MATERIAL PROPERTY CAPACITANCE SENSOR
    1.
    发明申请

    公开(公告)号:WO2018152211A1

    公开(公告)日:2018-08-23

    申请号:PCT/US2018/018192

    申请日:2018-02-14

    IPC分类号: G01N27/22

    摘要: A system may include a controller configured to cause a capacitance probe to subject a material to a first electric signal having a first frequency and determine a first capacitance of the material at the first frequency. The controller is configured to cause the capacitance probe to subject the material to a second electric signal at a second frequency and determine a second capacitance of the material at the second frequency. The material includes at least a first constituent phase and a second constituent phase. The first constituent phase and the second constituent phase have substantially similar dielectric constants at the first frequency and substantially different dielectric constants at the second frequency. The controller is further configured to determine a porosity of the material based on the first capacitance and determine a relative phase composition of the first constituent phase and the second constituent phase based on the second capacitance.

    NONDESTRUCTIVE TESTING OF A COMPONENT BY THERMOGRAPHY WITH ONE HOT FLASH LAMP EXCITATION ON THE OUTSIDE AND ONE EXCITATION BY FLOWING FLUID THROUGH THE INSIDE OF THE COMPONENT
    4.
    发明申请
    NONDESTRUCTIVE TESTING OF A COMPONENT BY THERMOGRAPHY WITH ONE HOT FLASH LAMP EXCITATION ON THE OUTSIDE AND ONE EXCITATION BY FLOWING FLUID THROUGH THE INSIDE OF THE COMPONENT 审中-公开
    通过热像仪在外部进行一次热闪光灯激发的组件的非绝缘测试,以及通过流体通过组件内部的流体激活

    公开(公告)号:WO2014143300A1

    公开(公告)日:2014-09-18

    申请号:PCT/US2013/076222

    申请日:2013-12-18

    IPC分类号: G01N25/72

    CPC分类号: G06T7/0008 G01N25/72 H04N5/33

    摘要: A system and a method for nondestructive testing of a component (12), e.g. a gas turbine engine blade, on a movable stage (26) in an inspection station (11) is disclosed. It includes providing a heat pulse to the exterior of the component (12), e.g. by flashing the component using a flash lamp (20) configured for flash thermography. It further includes collecting first image data regarding the component (12) using an infrared camera (14), flowing a fluid, e.g. cooling air, from a fluid supply (22) through the component (12), and collecting second image data regarding the component (12) using the infrared camera (14).

    摘要翻译: 用于组件(12)的非破坏性测试的系统和方法,例如, 公开了一种在检查站(11)中的可移动台(26)上的燃气涡轮发动机叶片。 它包括向组件(12)的外部提供加热脉冲,例如。 通过使用配置为闪光热成像的闪光灯(20)来闪烁组件。 它还包括使用红外线照相机(14)收集关于组件(12)的第一图像数据,流动流体,例如, 从流体供应源(22)通过部件(12)冷却空气,以及使用红外相机(14)收集关于部件(12)的第二图像数据。

    SLOTTED LABYRINTH SEAL
    8.
    发明申请
    SLOTTED LABYRINTH SEAL 审中-公开
    缝制乳胶密封

    公开(公告)号:WO2014138623A1

    公开(公告)日:2014-09-12

    申请号:PCT/US2014/021902

    申请日:2014-03-07

    发明人: GORE, Patrick, E.

    IPC分类号: F16J15/447 F01D11/02

    摘要: A seal for use in a machine, such as a machine with rotating members, includes a labyrinth seal with multiple fins. The seal is slotted and is designed to limit fluid flow to the desired amount from the high pressure side of the seal to the low pressure side of the seal inside partially or exclusively radially extending cavities between two rotating members. The rotating members may operate at different speeds with a common axis of rotation. The seal remains effective when the rotating members move axially in relation to one another despite the fins having a component parallel to the axis of rotation.

    摘要翻译: 用于机器的密封件,例如具有旋转构件的机器,包括具有多个翅片的迷宫式密封件。 密封件是开槽的,并且被设计成将流体流量从密封件的高压侧限制到密封件的低压侧,部分地或仅在两个旋转构件之间的径向延伸的空腔中。 旋转构件可以以与公共旋转轴线不同的速度操作。 尽管翅片具有平行于旋转轴线的分量,但是当旋转构件相对于彼此轴向移动时,密封件仍然有效。

    GAS TURBINE ENGINE FUEL AIR MIXER
    10.
    发明申请
    GAS TURBINE ENGINE FUEL AIR MIXER 审中-公开
    燃气涡轮发动机燃油空气混合器

    公开(公告)号:WO2014137412A1

    公开(公告)日:2014-09-12

    申请号:PCT/US2013/067769

    申请日:2013-10-31

    发明人: NICKOLAUS, Daniel

    摘要: A gas turbine engine device is disclosed for mixing fuel and air prior to a combustion. The device includes a pilot mixer (60) and a main mixer (62) each having a fuel opening (88, 68) for the delivery of fuel to one or more passages. In one form the main mixer includes an inner passage (74) and an outer passage (76) and in which a fuel opening delivers fuel to the inner passage (74). The main mixer (62) can include swirlers in the inner and/or outer passages. The pilot mixer (60) can also include a swirler (66). In one embodiment the main mixer (62) includes a converging flow path and/or a diverging flow path. The pilot mixer (60) can also include a converging and/or diverging flow path and in one form is sheltered from an exit of the device. The main mixer fuel opening (88) can be disposed between an upstream end and a downstream end of the mixer.

    摘要翻译: 公开了一种在燃烧之前混合燃料和空气的燃气涡轮发动机装置。 该装置包括一个先导式混合器(60)和一个主混合器(62),每个混合器具有用于将燃料输送到一个或多个通道的燃料开口(88,68)。 在一种形式中,主混合器包括内通道(74)和外通道(76),其中燃料开口将燃料输送到内通道(74)。 主混合器(62)可以在内部和/或外部通道中包括旋流器。 引燃混合器(60)还可以包括旋流器(66)。 在一个实施例中,主混合器(62)包括会聚流动路径和/或发散流动路径。 先导混合器(60)还可以包括会聚和/或发散的流动路径,并且一种形式从设备的出口被遮蔽。 主混合器燃料开口(88)可以设置在混合器的上游端和下游端之间。