SYSTEM AND METHOD FOR PROTECTING STRENGTH OF MOTOR PYLON
HOUSING STRUCTURE, INSTALLED BETWEEN THE ENGINE AND THE NACELLE USING THE PLATE WITH SCREWS
STATOR BLADE STRUCTURE AND TURBOFAN JET ENGINE USING SUCH BLADE
КОНСТРУКЦИЯ ЛОПАТКИ СТАТОРА И ТУРБОВЕНТИЛЯТОРНЫЙ РЕАКТИВНЫЙ ДВИГАТЕЛЬ С ИСПОЛЬЗОВАНИЕМ ТАКОЙ ЛОПАТКИ
OIL DISCHARGE DEVICE FOR AND TURBOMACHINE CONTAINING SUCH A DEVICE
HULL STRUCTURE WITH THE SHELL TURNING SECTORS, INSTALLED BETWEEN THE ENGINE AND THE NACELLE
TURBO MACHINE WITH PROPELLER (-S) FOR AIRCRAFT WITH PROPELLER PITCH CHANGE SYSTEM
TURBO-PROPELLER ENGINE CONTROL DEVICE FOR FAN BLADES ORIENTATION OF TURBO-PROPELLER ENGINE
QUICK-RELIEF DEVICE FOR ENGINE WITH FREE AIRCRAFT TURBINE
DEVICE FOR RETAINING DRAINED FLUIDS FOR PROPULSIVE ASSEMBLY
METHOD OF CONTROLLING TWIN-ROTOR GAS-TURBINE ENGINE OF AIRCRAFT AT STOPPAGE