发明名称 METHOD TO PRESSURISE TWO-ROTOR GAS TURBINE ENGINE BEARINGS
摘要 FIELD: engines and pumps. ^ SUBSTANCE: invention relates to turbine engine production, particularly to methods of pressurisation of gas turbine engine bearings. Air is forced from high-pressure compressor into oil chamber of LP compressor rear bearings and, via air ducts, into remaining oil chamber of other compressor and turbine bearings during starting and accelerating to rotor RPM approximating to "idle" conditions and decelerating engine from aforesaid conditions to complete stop. Note here that in stopping conditions, compressor and turbine venting valves are closed prior to changing the valve over to bleeding air from high-pressure compressor. During air feed from HP compressor, compressor and turbine venting vales communicating with oil chambers of compressor and turbine bearings are closed. In other engine operating conditions, the valve is changed over to air feed from LP compressor, or gas-air circuit behind the compressor. Note here that after the said change over, aforesaid venting valves are opened. ^ EFFECT: higher tightness, engine longer life and higher reliability. ^ 2 cl, 1 dwg
申请公布号 RU2374470(C1) 申请公布日期 2009.11.27
申请号 RU20080109656 申请日期 2008.03.14
申请人 OTKRYTOE AKTSIONERNOE OBSHCHESTVO "NAUCHNO-PROIZVODSTVENNOE OB"EDINENIE "SATURN" (OAO "NPO "SATURN") 发明人 KANAKHIN JURIJ ALEKSANDROVICH;KIRJUKHIN VLADIMIR VALENTINOVICH;MARCHUKOV EVGENIJ JUVENAL'EVICH
分类号 F02C7/06 主分类号 F02C7/06
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