B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
B64D33/00—Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for
B64D33/02—Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes
B—PERFORMING OPERATIONS; TRANSPORTING
B64—AIRCRAFT; AVIATION; COSMONAUTICS
B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
B64D33/00—Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for
B64D33/02—Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes
B64D2033/0266—Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes specially adapted for particular type of power plants
B64D2033/028—Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes specially adapted for particular type of power plants for piston engines
Procede pour ameliorer les caracteristiques de performances d'une nacelle de moteur a turbine d'avion et nacelle ainsi qu'entree de nacelle obtenues a l'aide de ce procede.
Ensemble propulsif d'aeronef comportant deux moteurs adjacents, dont les tuyeres de sorties presentent une portion droite a proximite d'un plan median de l'ensemble propulsif
Procede pour etablir le profil de l'entree de la nacelle d'un moteur a turbine a gaz d'avion et entree de nacelle ainsi que nacelle obtenues a l'aide de ce procede.