Sebastien Alain Christophe Bourgois

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Archive | 2010

Air and fuel injecting system for annular combustion chamber of turbomachine of aircraft, has air intake annular space arranged radially and inwardly relative to ejecting units for admission of air flow to mix with fuel in annular channel

Sebastien Alain Christophe Bourgois; Patrice Andre Commaret; Didier Hernandez

Archive | 2009

Fuel injecting system for e.g. annular direct flow combustion chamber of turboprop engine of aircraft, has air passage channels formed with holes, where air flow delivered through holes is utilized to clean up head of fuel injector

Sebastien Alain Christophe Bourgois; Didier Hernandez; Lorenzo Hernandez; Christophe Nicolas Henri Viguier

Archive | 2009

TURBOMACHINE COMBUSTION CHAMBER WALL HAVING A SINGLE ANNULAR ROW OF INLET ORIFICES FOR PRIMARY AIR AND FOR DILUTION AIR

Sebastien Alain Christophe Bourgois; Patrice Andre Commaret; Thierry Cortes

Archive | 2011

AERODYNAMIC SHROUD FOR THE BACK OF A COMBUSTION CHAMBER OF A TURBOMACHINE

Sebastien Alain Christophe Bourgois; Didier Hernandez

Archive | 2010

MIXING SCREW FOR A FUEL INJECTOR IN A COMBUSTION CHAMBER OF A GAS TURBINE, AND CORRESPONDING COMBUSTION DEVICE

Sebastien Alain Christophe Bourgois; Didier Hernandez; Matthieu Francois Rullaud

Archive | 2009

Wall for combustion chamber in a turbine engine with single annular row of intake openings for primary and dilution air

Sebastien Alain Christophe Bourgois; Patrice Andre Commaret; Thierry Cortes

Archive | 2012

Annular combustion chamber in a turbomachine

Sebastien Alain Christophe Bourgois; Denis Jean Maurice Sandelis

Archive | 2010

TURBOMACHINE COMBUSTION CHAMBER COMPRISING IMPROVED MEANS OF AIR SUPPLY

Sebastien Alain Christophe Bourgois; Romain Nicolas Lunel; Thomas Olivier Marie Noel

Archive | 2017

câmara de combustão anular em uma turbomáquina

Denis Jean Maurice Sandelis; Sebastien Alain Christophe Bourgois

ASME Turbo Expo 2016: Turbomachinery Technical Conference and Exposition | 2016

Turbines and Structures for Ultra-High Pressure Ratio Aero-Engines

Anders Lundbladh; Ralf von der Bank; Richard Avellán; Stefan Forsman; Stefan Donnerhack; Wolfgang Sturm; Joris Versluis; Anthony Rae; Mark Stokes; Oscar Caballero; Natalia Soldevilla; Artur Ornat; Tomasz Mrugala; Lucjan Kraj; Sebastien Alain Christophe Bourgois

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