发明名称 Adequate oil supply for an aeroengine oil tank system
摘要 A gas turbine engine (10) comprising an oil system (50) and a gearbox (33), the gearbox (33) is driven by at least one engine shaft (23, 24, 25), the oil system (50) comprises a pump (38) drivingly connected to the gearbox (33), an oil tank (42) connected to the pump (38) via a supply pipe (46) and a delivery pipe (47) connecting the pump to the engine (10) for delivery of oil thereto, an anti-siphon pipe (52) is connected between the tank (42) and the delivery pipe (47) to provide an excess oil flow to the engine (10) characterised in that the anti-siphon pipe (52) includes a variable flow valve (60) 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 (54) in the tank (42).
申请公布号 EP1647675(A1) 申请公布日期 2006.04.19
申请号 EP20050255566 申请日期 2005.09.10
申请人 ROLLS-ROYCE PLC 发明人 CHAMPION, CLARE DIANA;CHRISTOL, PHILIPPE
分类号 F01D25/18;F01D21/14;F01D25/20;F02C7/14;F02C7/25;F02C7/36 主分类号 F01D25/18
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