System and method for emergency starting of an aircraft turbomachine
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United States of America Patent
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Apr 24, 2018
Issued Date -
N/A
app pub date -
Sep 12, 2014
filing date -
Sep 19, 2013
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Abstract
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.
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