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    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

    Applicant: UNITED TECHNOLOGIES CORP

    Inventor： PARNIN FRANCIS ,  DOLMAN PAUL H ,  DALEY DAVID M ,  JAMES DENMAN H ,  CLARK RICHARD W

    IPC: F02C7/06

    CPC classification number: F02C7/06 ,  F01D25/20 ,  F05D2270/301 ,  F05D2270/304 ,  F05D2270/331 ,  F05D2270/332 ,  F05D2270/335 ,  Y02T50/671

    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。

    DIRECT FEED AUXILIARY OIL SYSTEM FOR GEARED TURBOFAN ENGINE
    2.
    发明申请
    DIRECT FEED AUXILIARY OIL SYSTEM FOR GEARED TURBOFAN ENGINE 审中-公开
    用于齿轮式涡轮发动机的直接进料辅助油系统

    公开(公告)号：WO2014031194A3

    公开(公告)日：2014-05-08

    申请号：PCT/US2013041769

    申请日：2013-05-20

    Applicant: UNITED TECHNOLOGIES CORP

    Inventor： PARNIN FRANCIS ,  DOLMAN PAUL H

    IPC: F01D25/18 ,  F02C7/06

    CPC classification number: F16H57/045 ,  F01D25/18 ,  F02C3/107 ,  F05D2260/4031 ,  F16H57/0441 ,  F16H57/0479

    Abstract: A lubrication system for a fan drive gear system includes a main lubrication system and an auxiliary lubrication system. The auxiliary lubrication system including a collection channel disposed about the fan drive gear system for collecting expelled lubricant and an auxiliary pump including an inlet receiving lubricant from the collection channel and an outlet in communication with an auxiliary passage. The auxiliary pump supplies lubricant through the auxiliary passages to a bearing passage for communicating lubricant to a bearing. The auxiliary passages include a reservoir after the outlet of the auxiliary pump and before the bearing passage for storing lubricant.

    Abstract translation: 用于风扇驱动齿轮系统的润滑系统包括主润滑系统和辅助润滑系统。 辅助润滑系统包括围绕风扇驱动齿轮系统设置的用于收集排出的润滑剂的收集通道和包括从收集通道接收润滑剂的入口和与辅助通道连通的出口的辅助泵。 辅助泵通过辅助通道将润滑剂供给到用于将润滑剂与轴承连通的轴承通道。 辅助通道包括在辅助泵的出口之后以及用于储存润滑剂的轴承通道之前的储液器。

    LUBRICATION SYSTEM FOR GAS TURBINE ENGINES
    4.
    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

    Applicant: UNITED TECHNOLOGIES CORP

    Inventor： PARNIN FRANCIS ,  DOLMAN PAUL H ,  DALEY DAVID M ,  JAMES DENMAN H ,  CLARK RICHARD W

    IPC: F01D25/00 ,  F01D25/18 ,  F01D25/20

    CPC classification number: F02C7/06 ,  F01D25/20 ,  F05D2270/301 ,  F05D2270/304 ,  F05D2270/331 ,  F05D2270/332 ,  F05D2270/335 ,  Y02T50/671

    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。

    AUXILIARY OIL SYSTEM FOR NEGATIVE GRAVITY EVENT
    5.
    发明公开
    AUXILIARY OIL SYSTEM FOR NEGATIVE GRAVITY EVENT 审中-公开
    HILFSÖLSYSTEMFÜRNEGATIVES SCHWERKRAFTEREIGNIS

    公开(公告)号：EP2855883A4

    公开(公告)日：2016-05-04

    申请号：EP13797647

    申请日：2013-05-13

    Applicant: UNITED TECHNOLOGIES CORP

    Inventor： SHERIDAN WILLIAM G ,  DOLMAN PAUL H

    IPC: F02C7/06 ,  F01D25/18 ,  F01M1/16 ,  F01M11/06 ,  F02C9/00

    CPC classification number: F02C7/06 ,  F01D25/20 ,  F01M11/067 ,  F05D2220/323 ,  F05D2260/98 ,  F16K15/04

    Abstract: A lubrication system includes a bearing compartment. A main reservoir is fluidly connected to the bearing compartment by a main supply passage. A main pump is arranged in the main supply passage configured to provide fluid from the main reservoir to the bearing compartment during a positive gravity condition. A secondary supply passage fluidly connects the main reservoir to at least one segment of the main supply passage, thereby providing fluid from the main reservoir to the bearing compartment during a negative gravity condition. A method of supplying a bearing compartment with fluid includes pumping a fluid from a main reservoir to a bearing compartment through a main supply passage during a positive gravity condition, and providing fluid from the main reservoir to the bearing compartment through a secondary supply passage, fluidly connected to at least one segment of the main supply passage, in response to a negative gravity condition.

    Abstract translation: 润滑系统包括轴承室。 主容器通过主供应通道流体地连接到轴承室。 主泵设置在主供应通道中，构造成在正重力条件期间将流体从主容器提供到轴承室。 二次供应通道将主容器流体地连接到主供应通道的至少一个部分，从而在负重重力条件期间将流体从主容器提供到轴承室。 向轴承室供应流体的方法包括在正重力条件下将流体从主容器泵送到通过主供应通道的轴承室，并且通过次级供应通道将流体从主容器提供到轴承室， 响应于负重重力条件连接到主供应通道的至少一个段。

    DIRECT FEED AUXILIARY OIL SYSTEM FOR GEARED TURBOFAN ENGINE
    7.
    发明公开
    DIRECT FEED AUXILIARY OIL SYSTEM FOR GEARED TURBOFAN ENGINE 审中-公开
    DIREKTFLUSS-HILFSÖLSYSTEMFÜRGETRIEBETURBOLÜFTER

    公开(公告)号：EP2855859A4

    公开(公告)日：2016-04-13

    申请号：EP13830287

    申请日：2013-05-20

    Applicant: UNITED TECHNOLOGIES CORP

    Inventor： PARNIN FRANCIS ,  DOLMAN PAUL H

    IPC: F01D25/18 ,  F02C7/06

    CPC classification number: F16H57/045 ,  F01D25/18 ,  F02C3/107 ,  F05D2260/4031 ,  F16H57/0441 ,  F16H57/0479

    Abstract: A lubrication system for a fan drive gear system includes a main lubrication system and an auxiliary lubrication system. The auxiliary lubrication system including a collection channel disposed about the fan drive gear system for collecting expelled lubricant and an auxiliary pump including an inlet receiving lubricant from the collection channel and an outlet in communication with an auxiliary passage. The auxiliary pump supplies lubricant through the auxiliary passages to a bearing passage for communicating lubricant to a bearing. The auxiliary passages include a reservoir after the outlet of the auxiliary pump and before the bearing passage for storing lubricant.

    Abstract translation: 用于风扇驱动齿轮系统的润滑系统包括主润滑系统和辅助润滑系统。 辅助润滑系统包括围绕风扇驱动齿轮系统设置的用于收集排出的润滑剂的收集通道和包括从收集通道接收润滑剂的入口和与辅助通道连通的出口的辅助泵。 辅助泵通过辅助通道将润滑剂供给到用于将润滑剂与轴承连通的轴承通道。 辅助通道包括在辅助泵的出口之后以及用于储存润滑剂的轴承通道之前的储存器。

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