Aircraft propulsion assembly comprising an air flow valve with a variable flow rate
AIRCRAFT PROPULSION ASSEMBLY COMPRISING AN AIR FLOW VALVE WITH A VARIABLE FLOW RATE
COMBINED MOTIVE POWER APPARATUS AND SHIP EQUIPPED WITH SAME
COMBINED MOTIVE POWER APPARATUS AND SHIP EQUIPPED WITH SAME
COMBINED MOTIVE POWER APPARATUS AND SHIP EQUIPPED WITH SAME
AIRCRAFT TURBOJET ENGINE NACELLE COMPRISE AN INCREASED-RIGIDITY AIR INTAKE
Aircraft turbojet engine nacelle comprise an increased-rigidity air intake
Endwall component for a turbine stage of a gas turbine engine
Endwall component for a turbine stage of a gas turbine engine
Aircraft engine nacelle bulkheads and methods of assembling the same
AIRCRAFT ENGINE NACELLE BULKHEADS AND METHODS OF ASSEMBLING THE SAME
Engine Mount Waiting Fail Safe Lug Joint with Reduced Dynamic Amplification Factor
Engine mount waiting fail safe lug joint with reduced dynamic amplification factor
Airfoils including tip profile for noise reduction and method for fabricating same
Airfoils including tip profile for noise reduction and method for fabricating same
Lifting tool for rotary shaft and lifting method for rotary shaft
Propeller Including a Discrete Blade Edge Cover Member
Propeller including a discrete blade edge cover member
METHOD AND DEVICE FOR MOUNTING AND REMOVING TURBINE COMPONENT
Method for optimising the shape of an aerofoil and corresponding aerofoil
THRUST REVERSER TORQUE BOX WITH DISCRETE MAJOR FITTINGS
Method of dynamic energy-saving superconductive propeller interaction with a fluid medium
Method of dynamic energy-saving superconductive propeller interaction with a fluid medium
METHOD OF DYNAMIC ENERGY-SAVING SUPERCONDUCTIVE PROPELLER INTERACTION WITH A FLUID MEDIUM
METHOD OF DYNAMIC ENERGY-SAVING SUPERCONDUCTIVE PROPELLER INTERACTION WITH A FLUID MEDIUM
TURBOPROPULSEUR MUNI D'UN DISPOSITIF D'ORIENTATION DE PALES
TURBOPROPULSEUR MUNI D'UN DISPOSITIF D'ORIENTATION DE PALES
CARTER DE TURBOMACHINE À VIROLE SANS EMPOCHEMENTS ET À CHAPES RENFORCÉES PAR DES RAIDISSEURS
Turbomachine blade incidence control system and turbomachine
Blade with reduced torsional rigidity, and rotor equipped with such a blade
BLADE WITH REDUCED TORSIONAL RIGIDITY, AND ROTOR EQUIPPED WITH SUCH A BLADE
FLOATING AND STORAGE GAS POWER PLANT AND HIGH POWER APPARATUS OF THE POWER PLANT
FLOATING AND STORAGE GAS POWER PLANT, AND HIGH POWER APPARATUS OF THE POWER PLANT