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Featured researches published by Patrick Marconi.


Archive | 2011

METHOD OF OPTIMIZING THE SPECIFIC FUEL CONSUMPTION OF A TWIN ENGINE HELICOPTER AND TWIN ENGINE ARCHITECTURE WITH CONTROL SYSTEM FOR IMPLEMENTING IT

Patrick Marconi; Romain Thiriet


Archive | 2011

Procede d'optimisation de la consommation specifique d'un helicoptere bimoteur et architecture bimoteur a systeme de regulation pour sa mise en oeuvre

Patrick Marconi; Romain Thiriet


Archive | 2008

Power generation system for an aircraft using a fuel cell

Patrick Marconi


Archive | 2016

Method and architecture for recombining the power of a turbomachine

Olivier Bedrine; Patrick Marconi; Alphonse Puerto


Archive | 2013

METHOD AND ARCHITECTURE FOR THE OPTIMIZED TRANSFER OF POWER BETWEEN AN AUXILIARY POWER MOTOR AND THE MAIN ENGINES OF A HELICOPTER

Pascal Dauriac; Olivier Bedrine; Patrick Marconi; Jean-François Rideau


Archive | 2011

METHOD FOR ADAPTING THE AIR FLOW OF A TURBINE ENGINE HAVING A CENTRIFUGAL COMPRESSOR AND DIFFUSER FOR IMPLEMENTING SAME

Pierre Biscay; Patrick Marconi; Hubert Hippolyte Vignau


Archive | 2017

TURBOSHAFT 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 HELICOPTER

Patrick Marconi; Romain Thiriet; Camel Serghine


Archive | 2015

Turboshaft 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 helicopteR

Patrick Marconi; Romain Thiriet; Olivier Bedrine


Archive | 2014

METHOD FOR OPTIMISING THE SPECIFIC CONSUMPTION OF A TWIN HELICOPTER

Patrick Marconi; Romain Thiriet


Archive | 2011

Bi-centrifugal compressor assembly for turbine engine of helicopter, has compression stage, and diffuser joint that is coupled to compressor stage of centrifugal compressor via air return channel that is inclined upstream

Pierre Biscay; Fabien Artus; Patrick Marconi; Eric Mignard

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