A system is provided for alternating starter use during multi-engine motoring in an aircraft. The system includes a first engine starting system of a first engine. A first controller is in communication with a second controller that controls a second engine starting system of a second engine, the first controller being configured to intermittently direct power to the first engine starting system to alternately accelerate and decelerate the first engine during motoring with respect to the second engine.
ALTERNATING STARTER USE DURING MULTI-ENGINE MOTORING
2020-07-30
Patent
Electronic Resource
English
Multi-engine coordination during gas turbine engine motoring
European Patent Office | 2021
|MULTI-ENGINE COORDINATION DURING GAS TURBINE ENGINE MOTORING
European Patent Office | 2021
|