017-01-31Method for rationalising a chain of electrical components of an aircraft, implementation architecture and corresponding aircraft
#65 | 2014-03-20METHOD AND DEVICE FOR SUPPLYING A LUBRICANT
#66 | 2014-02-13 β Patent 9,206,859 granted on 2015-12-08Mechanical protection device
#67 | 2014-01-02 β Patent 9,938,902 granted on 2018-04-10Turbomachine comprising a privileged injection device and corresponding injection method
#68 | 2013-12-12 β Patent 9,032,776 granted on 2015-05-19Method for calibrating a torsion torquemeter
#69 | 2013-11-21 β Patent 9,347,667 granted on 2016-05-24Injector for the combustion chamber of a gas turbine having a dual fuel circuit, and combustion chamber provided with at least one such injector
#70 | 2013-11-14DEVICE AND METHOD FOR MONITORING A ROTOR
#71 | 2013-11-07 β Patent 9,518,512 granted on 2016-12-13Method for starting a turbomachine
#72 | 2013-10-24MECHANICAL PROTECTION METHOD AND DEVICE
#73 | 2013-10-24 β Patent 10,138,756 granted on 2018-11-27Method for damping a gas-turbine blade, and vibration damper for implementing same
#74 | 2013-09-19 β Patent 8,783,729 granted on 2014-07-22Coupling system including a safety fastener device
#75 | 2013-09-12 β Patent 8,866,318 granted on 2014-10-21Method for controlling the generation of electricity applied to an aircraft gas turbine, and device implementing such a method
#76 | 2013-08-29METHOD OF OPTIMIZING THE SPECIFIC FUEL CONSUMPTION OF A TWIN ENGINE HELICOPTER AND TWIN ENGINE ARCHITECTURE WITH CONTROL SYSTEM FOR IMPLEMENTING IT
#77 | 2013-08-15 β Patent 9,114,883 granted on 2015-08-25System for real time simulation of the environment of an aeroengine
#78 | 2013-08-15 β Patent 9,238,975 granted on 2016-01-19Lubricating device having a bypass valve
#79 | 2013-08-08 β Patent 9,409,228 granted on 2016-08-09Method for attaching the cover of a centrifugal compressor of a turbine engine, compressor cover implementing same and compressor assembly provided with such a cover
#80 | 2013-06-13 β Patent 9,303,566 granted on 2016-04-05Method for optimizing the control of a free turbine power package for an aircraft, and control for implementing same
#81 | 2013-06-13 β Patent 8,868,262 granted on 2014-10-21Method for optimizing the overall energy efficiency of an aircraft, and main power package for implementing same
#82 | 2013-06-06 β Patent 9,429,038 granted on 2016-08-30Method for mounting shielding on a turbine casing, and mounting assembly for implementing same
#83 | 2013-06-06 β Patent 9,404,419 granted on 2016-08-02Method for optimizing the operability of an aircraft propulsive unit, and self-contained power unit for implementing same
#84 | 2013-05-30 β Patent 8,459,699 granted on 2013-06-11Coupling system including a safety fastener device
#85 | 2013-05-23 β Patent 9,551,234 granted on 2017-01-24Device for controlling pivotable vanes of a turbo-machine
#86 | 2013-05-16 β Patent 9,162,304 granted on 2015-10-20Method for the induction brazing of parts having complex shapes, and single or multiple brazing station for implementing same
#87 | 2013-04-25 β Patent 9,422,863 granted on 2016-08-23Method and architecture for recombining the power of a turbomachine
#88 | 2013-04-25DETECTION OF THE OVERSPEED OF A FREE TURBINE BY MEASURING USING A TORQUE METER
#89 | 2013-04-11 β Patent 10,336,442 granted on 2019-07-02Non-lubricated architecture for a turboshaft engine
#90 | 2013-04-11 β Patent 8,777,490 granted on 2014-07-15Method for dynamically absorbing shocks in a power shaft, in particular a supercritical shaft, and shock-absorbing architecture for implementing said method
#91 | 2013-04-11 β Patent 9,500,128 granted on 2016-11-22Heat-exchange architecture built into the exhaust of a turbine engine
#92 | 2013-03-14 β Patent 8,806,926 granted on 2014-08-19Device for multipoint acquisition/distribution of fluid, in particular probe for tapping pressure in a turbomachine air inlet
#93 | 2013-02-28 β Patent 9,506,652 granted on 2016-11-29Multi-pierced combustion chamber with counter-rotating tangential flows
#94 | 2013-02-07METHOD FOR ADAPTING THE AIR FLOW OF A TURBINE ENGINE HAVING A CENTRIFUGAL COMPRESSOR AND DIFFUSER FOR IMPLEMENTING SAME
#95 | 2013-01-03 β Patent 8,701,822 granted on 2014-04-22Gas-guiding pipe comprising a noise-attenuating covering with variable porosity
#96 | 2013-01-03DEVICE FOR EJECTING GAS FROM A GAS TURBINE ENGINE AND GAS TURBINE ENGINE
#97 | 2012-12-20 β Patent 9,163,526 granted on 2015-10-20Vertical shaft turbomachine
#98 | 2012-12-20 β Patent 9,194,253 granted on 2015-11-24Flexible rear bearing mounting, having an abutment, for a turbine engine
#99 | 2012-11-22 β Patent 9,188,338 granted on 2015-11-17Injector device and combustion chamber for a turbomachine provided with such injector device
#100 | 2012-10-11METHOD FOR COOLING TURBINE STATORS AND COOLING SYSTEM FOR IMPLEMENTING SAID METHOD
Also check out Turbomeca's (Bordes, France) applicant profile with 34 patent applications submitted.
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