发明名称 AIRCRAFT GAS TURBINE
摘要 FIELD: engines and pumps.SUBSTANCE: oil-air emulsion with high content of air is formed at discharge pump inlet at extreme engine operating conditions (for example, at aircraft acrobatic flights) due to increase in hydraulic resistance in discharge lines, increased mixing of oil with fuel and intensified dissolution of air in oil. This can result in decrease in lift and discharge pump efficiency, discharge pump being a reliable component of oil system. Problem pump oil chamber feed and discharge balance is disturbed to overfill said chamber and to overheat the oil. Both indications are accompanied with oil leaks from oil tank that brings about the engine "oil hunger" conditions.EFFECT: recovery of oil feed and discharge, normal operation of the engine.3 cl, 1 dwg
申请公布号 RU2522713(C1) 申请公布日期 2014.07.20
申请号 RU20130122545 申请日期 2013.05.16
申请人 OTKRYTOE AKTSIONERNOE OBSHCHESTVO "UFIMSKOE MOTOROSTROITEL'NOE PROIZVODSTVENNOE OB"EDINENIE" (OAO "UMPO") 发明人 GOLUBOV ALEKSANDR NIKOLAEVICH;SEMENOV VADIM GEORGIEVICH;FOMIN VJACHESLAV NIKOLAEVICH
分类号 F02C7/06 主分类号 F02C7/06
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