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Featured researches published by Guillaume Lefort.


Archive | 2007

Bypass turbojet engine nacelle

Guy Bernard Vauchel; Jerome Collier; Patrice Dhainault; Francois Raymond Conte; Nicolas Hillereau; Pierre-Alain Jean-Marie Philippe Hugues Chouard; Guillaume Lefort


Archive | 2007

PROPULSION SYSTEM WITH INTEGRATED PYLON

Thibaud Jean-Baptiste Guibert; Guillaume Lefort; Marc Tesniere


Archive | 2007

INTEGRATED PROPULSIVE SYSTEM COMPRISING A BYPASS TURBOJET ENGINE

Thibaud Jean-Baptiste Guibert; Guillaume Lefort; Marc Tesniere


Archive | 2007

Aircraft propulsion system with integrated pylon

Thibaud Jean-Baptiste Guibert; Guillaume Lefort; Marc Tesniere


Archive | 2007

NACELLE FOR THE JET ENGINE OF AN AIRCRAFT

Guy Bernard Vauchel; Nicolas Hillereau; Jerome Collier; Pierre-Alain Jean-Marie Philippe Hugues Chouard; Guillaume Lefort


Archive | 2007

Isostatic jet engine pylon suspension for aircraft, has front attachment with beam transversal with respect to axis, where plane formed by rods of front attachment and transmission rod are convergent in point on axis of motor or near axis

Pierre Alain Jean Marie Chouard; Benoit Marc Michel Fauvelet; Guillaume Lefort; Mathieu Jean Pierre Trohel


Archive | 2008

SUSPENSION FOR MOUNTING A TURBOJET ENGINE ON AN AIRCRAFT

Pierre-Alain Jean-Marie Philippe Hugues Chouard; Guillaume Lefort


Archive | 2008

Turbojet suspended from an aircraft mast

André Baillard; Pierre-Alain Jean-Marie Philippe Hugues Chouard; Francois Raymond Conte; Guillaume Lefort


Archive | 2007

Nacelle for turbojet engine of aeroplane, has rear section with external structure that is connected to downstream part of casing of fan to support engine, and attachment unit attaching nacelle to strut destined to be connected to fan

Nicolas Hillereau; Pierre Alain Jean Marie Chouard; Guillaume Lefort; Jerome Collier


Archive | 2010

BEAM FOR SUSPENDING A TURBOSHAFT ENGINE FROM AN AIRCRAFT STRUCTURE

Patrick Dunleavy; Guillaume Lefort; Richard Masson; Thibaut Francois Roux; Guilhem Seize

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