An emergency start system for a turbine engine of an aircraft including at least one solid propellant gas generator, an electrically controlled ignition device, a computer connected to the ignition device, and at least one starter motor comprising a turbine for driving a shaft which is for coupling to a shaft of the turbine engine The outlet of the gases from the generator are connected to the inlet of the turbine of the starter motor.
SYSTEME ET PROCEDE DE DEMARRAGE D'URGENCE D'UNE TURBOMACHINE D'AERONEF
2018-03-02
Patent
Electronic Resource
French
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