DEVICE FOR RETAINING DRAINED FLUIDS FOR PROPULSIVE ASSEMBLY
FAN WITH VARIABLE ANGLE OF INSTALLATION BY VARIOUS ROTATION OF FAN DISCS
FLEXIBLE SUPPORT STRUCTURE FOR GEARED ARCHITECTURE OF GAS TURBINE ENGINE
HOUSING STRUCTURE, INSTALLED BETWEEN THE ENGINE AND THE NACELLE USING THE PLATE WITH SCREWS
HUB FOR PROPELLER WITH POLYGONAL REINFORCED RING AND TURBOMACHINE EQUIPPED BY SUCH HUB