发明名称 Gas turbine engine lubrication system including three stage flow control valve
摘要 A lubrication supply system for providing lubricant to the bearings and the gear box assemblies of a gas turbine engine includes a three stage poppet control valve means interposed between the source of pressurized lubricant and the bearings. The control valve is responsive to the engine speed which determines the level of pressurization of the pressurized lubricant. The control valve by-passes all lubricant to a sump below a selected speed, opens a first passage to the bearings, etc. during idling speed and, modulates the opening of a second passage to the bearings, etc., at speeds above idling.
申请公布号 US4245465(A) 申请公布日期 1981.01.20
申请号 US19790071230 申请日期 1979.08.30
申请人 AVCO CORPORATION 发明人 MILO, GEORGE T.
分类号 F02C7/06;F01D25/18;F01M1/16;F16N27/00;(IPC1-7):F02C7/06 主分类号 F02C7/06
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