发明名称 AIRCRAFT ENGINE FUEL PUMP BEARING FLOW AND ASSOCIATED SYSTEM AND METHOD
摘要 An assembly or system is provided for selectively regulating journal bearing lubrication between at least first and second levels in an aircraft engine. A high pressure pump includes movable portions at least in part supported by a journal bearing. A selector valve is configured to selectively supply lubrication flow to the journal bearing. In addition, a relief valve is configured to receive a signal from the selector valve defining a pressure level at which the relief valve should relieve pressure.
申请公布号 EP2841719(A1) 申请公布日期 2015.03.04
申请号 EP20130775578 申请日期 2013.04.05
申请人 EATON CORPORATION 发明人 CLEMENTS, MARTIN, A.
分类号 F01D25/20;F02C7/06;F02C7/232 主分类号 F01D25/20
代理机构 代理人
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