Xavier Flandrois

Control system for turbo machine of engine of aircraft, has switching unit comprising commutation modules and switches and switching between selected path and passive path in response to detection of failure by monitoring units

Stephane Bernard, Michael Dinsart, Xavier Flandrois, 2010 .

High-pressure pump monitoring device for e.g. jet engine, of aircraft, has comparing unit for comparing value with predetermined threshold to direct replacement of high-pressure pump in fuel supply circuit when value attains threshold

Franck Godel, Xavier Flandrois, Christian Aurousseau, 2007 .

the state of health monitoring system of equipment involved in the ability to boot from a turbojet

Xavier Flandrois, Christian Aurousseau, Jean Remi Masse, 2009 .

distributed control system for a turbine engine

Michael Dinsart, Xavier Flandrois, Stephane Bernard, 2010 .

Method and device for monitoring a control loop of a variable geometry actuating system of a turbojet

Xavier Flandrois, Regis Michel Paul Deldalle, Christian Aurousseau, 2010 .

Expertise Transfer and Automatic Failure Classification for the Engine Start Capability System

Xavier Flandrois, Jerome Lacaille, Jean-Remi Masse, 2009 .