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    • 1. 发明授权
    • Apparatus and method for non-contacting blade oscillation measurement
    • 不接触叶片振动测量的装置和方法
    • US08225671B2
    • 2012-07-24
    • US12520453
    • 2007-12-12
    • Michael ZielinskiGerhard Ziller
    • Michael ZielinskiGerhard Ziller
    • G01H1/00
    • G01H1/006
    • An apparatus and method for non-contact blade vibration measurement is disclosed. The apparatus and method includes sensors which are arranged around the circumference of a rotor which is formed with rotor blades, a signal detection unit, and an evaluation unit. Devices are provided to determine the rotor position and/or the housing deformation. This avoids the technical problems of the prior art, and provides an improved apparatus and an improved method for non-contact blade vibration measurement. In particular, the attainment according to the invention eliminates the effect of rotor radial movements and housing deformations, i.e., oval deformations, on the measurement data, thereby ensuring high amplitude resolution for the vibration analysis under all conditions.
    • 公开了一种用于非接触式叶片振动测量的装置和方法。 该装置和方法包括围绕形成有转子叶片的转子的圆周布置的传感器,信号检测单元和评估单元。 提供设备以确定转子位置和/或壳体变形。 这避免了现有技术的技术问题,并且提供了一种用于非接触式叶片振动测量的改进的装置和改进的方法。 特别地,根据本发明的实现消除了转子径向运动和壳体变形(即,椭圆形变形)对测量数据的影响,从而确保了在所有条件下的振动分析的高振幅分辨率。
    • 2. 发明申请
    • Device and method for determining torques on a turbine shaft
    • 用于确定涡轮轴上的扭矩的装置和方法
    • US20060032319A1
    • 2006-02-16
    • US11201947
    • 2005-08-11
    • Michael Zielinski
    • Michael Zielinski
    • G01L1/22
    • G01L3/12
    • A device is described for determining the torque which is applied to a turbine shaft (10), the determination device having at least one system for contactless measurement of the integral torsion of the turbine shaft (10) and a unit for contactless measurement of the restoring constant of the turbine shaft (10). Furthermore, a method is described for determining the torque which is applied to the low-pressure turbine shaft (10) of a turbine engine, which is distinguished in that, to determine the torque, the integral torsion of the turbine shaft is measured by a contactless method and the restoring constant of the turbine shaft is measured.
    • 描述了一种用于确定施加到涡轮轴(10)的扭矩的装置,所述确定装置具有至少一个用于非接触式测量涡轮轴(10)的整体扭矩的系统和用于非接触式测量恢复的单元 涡轮轴(10)的常数。 此外,描述了一种用于确定施加到涡轮发动机的低压涡轮机轴(10)的扭矩的方法,其特征在于为了确定扭矩,涡轮轴的整体扭矩由 测量非接触式方法和涡轮轴的恢复常数。
    • 3. 发明授权
    • Method for producing time marks at any points on moving components
    • 移动部件上任何点产生时间标记的方法
    • US06587207B2
    • 2003-07-01
    • US09913873
    • 2001-10-13
    • Roland HessertMichael ZielinskiGerhard Ziller
    • Roland HessertMichael ZielinskiGerhard Ziller
    • G01B902
    • G01H9/00
    • In a method for generating time markers of arbitrary points on moving components and an optical trigger device for performing the method, light from a broadband light source with a correspondingly short coherence length is split into two paths, namely a measurement light path and a reference light path, and is coupled into two optical waveguides, the light of the reference light path is at least partially coupled back and the light of the measurement light path is focused at a measurement point and reflected by the component passing through the focus, wherein the light distances in the measurement light path up to the focus and in the reference light path up to the coupling-back plane are of the same length within the coherence length of the radiated light, wherein the coupled-back light from the reference light path and the measurement light path is brought to interference and detected by a detector, and wherein a short modulation event occurs at the detector when the component passes through the focus.
