LUBRICATION SYSTEM FOR GAS TURBINE ENGINES
    1.
    发明申请
    LUBRICATION SYSTEM FOR GAS TURBINE ENGINES 审中-公开
    瓦斯涡轮发动机润滑系统

    公开(公告)号:WO2014085031A2

    公开(公告)日:2014-06-05

    申请号:PCT/US2013068275

    申请日:2013-11-04

    Abstract: A lubrication system is disclosed. The lubrication system may be used in conjunction with a gas turbine engine for generating power or lift. The lubrication system utilized a flow scheduling valve which reduces lubricant flow to at least one component based on an engine load. The lubrication system may further include a main pump which may be regulated by an engine speed. Thus, a lubrication system which provides a lubricant to engine components based on the load and speed of the engine is possible. The system may improve efficiency of the engine by reducing the power previously spent in churning excess lubricant by at least one engine component as well as reducing the energy used by a lubricant cooler in cooling the excess lubricant. The lubricant cooler size may also be minimized to reduce weight and air drag due to the reduced lubricant flow.

    Abstract translation: 公开了润滑系统。 润滑系统可以与用于产生动力或升力的燃气涡轮发动机结合使用。 润滑系统使用流量调节阀,其基于发动机负载减少至少一个部件的润滑剂流量。 润滑系统还可以包括可以由发动机转速调节的主泵。 因此,可以基于发动机的负载和速度向发动机部件提供润滑剂的润滑系统。 该系统可以通过减少先前由至少一个发动机部件搅拌多余的润滑剂而减少先前消耗的功率并且降低润滑剂冷却器在冷却多余润滑剂时使用的能量来提高发动机的效率。 润滑剂冷却器尺寸也可以最小化,以减少润滑剂流动导致的重量和空气阻力。

    CIRCULATING LUBRICANT THROUGH A TURBINE ENGINE COMPONENT WITH PARALLEL PUMPS
    3.
    发明申请
    CIRCULATING LUBRICANT THROUGH A TURBINE ENGINE COMPONENT WITH PARALLEL PUMPS 审中-公开
    通过涡轮发动机与平行泵组件循环润滑

    公开(公告)号:WO2014152347A2

    公开(公告)日:2014-09-25

    申请号:PCT/US2014027238

    申请日:2014-03-14

    Abstract: A system for a turbine engine includes a turbine engine component, a lubricant collection device and a plurality of lubricant circuits. The lubricant collection device is fluidly coupled with the turbine engine component. The lubricant circuits are fluidly coupled between the lubricant collection device and the turbine engine component. The lubricant circuits include a first circuit and a second circuit configured in parallel with the first circuit. Each of the lubricant circuits includes a lubricant pump. The first and the second circuits receive lubricant from the lubricant collection device, and direct the received lubricant to the turbine engine component.

    Abstract translation: 一种用于涡轮发动机的系统包括涡轮发动机部件,润滑剂收集装置和多个润滑剂回路。 润滑剂收集装置与涡轮发动机部件流体地联接。 润滑剂回路流体联接在润滑剂收集装置和涡轮发动机部件之间。 润滑剂回路包括与第一回路并联配置的第一回路和第二回路。 每个润滑剂回路包括润滑剂泵。 第一回路和第二回路从润滑剂收集装置接收润滑剂,并将接收到的润滑剂引导至涡轮发动机部件。

    LUBRICATION SYSTEM FOR GAS TURBINE ENGINES
    6.
    发明公开
    LUBRICATION SYSTEM FOR GAS TURBINE ENGINES 审中-公开
    燃气轮机发动机润滑系统

    公开(公告)号:EP2925974A4

    公开(公告)日:2016-07-20

    申请号:EP13858861

    申请日:2013-11-04

    Abstract: A lubrication system is provided. The lubrication system may be used in conjunction with a gas turbine engine for generating power or lift. The lubrication system utilized a flow scheduling valve which reduces lubricant flow to at least one component based on an engine load. The lubrication system may further include a main pump which may be regulated by an engine speed. Thus, a lubrication system which provides a lubricant to engine components based on the load and speed of the engine is possible. The system may improve efficiency of the engine by reducing the power previously spent in churning excess lubricant by at least one engine component as well as reducing the energy used by a lubricant cooler in cooling the excess lubricant. The lubricant cooler size may also be minimized to reduce weight and air drag due to the reduced lubricant flow.

    Abstract translation: 公开了一种润滑系统。 润滑系统可以与用于产生动力或升力的燃气涡轮发动机结合使用。 润滑系统使用流量调节阀,其基于发动机负载减少润滑剂流向至少一个部件。 润滑系统还可以包括可以通过发动机转速来调节的主泵。 因此,可以基于发动机的负载和速度向发动机部件提供润滑剂的润滑系统。 该系统可以通过减少先前由至少一个发动机部件搅拌多余的润滑剂而减少在减少多余的润滑剂冷却过程中由润滑剂冷却器使用的能量的功率来提高发动机的效率。 润滑剂冷却器尺寸也可以最小化,以减少由于减少的润滑剂流动引起的重量和空气阻力。

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