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    VARIABLE SHAPE INLET SECTION FOR A NACELLE ASSEMBLY OF A GAS TURBINE ENGINE
    14.
    发明申请
    VARIABLE SHAPE INLET SECTION FOR A NACELLE ASSEMBLY OF A GAS TURBINE ENGINE 审中-公开
    燃气轮机发动机组件的变形形状入口部分

    公开(公告)号：US20130170950A1

    公开(公告)日：2013-07-04

    申请号：US13777300

    申请日：2013-02-26

    Applicant: United Technologies Corporation

    Inventor： Ashok K. Jain ,  Zaffir A. Chaudhry

    IPC: F01D17/00

    CPC classification number: F01D17/00 ,  F04D27/0253 ,  F04D29/563 ,  Y10T137/0536 ,  Y10T137/0645

    Abstract: A method of improving the aerodynamic performance of an inlet section of a nacelle assembly of a gas turbine engine, according to an exemplary aspect of the present disclosure includes, among other things, (a) sensing an operability condition, (b) adjusting a leading edge of the inlet section in response to the step (a), and (c) adjusting a thickness of the inlet section in response to the step (a).

    Abstract translation: 根据本公开的示例性方面，根据本公开的示例性方面，改进燃气涡轮发动机的机舱组件的入口部分的空气动力学性能的方法包括（a）感测可操作性条件，（b）调整前导 响应于步骤（a）的入口部分的边缘，和（c）响应于步骤（a）调整入口部分的厚度。

    SURFACE MOUNT PERMANENT MAGNET ATTACHMENT FOR ELECTRIC MACHINE
    19.
    发明申请
    SURFACE MOUNT PERMANENT MAGNET ATTACHMENT FOR ELECTRIC MACHINE 审中-公开

    公开(公告)号：US20180205275A1

    公开(公告)日：2018-07-19

    申请号：US15869793

    申请日：2018-01-12

    Applicant: United Technologies Corporation

    Inventor： Jagadeesh Tangudu ,  Zaffir A. Chaudhry

    IPC: H02K1/27 ,  H02K1/28

    CPC classification number: H02K1/278 ,  H02K1/28

    Abstract: A rotor of an electric machine includes a rotor core having a plurality of axially-stacked rotor laminations, and a plurality of permanent magnets. The plurality of permanent magnets are first permanent magnets secured at the core outer circumferential surface of the rotor core and are made of a first permanent magnet material with a first magnetic orientation. The plurality of permanent magnets are secured to the rotor core via a plurality of mechanical interface joints defined by at least one first mechanical interface feature having a permanent magnet channel with a magnet channel surface, located inside the permanent magnet and at least one second mechanical interface feature having a core channel with a core channel surface located inside of the rotor core. At least one complimentary mechanical interface member is inserted in the magnet channel and the core channel, having surfaces complimentary to the magnet channel and the core channel.

    FAN VARIABLE AREA NOZZLE WITH CABLE ACTUATOR SYSTEM
    20.
    发明申请
    FAN VARIABLE AREA NOZZLE WITH CABLE ACTUATOR SYSTEM 审中-公开
    风扇可变区域带电缆执行器系统

    公开(公告)号：US20140305097A1

    公开(公告)日：2014-10-16

    申请号：US14315396

    申请日：2014-06-26

    Applicant: United Technologies Corporation

    Inventor： Zaffir A. Chaudhry

    IPC: F02K1/12

    Abstract: An assembly for pivoting a flap according to an exemplary aspect of the present disclosure includes, among other things, a structure is mounted at least partially around an axis. The structure is attached to a pivotable flap arranged to define a nozzle area. A cable passes through an orifice defined by the flap. An actuator system is operable to mechanically retract the cable therein to lessen the nozzle area and mechanically extend the cable to enable the flow to increase the nozzle area. The actuator system is engaged with the cable. A segment of the cable, opposite the actuator system, is attached to a fixed structure. A method of providing a variable fan exit area is also disclosed.

    Abstract translation: 根据本公开的示例性方面的用于枢转翼片的组件包括除了别的以外，至少部分地围绕轴线安装结构。 该结构附接到可枢转的翼片，其布置成限定喷嘴区域。 电缆穿过由翼片限定的孔口。 致动器系统可操作以在其中机械地缩回电缆以减小喷嘴面积并且机械地延伸电缆以使流量增加喷嘴面积。 执行器系统与电缆接合。 与致动器系统相对的电缆的一段连接到固定结构。 还公开了一种提供可变风扇出口区域的方法。

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