GAS TURBINE LUBRICATION SYSTEMS
    1.
    发明公开
    GAS TURBINE LUBRICATION SYSTEMS 审中-公开
    SCHMIERMITTELSYSTEMEFÜRGASTURBINEN

    公开(公告)号:EP3060779A4

    公开(公告)日:2017-07-26

    申请号:EP14855369

    申请日:2014-10-01

    IPC分类号: F02C7/06 F01D25/16 F01D25/20

    摘要: A lubrication circuit for a gas turbine engine includes a bearing compartment, an air inlet connected to the bearing compartment, a lubricant inlet, and a lubricant outlet. The air inlet fluidly connects the bearing compartment to an environment external to the compartment. The lubricant inlet and outlet are connected to the bearing compartment. A scavenge valve is operatively connected between the lubricant outlet and a scavenge pump that is responsive to bearing compartment pressure for controlling pres sure drop across the air inlet.

    摘要翻译: 用于燃气涡轮发动机的润滑回路包括轴承室,连接到轴承室的进气口,润滑剂入口和润滑剂出口。 进气口将轴承室流体连接至隔室外部的环境。 润滑剂入口和出口连接到轴承舱。 回油阀可操作地连接在润滑剂出口和回油泵之间,该回油泵响应于轴承室压力来控制通过进气口的压降。