AIRCRAFT GAS TURBINE ENGINE EMERGENCY STARTING SYSTEM AND METHOD Russian patent published in 2018 - IPC F02C7/26 

FIELD: motors and pumps.

SUBSTANCE: disclosed is the gas turbine engine emergency start system containing at least one gas generator on solid rocket fuel, electrically controlled ignition device, associated with the ignition device computing device, and at least two independent starters, each of which is designed for the one gas turbine engine starting, at that, each starter comprises the shaft drive turbine for connection to the corresponding gas turbine engine shaft, at that, the generator gases output is connected to the starter turbine input of each starter via connected to the computing device single distribution valve. Also disclosed are aircraft and the gas turbine engine emergency starting method.

EFFECT: simplification, increase in efficiency and effectiveness.

6 cl, 4 dwg