ELECTRICITY GENERATOR, AND AIRCRAFT MULTI-SHAFT GAS TURBINE ENGINE PROVIDED WITH SAID ELECTRICITY GENERATOR

An electric generator equipped in a multi-shaft gas turbine engine (10) for aircraft, includes: a rotor (31) attached to the rear end portion (17a) of a low-pressure shaft (17) rotatably supported by a bearing (29) in the gas turbine engine; a stator (32) provided around the rotor (31); wherein the...

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Bibliographische Detailangaben
1. Verfasser:	SEKI, Naoki
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	AIR INTAKES FOR JET-PROPULSION PLANTS BLASTING COMBUSTION ENGINES CONTROL OR REGULATION OF ELECTRIC MOTORS, ELECTRIC GENERATORSOR DYNAMO-ELECTRIC CONVERTERS CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS CONTROLLING TRANSFORMERS, REACTORS OR CHOKE COILS CONVERSION OR DISTRIBUTION OF ELECTRIC POWER DYNAMO-ELECTRIC MACHINES ELECTRICITY ENGINE PLANTS IN GENERAL GAS-TURBINE PLANTS GENERATION HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS JET-PROPULSION 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:	An electric generator equipped in a multi-shaft gas turbine engine (10) for aircraft, includes: a rotor (31) attached to the rear end portion (17a) of a low-pressure shaft (17) rotatably supported by a bearing (29) in the gas turbine engine; a stator (32) provided around the rotor (31); wherein the electric generator has no structure to support the low-pressure shaft (17) and the rotor (31).