Bruno Robert Gaully

System for controlling variable geometry apparatuses in a turbine engine

SYSTEM FOR CONTROLLING AT LEAST TWO VARIABLE-GEOMETRY EQUIPMENTS OF A GAS TURBINE ENGINE, PARTICULARLY BY RACK

System for controlling variable-geometry equipments of a turbomachine, particularly by articulated bellcranks

Method for controlling the clearance at the tips of blades of a turbine rotor

CONTROL UNIT AND A METHOD FOR CONTROLLING BLADE TIP CLEARANCE

METHOD AND SYSTEM FOR CONTROLLING AIRCRAFT ENGINE STARTER/GENERATOR

SYSTEM FOR CONTROLLING VARIABLE GEOMETRY EQUIPMENT OF A GAS TURBINE ENGINE PARTICULARLY COMPRISING A BARREL LINK

System for controlling variable geometry equipment for a turbine engine, especially by bellcranks

METHOD AND DEVICE FOR ADJUSTING A THRESHOLD VALUE OF A FUEL FLOW RATE

DEVICE FOR CHANGING THE TRANSMISSION RATIO BETWEEN A TURBINE SHAFT AND A SHAFT OF A STARTER-GENERATOR OF AN AEROENGINE