A system is provided for multi-engine coordination of gas turbine engine motoring in an aircraft. The system includes a controller operable to determine a motoring mode as a selection between a single engine dry motoring mode and a multi-engine dry motoring mode based on at least one temperature of a plurality of gas turbine engines and initiate dry motoring based on the motoring mode.
MULTI-ENGINE COORDINATION DURING GAS TURBINE ENGINE MOTORING
2021-10-21
Patent
Elektronische Ressource
Englisch
IPC: | F01D Strömungsmaschinen [Kraft- und Arbeitsmaschinen oder Kraftmaschinen], z.B. Dampfturbinen , NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen / F02C Gasturbinenanlagen , GAS-TURBINE PLANTS |
Multi-engine coordination during gas turbine engine motoring
Europäisches Patentamt | 2021
|MULTI-ENGINE COORDINATION DURING GAS TURBINE ENGINE MOTORING
Europäisches Patentamt | 2018
|Multi-engine coordination during gas turbine engine motoring
Europäisches Patentamt | 2023
|Cross engine coordination during gas turbine engine motoring
Europäisches Patentamt | 2019
|CROSS ENGINE COORDINATION DURING GAS TURBINE ENGINE MOTORING
Europäisches Patentamt | 2018
|