GAS TURBINE ENGINE THERMAL MANAGEMENT SYSTEM
    1.
    发明申请
    GAS TURBINE ENGINE THERMAL MANAGEMENT SYSTEM 审中-公开
    气体涡轮发动机热管理系统

    公开(公告)号:US20140360153A1

    公开(公告)日:2014-12-11

    申请号:US14247575

    申请日:2014-04-08

    Abstract: A gas turbine engine according to an exemplary embodiment of this disclosure, among other possible things includes a fan. A geared architecture is configured for driving the fan. A turbine section is configured for driving the geared architecture. A thermal management system that includes a first fluid circuit and a second fluid circuit that manage heat generated in at least a portion of the gas turbine engine. A first heat exchanger is incorporated into each of the first fluid circuit and the second fluid circuit. A second heat exchanger is incorporated into the first fluid circuit. A valve controls an amount of a first fluid that is communicated to the first heat exchanger and the second heat exchanger. A controller is configured to control a positioning of the valve. The amount of the first fluid communicated to the first heat exchanger is based on a first characteristic of a second fluid and the amount of the first fluid communicated to the second heat exchanger is based on a second characteristic of the second fluid. A method and a system are also disclosed.

    Abstract translation: 根据本公开的示例性实施例的燃气涡轮发动机以及其它可能的事情包括风扇。 齿轮架构配置为驱动风扇。 涡轮机部分被配置用于驱动齿轮架构。 一种热管理系统,其包括第一流体回路和第二流体回路,其管理在燃气涡轮发动机的至少一部分中产生的热量。 第一热交换器被并入到第一流体回路和第二流体回路的每一个中。 第二热交换器被并入到第一流体回路中。 阀门控制与第一热交换器和第二热交换器连通的第一流体的量。 控制器被配置为控制阀的定位。 与第一热交换器连通的第一流体的量基于第二流体的第一特性,并且与第二热交换器连通的第一流体的量基于第二流体的第二特性。 还公开了一种方法和系统。

    Gas turbine engine thermal management system
    4.
    发明授权
    Gas turbine engine thermal management system 有权
    燃气轮机发动机热管理系统

    公开(公告)号:US09038397B2

    公开(公告)日:2015-05-26

    申请号:US14247575

    申请日:2014-04-08

    Abstract: A gas turbine engine according to an exemplary embodiment of this disclosure, among other possible things includes a fan. A geared architecture is configured for driving the fan. A turbine section is configured for driving the geared architecture. A thermal management system that includes a first fluid circuit and a second fluid circuit that manage heat generated in at least a portion of the gas turbine engine. A first heat exchanger is incorporated into each of the first fluid circuit and the second fluid circuit. A second heat exchanger is incorporated into the first fluid circuit. A valve controls an amount of a first fluid that is communicated to the first heat exchanger and the second heat exchanger. A controller is configured to control a positioning of the valve. The amount of the first fluid communicated to the first heat exchanger is based on a first characteristic of a second fluid and the amount of the first fluid communicated to the second heat exchanger is based on a second characteristic of the second fluid. A method and a system are also disclosed.

    Abstract translation: 根据本公开的示例性实施例的燃气涡轮发动机以及其它可能的事情包括风扇。 齿轮架构配置为驱动风扇。 涡轮机部分被配置用于驱动齿轮架构。 一种热管理系统,其包括第一流体回路和第二流体回路,其管理在燃气涡轮发动机的至少一部分中产生的热量。 第一热交换器被并入到第一流体回路和第二流体回路的每一个中。 第二热交换器被并入到第一流体回路中。 阀门控制与第一热交换器和第二热交换器连通的第一流体的量。 控制器被配置为控制阀的定位。 与第一热交换器连通的第一流体的量基于第二流体的第一特性,并且与第二热交换器连通的第一流体的量基于第二流体的第二特性。 还公开了一种方法和系统。

    Auxiliary journal oil supply system

    公开(公告)号:US10513949B2

    公开(公告)日:2019-12-24

    申请号:US15260995

    申请日:2016-09-09

    Abstract: A fluid circulation system may comprise a main pump configured to provide oil to a journal bearing. An auxiliary system including a pump system may be configured to provide oil to the journal bearing. A manifold may be configured to mix the oil from the main pump with oil from the auxiliary system. A journal delivery line may be configured to deliver the oil from the manifold to the journal bearing.

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