    • 在用于产生移动部件上的任意点的时间标记的方法和用于执行该方法的光学触发装置的方法中,来自具有相应短的相干长度的宽带光源的光被分成两条路径,即测量光路和参考光 并且被耦合到两个光波导中,参考光路的光至少部分耦合回来,并且测量光路的光聚焦在测量点处并被穿过焦点的分量反射,其中光 在测量光路中直到聚焦和参考光路直到耦合背面的距离在辐射光的相干长度内具有相同的长度,其中来自参考光路的耦合反射光和 测量光路由检测器引起干扰并检测,并且其中当分量通过时,在检测器处发生短调制事件 通过焦点。
    • 4. 发明授权
    • Turbomachine, gap-measuring system, and method for determining a rotor gap
    • 涡轮机,间隙测量系统和确定转子间隙的方法
    • US08560266B2
    • 2013-10-15
    • US12739720
    • 2008-10-17
    • Michael Zielinski
    • Michael Zielinski
    • G01B7/14G01B11/14
    • G01B7/14F01D11/20F01D21/003Y02T50/671
    • The invention relates to a turbomachine having a rotor (10) comprising rotor blades (12), having a rotor housing (16) which surrounds at least sections of the rotor (10) or the rotor blade (12) so as to form a rotor gap (d), and having a gap-measuring system (18) which is coupled to a capacitive sensor device (20) having an electrode and a counterelectrode for determining measured capacitance values (C) which characterize the rotor gap (d), wherein the rotor (10) or the rotor blades (12) is/are connected as the electrode of the sensor device (20), wherein at least part (22) of the rotor housing (16) is connected as the counterelectrode. The invention also relates to a gap-measuring system (18) and to a method for determining a rotor gap (d) between a rotor (10) comprising rotor blades (12) and a rotor housing (16) of a turbomachine, which rotor housing surrounds at least sections of the rotor (10) or the rotor blades (12).
    • 本发明涉及一种涡轮机,其具有包括转子叶片(12)的转子(10),转子叶片(12)具有围绕转子(10)或转子叶片(12)的至少部分的转子壳体(16),以形成转子 间隙(d),并且具有间隙测量系统(18),该间隙测量系统(18)耦合到具有电极和反电极的电容传感器装置(20),用于确定表征转子间隙(d)的测量电容值(C),其中 转子(10)或转子叶片(12)作为传感器装置(20)的电极连接,其中转子壳体(16)的至少一部分(22)作为反电极连接。 本发明还涉及一种间隙测量系统(18)以及用于确定包括转子叶片(12)的转子(10)和涡轮机的转子壳体(16)之间的转子间隙(d)的方法,该转子 壳体围绕转子(10)或转子叶片(12)的至少部分。
    • 7. 发明申请
    • Self-tightening hose clamp
    • 自紧软管夹
    • US20060131875A1
    • 2006-06-22
    • US10999009
    • 2004-11-29
    • Michael Zielinski
    • Michael Zielinski
    • F16L33/00
    • F16L33/03D06F39/083
    • A method of applying a self-tightening hose clamp including the steps of providing a self-tightening hose clamp having a flexible member with a substantially circular shape and disposed in a first plane. The flexible member being expandable from a first position defining a first opening to a second position defining a second opening, the second opening being larger than the first opening. The flexible member also having first and second spaced apart ends. The flexible member is expanded from the first position to the second position. A first tubular member is then received in the opening of the hose clamp and the hose clamp is translated in a first direction along the first tubular member. The tubular member having a hollow chamber extending therethrough. A second tubular member is placed within the hollow chamber of the first tubular member, and the hose clamp is translated along the first tubular member to a position overlapping the second tubular member. The hose clamp is then allowed to contract back to the first position from the second position.
    • 一种施加自动紧固软管夹的方法,包括以下步骤:提供具有基本圆形形状并设置在第一平面中的柔性构件的自紧软管夹。 柔性构件从限定第一开口的第一位置可膨胀到限定第二开口的第二位置,第二开口大于第一开口。 柔性构件还具有第一和第二间隔开的端部。 柔性构件从第一位置扩展到第二位置。 然后将第一管状构件容纳在软管夹的开口中,并且软管夹沿着第一管状构件沿第一方向平移。 管状构件具有延伸穿过其中的中空室。 第二管状构件放置在第一管状构件的中空室内,并且软管夹沿着第一管状构件平移到与第二管状构件重叠的位置。 然后允许软管夹从第二位置收缩回第一位置。
    • 8. 发明申请
    • TURBOMACHINE, GAP-MEASURING SYSTEM, AND METHOD FOR DETERMINING A ROTOR GAP
    • 涡轮机,GAP测量系统和确定转子隙的方法
    • US20100268509A1
    • 2010-10-21
    • US12739720
    • 2008-10-17
    • Michael Zielinski
    • Michael Zielinski
    • G01B7/14
    • G01B7/14F01D11/20F01D21/003Y02T50/671
    • The invention relates to a turbomachine having a rotor (10) comprising rotor blades (12), having a rotor housing (16) which surrounds at least sections of the rotor (10) or the rotor blade (12) so as to form a rotor gap (d), and having a gap-measuring system (18) which is coupled to a capacitive sensor device (20) having an electrode and a counterelectrode for determining measured capacitance values (C) which characterize the rotor gap (d), wherein the rotor (10) or the rotor blades (12) is/are connected as the electrode of the sensor device (20), wherein at least part (22) of the rotor housing (16) is connected as the counterelectrode. The invention also relates to a gap-measuring system (18) and to a method for determining a rotor gap (d) between a rotor (10) comprising rotor blades (12) and a rotor housing (16) of a turbomachine, which rotor housing surrounds at least sections of the rotor (10) or the rotor blades (12).
