ELECTRIC MACHINE ASSEMBLY FOR A TURBINE ENGINE

A turbine engine (10, 110, 210, 310) with a turbine core (38, 138, 238, 338) that includes a compressor section (22, 122, 222, 322) having a compressor (26, 126, 226, 326) coupled to a high speed shaft (48, 148, 248, 348), a combustion section (28, 128, 228, 328), a turbine section (32, 132, 232, 33...

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Bibliographische Detailangaben
Hauptverfasser:	GEMIN, Paul, BALADI, Mehdi Milani
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 GAS-TURBINE PLANTS HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS LIGHTING MECHANICAL ENGINEERING WEAPONS
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Beschreibung
Zusammenfassung:	A turbine engine (10, 110, 210, 310) with a turbine core (38, 138, 238, 338) that includes a compressor section (22, 122, 222, 322) having a compressor (26, 126, 226, 326) coupled to a high speed shaft (48, 148, 248, 348), a combustion section (28, 128, 228, 328), a turbine section (32, 132, 232, 332) having a high pressure turbine (34, 134, 234, 334) coupled to the high speed shaft (48, 148, 248, 348) and a low pressure turbine (36, 136, 236, 336) coupled to a low speed shaft (56, 156, 256, 356), and a nozzle section (37, 137, 237, 337). The turbine engine (10, 110, 210, 310) also includes an electric machine (52, 152, 252, 352) that can operate in a first starting mode and a second generating mode.