Inventor · disambiguated record
Patrick Marconi
Also filed as: MARCONI PATRICK
10 granted patents·5 pending applications·50 citations·filing 2007–2020
86Inventor score
Files withSAFRAN HELICOPTER ENGINES7TURBOMECA3BEDRINE OLIVIER1MARCONI PATRICK1SAFRAN AIRCRAFT ENGINES1
Top patents by PatentIndex Score
15 records- 0189US11459960B2Method for checking the maximum available power of a turbine engine of an aircraft equipped with two turbine enginesSAFRAN HELICOPTER ENGINES·Filed 2018·Granted Oct 4, 2022·9 cites·12 claims
- 0285US10415482B2Turboshaft engine comprising a controlled mechanical coupling device, helicopter equipped with such a turboshaft engine, and method for optimising the zero-power super-idle speed of such a helicopterSAFRAN HELICOPTER ENGINES·Filed 2015·Granted Sep 17, 2019·5 cites·11 claims
- 0382US10059460B2Method and architecture for the optimized transfer of power between an auxiliary power motor and the main engines of a helicopterSAFRAN POWER UNITS·Filed 2013·Granted Aug 28, 2018·11 cites·12 claims
- 0477US9422863B2Method and architecture for recombining the power of a turbomachineBEDRINE OLIVIER·Filed 2011·Granted Aug 23, 2016·8 cites·9 claims
- 0572US10371062B2Turboshaft engine, twin-engine helicopter equipped with such a turboshaft engine, and method for optimising the zero-power super-idle speed of such a twin-engine helicopterSAFRAN HELICOPTER ENGINES·Filed 2015·Granted Aug 6, 2019·2 cites·4 claims
- 0669US9951694B2System and method for emergency starting of an aircraft turbomachineSNECMA·Filed 2014·Granted Apr 24, 2018·4 cites·6 claims
- 0767US7986052B2Power generation system for an aircraft using a fuel cellTURBOMECA·Filed 2007·Granted Jul 26, 2011·10 cites·12 claims
- 0861US10253699B2Device and method for testing the integrity of a helicopter turbine engine rapid restart systemSAFRAN HELICOPTER ENGINES·Filed 2015·Granted Apr 9, 2019·1 cites·10 claims
- 0950US12305582B2Turbogenerator with simplified control system for aircraftSAFRAN HELICOPTER ENGINES·Filed 2020·Granted May 20, 2025·0 cites·10 claims
- 1042US2013219905A1Method of optimizing the specific fuel consumption of a twin engine helicopter and twin engine architecture with control system for implementing itMARCONI PATRICK·Filed 2011·Application pending·0 cites
- 1139US2013034425A1Method for adapting the air flow of a turbine engine having a centrifugal compressor and diffuser for implementing sameTURBOMECA·Filed 2011·Application pending·0 cites
- 1239US2016237917A1Method for optimising the specific consumption of a twin helicopterTURBOMECA·Filed 2014·Application pending·0 cites
- 1337US10858999B2Removable pack for reactivating a turboshaft engine, architecture for a multi-engine system for propelling a helicopter, provided with such a pack, and corresponding helicopterSAFRAN HELICOPTER ENGINES·Filed 2015·Granted Dec 8, 2020·0 cites·13 claims
- 1435US2017292491A1Ignition system for a combustion chamber of a turboshaft engineSAFRAN HELICOPTER ENGINES·Filed 2015·Application pending·0 cites
- 1532US2017114723A1Device for assisting a solid propellant propulsion system of a single-engine helicopter, single-engine helicopter comprising such a deviceSAFRAN AIRCRAFT ENGINES·Filed 2015·Application pending·0 cites
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Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →