AIRFOILS WITH VIBRATION DAMPING SYSTEM
    1.
    发明申请
    AIRFOILS WITH VIBRATION DAMPING SYSTEM 有权
    具有振动阻尼系统的飞机

    公开(公告)号:US20100290893A1

    公开(公告)日:2010-11-18

    申请号:US12775804

    申请日:2010-05-07

    IPC分类号: F01D25/04

    CPC分类号: F01D5/225 F05D2300/507

    摘要: The disclosure relates to adjacently mounted circumferentially distributed turbo machine airfoils with a vibration damping system. Each adjacent pair of airfoils includes a fixing and receiving portion, extending between the paired adjacent airfoils, each with a face that are proximal (e.g., in contact with) each other. Vibration can be suppressed by the fixing and receiving portions each having a received magnet fixingly installed therein and a non-magnetic conducting plate therebetween. Each magnet has a pole that faces the pole of the other magnet in between which the non-magnetic conducting plate is located and in which eddy currents can be induced by the relative movement of the magnets due to vibration.

    摘要翻译: 本公开涉及具有减振系统的相邻安装的周向分布的涡轮机翼型。 每个相邻的一对翼型件包括固定和接收部分,其在成对的相邻翼型件之间延伸,每个具有彼此近端(例如,接触)的面。 可以通过固定和接收部分来抑制振动,所述固定和接收部分具有固定地安装在其中的接收的磁体和其间的非磁性导电板。 每个磁体具有面对位于非磁性导电板之间的另一个磁体的磁极的磁极,并且由于振动可以由磁体的相对运动引起涡流。

    Airfoils with vibration damping system
    2.
    发明授权
    Airfoils with vibration damping system 有权
    翼型减振系统

    公开(公告)号:US08376710B2

    公开(公告)日:2013-02-19

    申请号:US12775804

    申请日:2010-05-07

    IPC分类号: B64C11/16

    CPC分类号: F01D5/225 F05D2300/507

    摘要: The disclosure relates to adjacently mounted circumferentially distributed turbo machine airfoils with a vibration damping system. Each adjacent pair of airfoils includes a fixing and receiving portion, extending between the paired adjacent airfoils, each with a face that are proximal (e.g., in contact with) each other. Vibration can be suppressed by the fixing and receiving portions each having a received magnet fixingly installed therein and a non-magnetic conducting plate therebetween. Each magnet has a pole that faces the pole of the other magnet in between which the non-magnetic conducting plate is located and in which eddy currents can be induced by the relative movement of the magnets due to vibration.

    摘要翻译: 本公开涉及具有减振系统的相邻安装的周向分布的涡轮机翼型。 每个相邻的一对翼型件包括固定和接收部分,其在成对的相邻翼型件之间延伸,每个具有彼此近端(例如,接触)的面。 可以通过固定和接收部分来抑制振动,所述固定和接收部分具有固定地安装在其中的接收的磁体和其间的非磁性导电板。 每个磁体具有面对位于非磁性导电板之间的另一个磁体的磁极的磁极,并且由于振动可以由磁体的相对运动引起涡流。

    Method for determining the qualitative composition of the organic soil substance of mineral soils
    3.
    发明授权
    Method for determining the qualitative composition of the organic soil substance of mineral soils 失效
    确定矿物土壤有机土壤物质定性组成的方法

    公开(公告)号:US06382830B1

    公开(公告)日:2002-05-07

    申请号:US09601256

    申请日:2000-08-22

    申请人: Christian Siewert

    发明人: Christian Siewert

    IPC分类号: G01N2500

    CPC分类号: G01N5/04 G01N33/24

    摘要: The invention relates to a method of determining the qualitative composition of soil organic matter (SOM) of mineral soils using thermogravimetry, i.e., by subjecting a soil sample of constant weight to thermogravimetric analysis in the usual way and forming the quotient of the overall weight loss of the sample during heating from 200° C. to 450° C. and the overall weight loss of the sample during heating from 95° C. to 190° C. The method is straightforward and cost-effective, providing reliable figures for all mineral soils, regardless of region, climatic zone, or type of utilization.

    摘要翻译: 本发明涉及一种使用热重分析法确定矿物土壤的土壤有机质(SOM)的定性组成的方法,即通过以常规方式对恒重的土壤样品进行热重分析,并形成总体减重量 的样品在200°C至450°C的加热过程中,以及样品在95°C至190°C的加热过程中的总体重量损失。该方法简单直观,性价比高,为所有矿物提供了可靠的数据 土壤,不管区域,气候区或使用类型。