    • 本发明涉及一种涡轮机,其具有包括转子叶片(12)的转子(10),转子叶片(12)具有围绕转子(10)或转子叶片(12)的至少部分的转子壳体(16),以形成转子 间隙(d),并且具有间隙测量系统(18),该间隙测量系统(18)耦合到具有电极和反电极的电容传感器装置(20),用于确定表征转子间隙(d)的测量电容值(C),其中 转子(10)或转子叶片(12)作为传感器装置(20)的电极连接,其中转子壳体(16)的至少一部分(22)作为反电极连接。 本发明还涉及一种间隙测量系统(18)以及用于确定包括转子叶片(12)的转子(10)和涡轮机的转子壳体(16)之间的转子间隙(d)的方法,该转子 壳体围绕转子(10)或转子叶片(12)的至少部分。
    • 9. 发明授权
    • Device and method for determining torques on a turbine shaft
    • 用于确定涡轮轴上的扭矩的装置和方法
    • US07398701B2
    • 2008-07-15
    • US11201947
    • 2005-08-11
    • Michael Zielinski
    • Michael Zielinski
    • G01L1/22
    • G01L3/12
    • A device is described for determining the torque which is applied to a turbine shaft (10), the determination device having at least one system for contactless measurement of the integral torsion of the turbine shaft (10) and a unit for contactless measurement of the restoring constant of the turbine shaft (10). Furthermore, a method is described for determining the torque which is applied to the low-pressure turbine shaft (10) of a turbine engine, which is distinguished in that, to determine the torque, the integral torsion of the turbine shaft is measured by a contactless method and the restoring constant of the turbine shaft is measured.
    • 描述了一种用于确定施加到涡轮轴(10)的扭矩的装置,所述确定装置具有至少一个用于非接触式测量涡轮轴(10)的整体扭矩的系统和用于非接触式测量恢复的单元 涡轮轴(10)的常数。 此外,描述了一种用于确定施加到涡轮发动机的低压涡轮机轴(10)的扭矩的方法,其特征在于为了确定扭矩,涡轮轴的整体扭矩由 测量非接触式方法和涡轮轴的恢复常数。
    • 10. 发明申请
    • Illuminator-especially for cylindrical curved surfaces
    • 照明器 - 特别适用于圆柱形曲面
    • US20070097686A1
    • 2007-05-03
    • US11591343
    • 2006-11-01
    • Sheila DunnJoseph FlammeMichael MessinaMichael Zielinski
    • Sheila DunnJoseph FlammeMichael MessinaMichael Zielinski
    • F21S13/14
    • G01N21/952G01N21/8806G01N2021/8812G01N2021/8816G01N2201/062G01N2201/0634
    • A plurality of LED's, or electro luminescent strips, are disposed to project illumination to and thru, or towards, a diffuser; resulting in at least a portion of generated diffuse illumination being directed towards and upon the cylindrical surface of an article or part when disposed at an article illumination location. The article illumination location is established so that a centerline through the article is co-linear with a center line of the diffuse illumination projecting from, or reflected from, the diffusers. A housing may be provided for the LED's, electro luminescent strips and diffusers; or they may be otherwise arranged to coact to provide diffuse illumination directed towards the cylindrical surface of the part or other article. illumination reflected off of the article's cylindrical surface, and/or any markings, such as symbology, carried thereby is directed to a lens/camera arrangement to provide an image of same for transmission to a computer, controller, smart camera or other image utilization system.
    • 多个LED或电致发光条被设置成将照明照射到扩散器上并通过或朝向扩散器; 导致当设置在物品照明位置时,产生的漫射照明的至少一部分被引向物品或部件的圆柱形表面并朝向物体或部件的圆柱形表面。 物品照明位置被建立为使得穿过物品的中心线与从扩散器突出或从扩散器反射的漫射照明的中心线是共线的。 可以为LED,电致发光条和扩散器提供壳体; 或者它们可以以其它方式布置成共同作用以提供朝向部件或其它物品的圆柱形表面的漫射照明。 由物品的圆柱形表面反射的照明和/或由其携带的诸如符号系统的任何标记被引导到透镜/照相机装置,以提供相同的图像以传送到计算机,控制器,智能相机或其他图像利用系统 。