发明名称 ELASTO-DAMPER BEARING OF GAS TURBINE ENGINE
摘要 FIELD: engines and pumps. ^ SUBSTANCE: proposed bearing consists of case accommodating internal elasto-damper bush wherein roller bearing outer race and jet ring are locked by nut. Roller bearing internal ring is fitted on the shaft together with cage and rollers. Front and rear baffles are fitted on the shaft on front and rear sides from the ring. Front baffle taper wall features outer diametre D1, while rear baffle wall features taper-shape profile with outer diametre D2. Walls taper parts are directed toward labyrinth seals. Labyrinth seal knife edges are arranged on the walls. Oil chamber is insulated from cooling air by front and rear labyrinth seal knife edges, each consisting of front and rear labyrinths fitted on the shaft and stator front and rear flanges of labyrinths. Front and rear baffle labyrinth seal knife edges are directed toward outer cylindrical surfaces of front and rear labyrinth flanges to form, together with said walls, the front and rear air-oil chamber, each being communicated with oil chamber at the outlet. ^ EFFECT: higher reliability. ^ 1 dwg
申请公布号 RU2403417(C1) 申请公布日期 2010.11.10
申请号 RU20090121022 申请日期 2009.06.02
申请人 OTKRYTOE AKTSIONERNOE OBSHCHESTVO "AVIADVIGATEL'" 发明人 KUZNETSOV VALERIJ ALEKSEEVICH
分类号 F02C7/06 主分类号 F02C7/06
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