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    VARIABLE AREA NOZZLE FOR GAS TURBINE ENGINE
    1.
    发明申请
    VARIABLE AREA NOZZLE FOR GAS TURBINE ENGINE 审中-公开
    用于气体涡轮发动机的可变区域喷嘴

    公开(公告)号：US20160003190A1

    公开(公告)日：2016-01-07

    申请号：US14709654

    申请日：2015-05-12

    Applicant: United Technologies Corporation

    Inventor： Richard Alan Weiner

    IPC: F02K1/76 ,  F02K1/62 ,  F02K1/15

    CPC classification number: F02K1/763 ,  F02C7/14 ,  F02K1/08 ,  F02K1/085 ,  F02K1/1223 ,  F02K1/15 ,  F02K1/62 ,  F05D2260/213 ,  Y02T50/676

    Abstract: A variable area fan nozzle comprises an actuator flap and a follower flap. The actuator flap has a portion in contact with a portion of the follower flap. A bias member biases the follower flap outwardly. An actuator actuates the actuator flap inwardly and outwardly to, in turn, move the follower flap against the bias member and to vary an area of an exhaust nozzle. The flap actuator is operable to drive the actuator flap out of contact with the follower flap into a thrust reverser position.

    Abstract translation: 可变区域风扇喷嘴包括致动器挡板和从动挡板。 致动器翼片具有与从动翼片的一部分接触的部分。 偏压构件向外偏压从动翼。 致动器向内和向外致动致动器翼片，从而使从动翼片抵靠偏置构件移动并改变排气喷嘴的面积。 挡板致动器可操作以驱动致动器挡板与从动挡板不接触到推力反向器位置。

    Lubrication system for gas turbine engines
    2.
    发明授权
    Lubrication system for gas turbine engines 有权

    公开(公告)号：US10731559B2

    公开(公告)日：2020-08-04

    申请号：US15875179

    申请日：2018-01-19

    Applicant: United Technologies Corporation

    Inventor： Matthew D. Teicholz ,  Francis Parnin ,  Richard Alan Weiner ,  Katherine A. Knapp Carney

    IPC: F01D25/18 ,  F02C7/06 ,  F01D25/20 ,  F02C7/14 ,  F01M1/16 ,  F16H57/04 ,  F02C3/107 ,  F02C7/36 ,  F01M13/04

    Abstract: A lubrication system for a gas turbine engine according to an example of the present disclosure includes, among other things, a pump that moves a lubricant, a lubricant tank that stores the lubricant, a first engine component and a second engine component each requiring lubrication from the lubricant, a conduit between the lubricant tank and the first engine component and between the lubricant tank and the second engine component, a scheduling valve positioned in the conduit between the lubricant tank, and the first engine component and the second engine component, and a controller including a memory and a processor that controls the scheduling valve, wherein the memory includes an engine performance model, wherein the engine performance model includes stored relationship values between more than one condition experienced by the gas turbine engine during operation and a position of the scheduling valve, and wherein the scheduling valve varies a flow of the lubricant to the first engine component, the second engine component and the lubrication tank based on comparing the more than one condition with the engine performance model.

    DUAL FUNCTION AIR DIVERTER AND VARIABLE AREA FAN NOZZLE
    3.
    发明申请
    DUAL FUNCTION AIR DIVERTER AND VARIABLE AREA FAN NOZZLE 审中-公开
    双功能空气分流器和可变区域风扇喷嘴

    公开(公告)号：US20150198092A1

    公开(公告)日：2015-07-16

    申请号：US14513409

    申请日：2014-10-14

    Applicant: United Technologies Corporation

    Inventor： Richard Alan Weiner

    IPC: F02C7/14 ,  F01D25/18 ,  F01D25/12

    CPC classification number: F02C7/14 ,  F01D25/12 ,  F01D25/18 ,  F02C7/042 ,  F02K3/06 ,  F05D2220/32 ,  F05D2250/411 ,  F05D2260/213 ,  F05D2270/66

    Abstract: A modulating fan air diverter and annular air-oil cooler for a gas turbine engine located in the inner fixed structure adjacent to the core cowl is provided. The fan air diverter modulates between an open position, corresponding to maximum fan nozzle area and airflow through the air-oil cooler, and a closed position, corresponding to minimum fan nozzle area and airflow through the air-oil cooler. As such, the device is capable of supporting dual functions of engine heat management as well as engine performance and fan stability.

