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    FLEX CIRCUIT CONNECTOR CONFIGURATION
    91.
    发明公开
    FLEX CIRCUIT CONNECTOR CONFIGURATION 审中-公开
    FLEX电路连接器配置

    公开(公告)号：EP3220484A1

    公开(公告)日：2017-09-20

    申请号：EP17159684.4

    申请日：2017-03-07

    Applicant: Rosemount Aerospace Inc.

    Inventor： WHATCOTT, Neal R.

    IPC: H01R12/62 ,  H05K1/02 ,  H05K1/14

    Abstract: An electronic system of a device includes first (102) and second circuit boards (104) and a flexible connector configured to electrically connect the first and second circuit boards. The flexible connector includes a serpentine portion (28) that includes first, second and third legs (30, 32, 34). The first leg (30) that extends in a first direction, the second leg (32) extends in a second direction opposite of the first direction, and the third leg (34) extends in the first direction. The first, second and third legs (30, 32, 34) are configured in a common plane when the device is in an operational state.

    Abstract translation: 设备的电子系统包括第一（102）和第二电路板（104）以及被配置为电连接第一和第二电路板的柔性连接器。 该柔性连接器包括蛇形部分（28），该蛇形部分包括第一，第二和第三腿（30,32,34）。 沿第一方向延伸的第一腿部（30），第二腿部（32）沿与第一方向相反的第二方向延伸，并且第三腿部（34）沿第一方向延伸。 当装置处于操作状态时，第一，第二和第三支腿（30,32,34）被配置在共同的平面中。

    FLEX CIRCUIT CONNECTOR CONFIGURATION
    92.
    发明公开
    FLEX CIRCUIT CONNECTOR CONFIGURATION 审中-公开
    FLEX电路连接器配置

    公开(公告)号：EP3220096A1

    公开(公告)日：2017-09-20

    申请号：EP17161125.4

    申请日：2017-03-15

    Applicant: Rosemount Aerospace Inc.

    Inventor： WHATCOTT, Neal R.

    IPC: F42B35/00 ,  F42C19/06 ,  H05K1/02 ,  H05K1/14 ,  H05K3/36

    CPC classification number: H01R12/62 ,  F42B15/10 ,  F42B35/00 ,  F42C19/06 ,  H05K1/028 ,  H05K1/14 ,  H05K1/147 ,  H05K1/148 ,  H05K3/368 ,  H05K7/1434 ,  H05K2201/09027 ,  H05K2201/09063

    Abstract: An electronic system includes first and second circuit boards (202, 204) and a flexible circuit connector (40). The flexible circuit connector is configured to electrically connect the first and second circuit boards. The flexible circuit connector includes first and second connectors (42, 44) and a spiral portion (48). The first connector is configured to connect to the first circuit board. The second connector is configured to connect to the second circuit board. The spiral portion is connected between the first and second circuit boards and includes a circumferential portion (62) that extends around the second connector.

    Abstract translation: 电子系统包括第一和第二电路板（202,204）和柔性电路连接器（40）。 柔性电路连接器被配置为电连接第一和第二电路板。 柔性电路连接器包括第一和第二连接器（42,44）和螺旋部分（48）。 第一连接器被配置为连接到第一电路板。 第二连接器被配置为连接到第二电路板。 螺旋部分连接在第一和第二电路板之间并且包括围绕第二连接器延伸的周向部分（62）。

    AIR DATA PROBE WITH FLUID INTRUSION SENSOR
    93.
    发明授权
    AIR DATA PROBE WITH FLUID INTRUSION SENSOR 有权
    带有流体侵入传感器的大气数据探头

    公开(公告)号：EP2980589B1

    公开(公告)日：2017-09-13

    申请号：EP15178471.7

    申请日：2015-07-27

    Applicant: Rosemount Aerospace Inc.

    Inventor： DEANGELO, Timothy ,  SCHWARTZ, Richard Alan ,  DYKSTRA, Curt A.

    IPC: G01P13/02

    CPC classification number: G01M3/40 ,  G01N27/06 ,  G01P13/025

    Abstract: An air data probe includes a stationary housing assembly 12, an air data measurement unit 14, and a fluid sensing unit 60 disposed proximate to an interface between the housing assembly and the air data measurement unit. The air data measurement unit is rotatable about a longitudinal axis of the air data probe, relative to the stationary housing assembly. The fluid sensing unit includes a second electrically conductive sensing surface 80B physically and dielectrically spaced from a first sensing surface 80A.

