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    Pressure Difference Sensor
    2.
    发明申请
    Pressure Difference Sensor 审中-公开

    公开(公告)号：US20180031434A1

    公开(公告)日：2018-02-01

    申请号：US15652341

    申请日：2017-07-18

    申请人： Endress + Hauser GmbH + Co. KG

    发明人： Timo Kober ,  Benjamin Lemke ,  Rafael Teipen ,  Benjamin Mack

    IPC分类号： G01L19/04 ,  G01L9/00 ,  G01L13/06

    CPC分类号： G01L19/04 ,  G01L9/0072 ,  G01L9/0095 ,  G01L13/025 ,  G01L13/06 ,  G01L19/0007 ,  G01L19/0618 ,  G01L19/0681

    摘要： A pressure difference sensor for providing a pressure measurement signal, comprising: a pressure difference measuring cell, which is suppliable with first and second pressures and which outputs the pressure measurement signal; first and second ceramic stiffening elements, each of which is joined with the pressure difference measuring cell and has a duct, via which the first, respectively the second, pressure is suppliable to the pressure difference measuring cell; a platform with first and second pressure input openings, each of which extends from a first surface to a second surface of the platform, wherein the pressure input openings are sealed on the first surface, each with its own isolating diaphragm, and first and second pressures tubes, which are arranged between the stiffening elements and the platform, and wherein each of the first pressure tube and the second pressure tube has at least one bend in a region between the platform and a first, respectively second, connecting area of the corresponding pressure tube.

    SYSTEM FOR DETECTING A PRESSURE DIFFERENCE BETWEEN THE INTERIOR AND THE EXTERIOR OF AN AIRCRAFT
    4.
    发明申请
    SYSTEM FOR DETECTING A PRESSURE DIFFERENCE BETWEEN THE INTERIOR AND THE EXTERIOR OF AN AIRCRAFT 审中-公开
    检测内部与飞机外部压力差异的系统

    公开(公告)号：US20160061680A1

    公开(公告)日：2016-03-03

    申请号：US14844413

    申请日：2015-09-03

    申请人： Airbus Operations GmbH

    发明人： Thorsten KNIJNENBURG ,  Albin POTH

    IPC分类号： G01L13/06 ,  G01L19/14

    CPC分类号： G01L13/06 ,  B64C1/1492 ,  B64D13/04 ,  G01L19/143 ,  Y02T50/44

    摘要： A system to detect a pressure difference between the interior of a cabin of an aircraft and the exterior of the aircraft. The system includes a window arrangement having a first windowpane with a first surface and an opposite second surface and is adapted to be mounted in an aircraft such that the first surface of the first windowpane faces the exterior of the aircraft and is subjected to ambient outside atmospheric pressure and the second surface faces the cabin interior, and a pressure sensor including a first pressure port. The first windowpane includes a first air passage opening extending between the first and second surfaces of the first windowpane, and the pressure sensor is sealingly connected to the first air passage opening such that the first pressure port of the pressure sensor is subjected to pressure acting on the first surface of the first windowpane.

    摘要翻译： 一种用于检测飞行器舱室内部与飞行器外部之间的压力差的系统。 该系统包括具有第一窗玻璃的窗口装置，第一窗玻璃具有第一表面和相对的第二表面，并且适于安装在飞行器中，使得第一窗玻璃的第一表面面向飞行器的外部并且经受环境外的大气 并且所述第二表面面向所述舱内部，以及包括第一压力端口的压力传感器。 第一窗玻璃包括在第一窗玻璃的第一和第二表面之间延伸的第一空气通道开口，并且压力传感器密封地连接到第一空气通道开口，使得压力传感器的第一压力端口受到作用于 第一个窗玻璃的第一个表面。

    SELF PUMPING AND SENSING HOSE UTILIZING ELECTROACTIVE POLYMER STRIPS
    5.
    发明申请
    SELF PUMPING AND SENSING HOSE UTILIZING ELECTROACTIVE POLYMER STRIPS 有权
    自吸泵和感应软管利用电动聚合物条

