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Featured researches published by Alain Pierre Garassino.


Volume 5: Manufacturing Materials and Metallurgy; Ceramics; Structures and Dynamics; Controls, Diagnostics and Instrumentation; Education; IGTI Scholar Award | 1995

An Advanced Control System for Turbofan Engine: Multivariable Control and Fuzzy Logic (Application to the M88-2 Engine)

Alain Pierre Garassino

The search for better performance of present and future turbofan engine involves an increase on the number of variable geometries and thus of control loops.As we can not or do not want to disregard the interaction between loops any more, the future control systems will therefore be multivariable. The aim of the architecture of multivariable control presented here is to optimize a performance index during transients.This architecture consists of an inner loop which optimizes the performance index taking in account the limitations, an outer loop which brings the nominal steady-state offsets to zero and a trajectory which allows to take into account the topping schedule limitation.This basic architecture can be improved by fuzzy supervisor.Indeed, two control outputs are generated according to the description above:- the first one optimizes the thrust and does not care very much about LP stall margin limitation,- the second one optimizes again the thrust and strongly takes low pressure stall margin limitation into account.The fuzzy logic then allows to do a compromise between these two control outputs according to the engine state.Simulation results showing the efficiency of the method are given.Copyright


Archive | 2001

Hydromechanical system for limiting excess engine speed

David Maillard; Alain Pierre Garassino; Claude Maillard; Caroline Dessenne; Isabelle Vegiotti


Archive | 2001

Two-level pressurization valve controlled by a fuel metering unit

Claude Maillard; David Maillard; Alain Pierre Garassino


Archive | 2000

Self-testable architecture for overspeed limitation and cutoff systems when the turbojet stops

Jean-Marie Brocard; Alain Pierre Garassino; Christian Denis Le Boeuf; Alain Patrick Paya; Alain Michel Varizat


Archive | 2013

COOLING OF AN OIL CIRCUIT OF A TURBOMACHINE

Alain Pierre Garassino; Robert Michel Delepierre-Massue Olivier; Marc Missout; Jean Pierre Trohel Mathieu


Archive | 2013

REFROIDISSEMENT DU CIRCUIT D'HUILE D'UNE TURBOMACHINE

Alain Pierre Garassino; Olivier Robert Michel Delepierre-Massue; Marc Missout; Mathieu Jean Pierre Trohel


Archive | 2000

Hydro mechanical over speed limiter for aircraft gas turbine has limiter to restrict fuel flow when engine speed exceeds set value

David Maillard; Alain Pierre Garassino; Claude Maillard; Caroline Dessenne; Isabelle Vegiotti


Archive | 2017

caixa de engrenagens.

Alain Pierre Garassino; Bellal Waissi; Frantz Armange; Jordane Peltier; Lambert Olivier Marie Demoulin; Nuria Llamas Castro; Stephane Prunera Usach


Archive | 2015

GAS TURBINE ENGINE COMPRISING A STARTER ENGAGED WITH A LOW-PRESSURE BODY

Bellal Waissi; Sebastien Chalaud; Alain Pierre Garassino


Archive | 2014

Moteur a turbine a gaz a demarreur en prise avec un corps basse pression

Bellal Waissi; Sebastien Chalaud; Alain Pierre Garassino

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