Fabrice Marcel Noel Garin

BALANCING SYSTEM FOR TURBOMACHINE ROTOR

Fixed vane assembly for a turbine engine having a reduced weight, and turbine engine comprising at least one such fixed vane assembly

Ventilation of a high-pressure turbine in a turbomachine

Assembly including a turbine disc for a gas turbine engine and a bearing-supporting journal, and cooling circuit for the turbine disc of such an assembly

Rotor disc e.g. labyrinth disc, for e.g. low pressure turbine of aircraft's jet engine, has inner radial portion including bore, and carrying balancing flange equipped with balance weights, where weights and flange form balancing system

INTERFACE ELEMENT BETWEEN A BLADE ROOT AND A BLADE ROOT HOUSING OF A TURBINE DISC, AND TURBINE ROTOR COMPRISING AN INTERFACE ELEMENT

Turboshaft engine e.g. turbojet, for aircraft, has snap ring including tooth co-operating by shape coupling with axial slot above sleeve and another tooth co-operating by shape coupling with another axial slot of pivot

Retaining device for axially retaining a rotor disk flange in a turbomachine

Balancing system for a turbomachine rotor

Turbine engine including an improved means for adjusting the flow rate of a secondary air flow sampled at the output of a high-pressure compressor