SYSTEM COMPRISING A TURBOMACHINE CONTROL SYSTEM AND A TURBOMACHINE, METHOD OF OPERATING A TURBOMACHINE COMPLEX

A turbomachine complex includes at least one motor-generator, at least one power source coupled to the at least one motor-generator, and at least one load dissipative device coupled to the at least one motor-generator. The turbomachine complex is configured to energize the at least one motor-generat...

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Bibliographische Detailangaben
Hauptverfasser:	HOFER, Douglas, Carl, LEHAR, Matthew, Alexander
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	AIR INTAKES FOR JET-PROPULSION PLANTS BLASTING COMBUSTION ENGINES CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS ENGINE PLANTS IN GENERAL GAS-TURBINE PLANTS HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS LIGHTING MACHINES OR ENGINES IN GENERAL MECHANICAL ENGINEERING NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES STEAM ENGINES WEAPONS
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Beschreibung
Zusammenfassung:	A turbomachine complex includes at least one motor-generator, at least one power source coupled to the at least one motor-generator, and at least one load dissipative device coupled to the at least one motor-generator. The turbomachine complex is configured to energize the at least one motor-generator through the at least one power source. The turbomachine complex is further configured to simultaneously energize the at least one at least one load dissipative device through the at least one motor-generator.