发明名称 Aeroengine oil tank fire protection system
摘要 A gas turbine engine comprising an oil system and a gearbox, the gearbox is driven by at least one engine shaft, the oil system comprises a pump drivingly connected to the gearbox, an oil tank connected to the pump via a supply pipe and a delivery pipe connecting the pump to the engine for delivery of oil thereto, an anti-siphon pipe is connected between the tank and the delivery pipe to provide an excess oil flow to the engine characterized in that the anti-siphon pipe includes a variable flow valve for regulating the flow of oil passing therethrough such that at low engine speeds an adequate supply of oil is provided to a sight glass in the tank.
申请公布号 US7681402(B2) 申请公布日期 2010.03.23
申请号 US20050222738 申请日期 2005.09.12
申请人 ROLLS-ROYCE PLC 发明人 CHAMPION CLARE D;CHRISTOL PHILIPPE
分类号 F02C7/00;F01D25/20;F02C7/06;F02C7/14;F02C7/25;F02C7/36;F02G3/00 主分类号 F02C7/00
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