发明名称 HIGH-PRESSURE TURBINE
摘要 FIELD: engines and pumps.SUBSTANCE: proposed device comprises shaft running in bearing with oil cavity, internal sleeve and labyrinth seals between disc and bearing. Labyrinth higher-pressure air cavity communicates via labyrinth radial perforation with external annular slotted cavity. Said external annular slotted cavity is arranged between labyrinth and shaft ob bearing side in radial direction and between disc and bearing in axial direction. Besides, said external annular slotted cavity outlet communicates with internal annular slotted cavity via radial shaft openings nearby bearing. Internal annular slotted cavity is arranged between inner sleeve and shaft to communicate with low-pressure cavity located on disc side via radial shaft openings nearby disc.EFFECT: higher reliability.2 dwg
申请公布号 RU2470162(C1) 申请公布日期 2012.12.20
申请号 RU20110121211 申请日期 2011.05.25
申请人 OTKRYTOE AKTSIONERNOE OBSHCHESTVO "AVIADVIGATEL'" 发明人 SYCHEV VLADIMIR KONSTANTINOVICH;JAZEV VLADIMIR MIKHAJLOVICH;KUZNETSOV VALERIJ ALEKSEEVICH
分类号 F01D11/02 主分类号 F01D11/02
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