    公开(公告)号：US20150000423A1

    公开(公告)日：2015-01-01

    申请号：US14346826

    申请日：2012-09-24

    申请人： PARKER-HANNIFIN CORPORATION

    发明人： Jason T. Dunn ,  Mario A. Calvo ,  Andrew Brenner ,  Kenji A. Kingsford

    IPC分类号： F04B43/09 ,  G01F15/00 ,  G01L13/02 ,  G01F1/38 ,  F04B43/00 ,  G01L13/06

    CPC分类号： F04B43/09 ,  F04B43/0072 ,  F04B43/04 ,  G01F1/383 ,  G01F15/006 ,  G01L13/021 ,  G01L13/06

    摘要： One or more electroactive polymer (EAP) strips are circumferentially or lengthwise embedded or mounted around the fluid passage member. The EAP strips are configured to function as a pump when a prescribed electrical charge is applied and removed from the EAP strips, which causes the EAP strips to expand and constrict accordingly. A series of these strips may be mounted along a portion of the fluid passage member and electrically actuated in a prescribed manner to exert a squeezing force around the fluid passage member, which functions to pump fluid through the fluid passage member. The EAP strips also change electrical characteristics (e.g., capacitance, resistance) independent of the applied actuation as they are stretched, so they may be used to measure fluid pressure and/or fluid flow rate.

    摘要翻译： 一个或多个电活性聚合物（EAP）条在周向或纵向嵌入或安装在流体通道构件周围。 EAP条被配置为当从EAP条带上施加规定的电荷并从EAP条上移除时用作泵，这导致EAP条带相应地膨胀和收缩。 一系列这些条可以沿着流体通道构件的一部分安装并且以规定的方式电动致动，以便在流体通道构件周围施加挤压力，其作用是将流体泵送通过流体通道构件。 当它们被拉伸时，EAP带还可以独立于施加的致动而改变电特性（例如，电容，电阻），因此它们可以用于测量流体压力和/或流体流速。

    Ultra-precision micro-differential pressure measuring device and ultra-precision differential pressure measuring device
    7.
    发明申请
    Ultra-precision micro-differential pressure measuring device and ultra-precision differential pressure measuring device 审中-公开
    超精密微差压测量装置和超精密差压测量装置

    公开(公告)号：US20070022817A1

    公开(公告)日：2007-02-01

    申请号：US11536925

    申请日：2006-09-29

    申请人： Kotohiko SEKOGUCHI

    发明人： Kotohiko SEKOGUCHI

    IPC分类号： G01L15/00

    CPC分类号： G01L13/06

    摘要： The ultra-precision micro-differential pressure measuring device comprises a device body 1 having an inner space part therein, a pressure receiving plate 3 which is installed inside the inner space of the device body 1 and divides the said inner space hermetically into a lower space 7 and an upper part space 8, an electronic weighing and pressure converting device 2 which is installed in the lower space 7, and supports and secures the pressure receiving plate 3, and a liquid sealing part R which liquid-seals the outer peripheral part of the afore-mentioned pressure receiving plate 3 and maintains the air-tightness between the lower space 7 and the upper space 8. A micro-differential pressure between a pressure P1 inside the upper space 8 and a pressure P2 inside the lower space 7 is measured by the electronic weighing and pressure converting device 2 through the pressure receiving plate 3.

    摘要翻译： 超精密微差压测量装置包括其内部具有内部空间部分的装置主体1，压力接收板3，其安装在装置主体1的内部空间内部，并将所述内部空间气密地分成下部空间 7和上部空间8，电子称重和压力转换装置2，其安装在下部空间7中，并且支撑并固定压力接收板3;以及液体密封部分R，液体密封部分 上述压力接收板3并且保持下部空间7和上部空间8之间的气密性。 电子称量压力变换装置2通过受压板3测定上部空间8内的压力P 1与下部空间7内的压力P 2之间的微差压。

    Measurement mechanism for differential pressure measurement
    8.
    发明申请
    Measurement mechanism for differential pressure measurement 失效
    差压测量的测量机构

    公开(公告)号：US20030005773A1

    公开(公告)日：2003-01-09

    申请号：US10172236

    申请日：2002-06-14

    发明人： Wolfgang Scholz ,  Albrecht Vogel ,  Peter Krippner ,  Manfred Wetzko

    IPC分类号： G01L009/00

    CPC分类号： G01L13/06

    摘要： There is disclosed a measurement mechanism for differential pressure measurement. The mechanism has two housing portions with flanges. A differential pressure sensor is force-fit between the two flange faces. An electronics board is connected to the differential pressure sensor by means of a force-fit electrical contact.

    摘要翻译： 公开了用于差压测量的测量机构。 该机构具有带法兰的两个壳体部分。 差压传感器是两个法兰面之间的力配合。 电子板通过压配电接触连接到压差传感器。