    Abstract translation: 大气数据探头包括静止壳体组件12，大气数据测量单元14以及设置在壳体组件和大气数据测量单元之间的接口附近的流体传感单元60。 大气数据测量单元可相对于静止壳体组件围绕大气数据探头的纵向轴线旋转。 流体感测单元包括与第一感测表面80A物理地且介电地间隔开的第二导电感测表面80B。

    TOTAL AIR TEMPERATURE PROBE WITH EFFICIENT PARTICLE PASS THROUGH
    95.
    发明公开
    TOTAL AIR TEMPERATURE PROBE WITH EFFICIENT PARTICLE PASS THROUGH 审中-公开
    总高温探头，高效通过颗粒通过

    公开(公告)号：EP3205582A1

    公开(公告)日：2017-08-16

    申请号：EP17155028.8

    申请日：2017-02-07

    Applicant: Rosemount Aerospace Inc.

    Inventor： ISEBRAND, Scott D.

    IPC: B64D43/00 ,  G01K13/02

    CPC classification number: G01K13/028 ,  B64D43/00 ,  B64D45/00

    Abstract: A total air temperature probe (10) includes a housing (12) having inner surfaces defining an airflow passage, a first section of the airflow passage of the housing (12) having an airflow inlet scoop with a first cross-sectional area and an inertial separation bend downstream of the airflow inlet scoop, wherein the airflow passage is configured to be substantially straight; and a second section of the airflow passage of the housing having a main exit channel and an elongated outlet with a second cross-sectional area, wherein the airflow passage is contoured to direct particle deflections to the elongated outlet, wherein the second section is downstream from the first section, and wherein the first cross-sectional area is greater than the second cross-sectional area.

    Abstract translation: 总空气温度探测器（10）包括具有限定气流通道的内表面的壳体（12），壳体（12）的气流通道的第一部分具有带有第一横截面面积的气流入口勺和惯性 在所述气流入口勺下游的分离弯曲部，其中所述气流通道构造成基本笔直; 并且所述壳体的所述气流通道的第二部分具有主出口通道和具有第二横截面区域的细长出口，其中所述气流通道构造成将颗粒偏转引导至所述细长出口，其中所述第二部分位于所述细长出口的下游 第一部分，并且其中第一横截面积大于第二横截面积。

    PITOT TUBE WITH THERMALLY CONDUCTIVE INSERT
    96.
    发明公开
    PITOT TUBE WITH THERMALLY CONDUCTIVE INSERT 有权
    具有导热导热片的PITOT管

    公开(公告)号：EP3199955A1

    公开(公告)日：2017-08-02

    申请号：EP17153700.4

    申请日：2017-01-30

    Applicant: Goodrich Aerospace Services Private Limited ,  Rosemount Aerospace Inc.

    Inventor： JACOB, Robin ,  MAHAPATRA, Guru Prasad ,  JOHNSON, Paul Robert

    IPC: G01P5/165

    Abstract: A pitot tube includes a substantially cylindrical body portion (12) having an interior defining a flow passage and a tip portion (14) extending along a pitot tube axis from the body portion. The tip portion includes a disk (250), a tip cover (254) and a high thermal conductive insert (252) disposed between the disk and the tip cover and in thermal contact with both.

    Abstract translation: 皮托管包括大致圆柱形的主体部分（12），该主体部分具有限定流动通道的内部和从主体部分沿皮托管轴线延伸的尖端部分（14）。 末端部分包括盘（250），末端盖（254）和设置在盘和末端盖之间并与两者热接触的高导热插入物（252）。

    TOTAL AIR TEMPERATURE SENSORS
    99.
    发明公开
    TOTAL AIR TEMPERATURE SENSORS 审中-公开
    GESAMTLUFTTEMPERATURSENSOREN

    公开(公告)号：EP3101399A1

    公开(公告)日：2016-12-07

    申请号：EP16180210.3

    申请日：2014-10-15

    Applicant: Rosemount Aerospace Inc.

    Inventor： SCHWIE, Chester ,  CORNIEA, Kyle ,  JEWETT, Erik

    IPC: G01K13/02

    CPC classification number: B64F1/26 ,  G01K13/028

    Abstract: A total air temperature sensor includes a probe head (102), a strut (104), and a turbulence inducing surface (116). The probe head has an airflow inlet (106) and an airflow outlet (108). The strut defines a leading edge (110) and an opposed trailing edge (112) extending along a longitudinal axis (A), and connects between the probe head and an opposed probe mount (114). The turbulence inducing surface is defined in the strut aft the leading edge. The turbulence inducing surface is configured to trip a fluid boundary layer passing over the strut to transition from laminar to turbulent for moving flow separation toward the trailing edge to reduce acoustic noise emission from the total air temperature sensor.

    Abstract translation: 总空气温度传感器包括探头（102），支柱（104）和湍流诱导表面（116）。 探头具有气流入口（106）和气流出口（108）。 支柱限定了沿着纵向轴线（A）延伸的前缘（110）和相对的后缘（112），并且在探针头和相对的探针支架（114）之间连接。 湍流诱导表面定义在前缘后方的支柱中。 湍流诱导表面被配置为跳过通过支柱的流体边界层，以从层流转变为湍流，以将流动分离朝向后缘移动，以减少来自总空气温度传感器的声学噪声发射。

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