发明名称 TURBOGENERATOR ROTOR
摘要 FIELD: electrical engineering. SUBSTANCE: turbogenerator rotor has directly gas-cooled field winding 1 whose conductors 1a, 1b, 1c, and 1 b are placed in slots 2 of forged rotor 3 and closed with wedges 4. Insulating strip 6 is fitted between bottom of longitudinal slot 2 and field winding conductor 1d above it. According to invention, fitted between insulating strip 6 and mentioned conductor 1d of field winding 1, at end portion of rotor, is elastic gasket 8 in the form of parallel strip, better in the form of corrugated spring, to compensate for field winding sagging. Gasket 8 stretches from end of forged rotor 3 towards its center. For locking gasket 8 in axial position without contracting main section of slot 9 this gasket is provided with two downward projections 20 entering side depressions 10 of insulating strip 6; apart from longitudinal slots 2 forged rotor 3 has main slots 9 on its both end portions. EFFECT: improved design of field- winding axial-displacement locking means ensuring easy flow of cooling gas. 5 cl, 7 dwg
申请公布号 RU2144252(C1) 申请公布日期 2000.01.10
申请号 RU19940041732 申请日期 1994.11.03
申请人 ASEA BRAUN BOVERI AG 发明人 JOKHANN KLJAJNBURGER;KHANS TSIMMERMANN
分类号 H02K1/32;H02K3/24;H02K3/48;H02K9/08;H02K9/18;(IPC1-7):H02K3/48 主分类号 H02K1/32
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