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 and a controller. The controller is operable to coordinate control of the first engine starting system to alternate use of power from a power source relative to use of the power by one or more other engine starting systems of the aircraft while maintaining a starting spool speed of the first engine below a resonance speed of the starting spool during motoring of the first engine.
ALTERNATING STARTER USE DURING MULTI-ENGINE MOTORING
25.01.2018
Patent
Elektronische Ressource
Englisch
Multi-engine coordination during gas turbine engine motoring
Europäisches Patentamt | 2021
|MULTI-ENGINE COORDINATION DURING GAS TURBINE ENGINE MOTORING
Europäisches Patentamt | 2021
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