发明名称 Emergency lubrication system for a gas turbine engine
摘要 <p>An emergency lubrication system for a turbine engine includes a reservoir (50) containing a reserve quantity of lubricant (52) and having a lubricant inlet (54) and a lubricant outlet (56) . A lubricant supply line (62) and a lubricant outlet line (66) each have a respective valve (64,68) for regulating lubricant flow into and out of the reservoir. A fluid supply line (70) includes a valve (72) for selectively establishing communication between the reserve quantity of lubricant and a source of pressurized fluid. During normal operation the lubricant outlet valve (68) continuously releases lubricant at a normal rate to the component requiring lubrication while the lubricant inlet valve (64) concurrently admits fresh lubricant into the reservoir (50) . During abnormal operation, the lubricant inlet valve (64) closes in response to abnormally low lubricant pressure outside the reservoir thereby preventing backflow of reserve lubricant out of the reservoir. The fluid inlet valve (72) opens to admit pressurized fluid into the reservoir thus pressurizing the reserve lubricant. The lubricant outlet valve (68) opens or cycles open and closed in response to a command from a controller (26) so that the pressurized fluid forces lubricant through the outlet (56) as a subnormal rate, which persists until the lubricant reserve is substantially depleted.</p>
申请公布号 EP1510658(B1) 申请公布日期 2014.03.26
申请号 EP20040252784 申请日期 2004.05.13
申请人 UNITED TECHNOLOGIES CORPORATION 发明人 JAMES, DENMAN H.;GLAHN, J. AXEL
分类号 F01D25/18;F01D25/20;F16N7/00;F16N7/38;F16N29/02;F16N31/00 主分类号 F01D25/18
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