    Abstract translation: 提供了一种用于位于靠近核心罩的内部固定结构中的燃气涡轮发动机的调节风扇空气分流器和环形空气 - 油冷却器。 风扇空气分流器在对应于最大风扇喷嘴面积的打开位置和通过空气 - 油冷却器的气流之间调节，并且关闭位置，对应于最小风扇喷嘴面积和通过空气 - 油冷却器的气流。 因此，该装置能够支持发动机热管理的双重功能以及发动机性能和风扇稳定性。

    Dual function air diverter and variable area fan nozzle
    4.
    发明授权
    Dual function air diverter and variable area fan nozzle 有权

    公开(公告)号：US10145304B2

    公开(公告)日：2018-12-04

    申请号：US14513409

    申请日：2014-10-14

    Applicant: UNITED TECHNOLOGIES CORPORATION

    Inventor： Richard Alan Weiner

    IPC: F01D25/12 ,  F02C7/14 ,  F02K3/06 ,  F02C7/042 ,  F01D25/18

    Abstract: A modulating fan air diverter and annular air-oil cooler for a gas turbine engine located in the inner fixed structure adjacent to the core cowl is provided. The fan air diverter modulates between an open position, corresponding to maximum fan nozzle area and airflow through the air-oil cooler, and a closed position, corresponding to minimum fan nozzle area and airflow through the air-oil cooler. As such, the device is capable of supporting dual functions of engine heat management as well as engine performance and fan stability.

    Lubrication system for gas turbine engines
    7.
    发明授权
    Lubrication system for gas turbine engines 有权

    公开(公告)号：US10830140B2

    公开(公告)日：2020-11-10

    申请号：US15875279

    申请日：2018-01-19

    Applicant: United Technologies Corporation

    Inventor： Matthew D. Teicholz ,  Francis Parnin ,  Richard Alan Weiner ,  Katherine A. Knapp Carney

    IPC: F02C7/06 ,  F01D25/20 ,  F02C7/14 ,  F01M1/16 ,  F16H57/04 ,  F02C3/107 ,  F02C7/36 ,  F01M13/04

    Abstract: A method of controlling lubrication flow to a first engine component, a second engine component and a lubrication tank of a gas turbine engine according to an example of the present disclosure includes, among other things, determining more than one condition experienced by the gas turbine engine, comparing with a processor on a controller the more than one condition against an engine performance model stored in memory on the controller, wherein the engine performance model includes stored relationship values between the more than one condition and a position of a scheduling valve, the scheduling valve disposed between the lubricant tank and the first engine component and between the lubricant tank and the second engine component, pumping a lubricant from the lubricant tank through a conduit to the scheduling valve using a pump, and controlling the position of the scheduling valve to vary a flow of the lubricant to two or more of the first engine component, the second engine component and the lubrication tank based upon the comparing of the more than one condition experienced by the gas turbine engine.

    OIL SUPPLY SYSTEM FOR FLUID FILM DAMPER
    8.
    发明申请
    OIL SUPPLY SYSTEM FOR FLUID FILM DAMPER 审中-公开

    公开(公告)号：US20200018350A1

    公开(公告)日：2020-01-16

    申请号：US16035391

    申请日：2018-07-13

    Applicant: UNITED TECHNOLOGIES CORPORATION

    Inventor： Richard Alan Weiner

    IPC: F16C32/06 ,  F02C7/06 ,  F16C17/02 ,  F16C27/02

    Abstract: A fluid film damper may comprise a sleeve, an annular support housing surrounding the sleeve, an annular volume between the annular support housing and the sleeve, a first supply conduit in fluid communication with a first inlet to the annular volume, a second supply conduit in fluid communication with a second inlet to the annular volume, wherein the first inlet is disposed opposite the annular volume from the second inlet, and a common oil supply conduit in fluid communication with the annular volume via a check valve, wherein the common oil supply conduit supplies the fluid to the annular volume via the first supply conduit and the second supply conduit.

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